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MALIBU MIRAGE

PA-46-350P

SN 4636196 AND UP

PILOT’S

OPERATING

HANDBOOK

AND

FAA APPROVED

AIRPLANE FLIGHT MANUAL

AIRPLANE AIRPLANE

SERIAL NO. ___________________________ REGIST. NO. _______________________

PA-46-350P

REPORT: VB-1710 FAA APPROVED BY:

PETER E. PECK

D.O.A. NO. SO-1

DATE OF APPROVAL: THE NEW PIPER AIRCRAFT, INC.

FEBRUARY 23, 1999 VERO BEACH, FLORIDA

THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE

PILOT BY THE FEDERAL AVIATION REGULATIONS AND ADDITIONAL INFORMATION

PROVIDED BY THE MANUFACTURER AND CONSTITUTES THE FAA APPROVED

AIRPLANE FLIGHT MANUAL. THIS HANDBOOK MUST BE CARRIED IN THE

AIRPLANE AT ALL TIMES.

MALIBU MIRAGE

PA-46-350P

SN 4636196 AND UP

PILOT’S

OPERATING

HANDBOOK

AND

FAA APPROVED

AIRPLANE FLIGHT MANUAL

AIRPLANE AIRPLANE

SERIAL NO. ___________________________ REGIST. NO. _______________________

PA-46-350P

REPORT: VB-1710 FAA APPROVED BY:

PETER E. PECK

D.O.A. NO. SO-1

DATE OF APPROVAL: THE NEW PIPER AIRCRAFT, INC.

FEBRUARY 23, 1999 VERO BEACH, FLORIDA

THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE

PILOT BY THE FEDERAL AVIATION REGULATIONS AND ADDITIONAL INFORMATION

PROVIDED BY THE MANUFACTURER AND CONSTITUTES THE FAA APPROVED

AIRPLANE FLIGHT MANUAL. THIS HANDBOOK MUST BE CARRIED IN THE

AIRPLANE AT ALL TIMES.

TM TM

FOR REFERENCE ONLY

NOT FOR FLIGHT

Summary of content (417 pages)

PAGE 1
MALIBU MIRAGE MALIBU MIRAGE PA-46-350P PA-46-350P SN 4636196 AND UP SN 4636196 AND UP PILOT’S OPERATING HANDBOOK PILOT’S OPERATING HANDBOOK AND Y L NAPPROVED FAA O AIRPLANEEFLIGHT MANUAL C N E HT R E LIG F E F R R R O FO T F NO AND FAA APPROVED AIRPLANE FLIGHT MANUAL AIRPLANE SERIAL NO. ___________________________ AIRPLANE REGIST. NO. _______________________ PA-46-350P REPORT: VB-1710 FAA APPROVED BY: DATE OF APPROVAL: FEBRUARY 23, 1999 AIRPLANE SERIAL NO.
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WARNING WARNING EXTREME CARE MUST BE EXERCISED TO LIMIT THE USE OF THIS HANDBOOK TO APPLICABLE AIRCRAFT. T H I S H A N D - B O O K I S VA L I D F O R U S E W I T H T H E AIRPLANE IDENTIFIED ON THE FACE OF THE TITLE PAGE. SUBSEQUENT REVISIONS SUPPLIED BY PIPER MUST BE PROPERLY INSERTED. EXTREME CARE MUST BE EXERCISED TO LIMIT THE USE OF THIS HANDBOOK TO APPLICABLE AIRCRAFT. T H I S H A N D - B O O K I S VA L I D F O R U S E W I T H T H E AIRPLANE IDENTIFIED ON THE FACE OF THE TITLE PAGE.
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PA-46-350P, MALIBU PA-46-350P, MALIBU APPLICABILITY APPLICABILITY Application of this handbook is limited to the specific Piper PA-46-350P model airplane designated by serial number and registration number on the face of the title page of this handbook. Application of this handbook is limited to the specific Piper PA-46-350P model airplane designated by serial number and registration number on the face of the title page of this handbook.
PAGE 4
PA-46-350P, MALIBU PA-46-350P, MALIBU REVISIONS REVISIONS The information compiled in the Pilot’s Operating Handbook, with the exception of the equipment list, will be kept current by revisions distributed to the airplane owners. The equipment list was current at the time the airplane was licensed by the manufacturer and thereafter must be maintained by the owner.
PAGE 5
PA-46-350P, MALIBU PA-46-350P, MALIBU PILOT'S OPERATING HANDBOOK LOG OF REVISIONS PILOT'S OPERATING HANDBOOK LOG OF REVISIONS Current Revisions to the PA-46-350P Malibu Pilot's Operating Handbook, REPORT: VB-1710 issued FEBRUARY 23, 1999. Revision FAA Approved Number and Revised Description of Revisions Signature Code Pages and Date Rev. 1 v Added Rev. 1 to L of R pg. (PR990920) 3-11 Revised para. 3.3m 3-12 Revised para. 3.3m 3-32 Revised para. 3.27 3-35 Revised para. 3.43 4-13 Revised para. 4.
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PA-46-350P, MALIBU PA-46-350P, MALIBU PILOT'S OPERATING HANDBOOK LOG OF REVISIONS (cont) Revision Number and Code Rev. 1 (continued) Revised Pages 9-115 thru 9-122 Description of Revisions Added Section 9 Supplement 15 FAA Approved Signature and Date PILOT'S OPERATING HANDBOOK LOG OF REVISIONS (cont) Revision Number and Code Rev. 1 (continued) Revised Pages 9-115 thru 9-122 Peter E. Peck Description of Revisions Added Section 9 Supplement 15 Rev.
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PA-46-350P, MALIBU PA-46-350P, MALIBU PILOT'S OPERATING HANDBOOK LOG OF REVISIONS (cont) Revision FAA Approved Number and Revised Description of Revisions Signature Code Pages and Date Rev. 3 9-133 Added pages (PR010910) thru and Supplement 18. continued 9-142 9-143 Added pages thru and Supplement 19. 9-150 9-151 Added pages thru and Supplement 20. 9-156 9-157 Added pages Peter E. Peck thru and Supplement 21. 9-160 Sept. 10, 2001 Date Rev. 4 (PR011220) vi-a 9-116 Added Rev. 4 to L of R.
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PA-46-350P, MALIBU PA-46-350P, MALIBU PILOT'S OPERATING HANDBOOK LOG OF REVISIONS (cont) Revision Number and Code Rev. 7 (PR021014) Revised Pages iii iv vi-b 8-1 8-1A 8-1B 8-2 Rev. 8 (PR021108) Rev. 9 (PR040120) Description of Revisions Added Warning and moved info. to page iv. Moved info. from page iii. Added Rev. 7 to L of R. Moved info. to page 8-1B and revised para. 8.1. Added page and revised para. 8.1. Added page and moved info. from pages 8-1 and 8-2. Moved info. to page 8-1B and revised para.
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PA-46-350P, MALIBU PA-46-350P, MALIBU PILOT'S OPERATING HANDBOOK LOG OF REVISIONS (cont) Revision FAA Approved Number and Revised Description of Revisions Signature Code Pages and Date Rev. 10 vi-c Added page and Rev. 10 (PR040724) to L of R. vi-d Added page. 4-41 Revised para. 4.50. Albert J. Mill July 24, 2004 PILOT'S OPERATING HANDBOOK LOG OF REVISIONS (cont) Revision FAA Approved Number and Revised Description of Revisions Signature Code Pages and Date Rev. 10 vi-c Added page and Rev.
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PA-46-350P, MALIBU PA-46-350P, MALIBU PILOT'S OPERATING HANDBOOK LOG OF REVISIONS (cont) Revision Number and Code Revised Pages Description of Revisions FAA Approved Signature and Date PILOT'S OPERATING HANDBOOK LOG OF REVISIONS (cont) Revision Number and Code Revised Pages Description of Revisions FAA Approved Signature and Date Y L N O E C N E HT R E LIG F E F R R R O FO T F NO REPORT: VB-1710 vi-d ISSUED: FEBRUARY 23, 1999 REVISED: JULY 24, 2004 REPORT: VB-1710 vi-d ISSUED: FEBRUARY 23, 199
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PA-46-350P, MALIBU PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 1 GENERAL SECTION 1 GENERAL SECTION 2 LIMITATIONS SECTION 2 LIMITATIONS SECTION 3 EMERGENCY PROCEDURES SECTION 3 EMERGENCY PROCEDURES SECTION 4 NORMAL PROCEDURES SECTION 4 NORMAL PROCEDURES SECTION 5 PERFORMANCE SECTION 5 PERFORMANCE SECTION 6 WEIGHT AND BALANCE SECTION 6 SECTION 7 DESCRIPTION AND OPERATION OF THE AIRPLANE AND ITS SYSTEMS SECTION 8 AIRPLANE HANDLING, SERVICING AND MAINTENANCE SEC
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SECTION GENERAL PA-46-350P, MALIBU SECTION GENERAL PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 1 SECTION 1 GENERAL GENERAL Paragraph No. 1.1 1.3 1.5 1.7 1.9 1.11 1.13 1.15 1.17 1.19 1.21 Page No. Introduction .............................................................................. Engine....................................................................................... Propeller ................................................................................... Fuel.
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SECTION 1 GENERAL PA-46-350P, MALIBU SECTION 1 GENERAL PA-46-350P, MALIBU SECTION 1 SECTION 1 GENERAL GENERAL 1.1 INTRODUCTION 1.1 INTRODUCTION This Pilot’s Operating Handbook is designed for maximum utilization as an operating guide for the pilot. It includes the material required to be furnished to the pilot by the Federal Aviation Regulations and additional information provided by the manufacturer and constitutes the FAA Approved Airplane Flight Manual.
PAGE 14
SECTION 1 GENERAL PA-46-350P, MALIBU SECTION 1 GENERAL PA-46-350P, MALIBU Y L N O E C N E HT R E LIG F E F R R R O FO T F NO THREE VIEW Figure 1-1 REPORT: VB-1710 1-2 ISSUED: FEBRUARY 23, 1999 THREE VIEW Figure 1-1 REPORT: VB-1710 1-2 ISSUED: FEBRUARY 23, 1999
PAGE 15
PA-46-350P, MALIBU 1.3 ENGINE (a)Number of Engines (b) Engine Manufacturer (c) Engine Model Number (d) Rated Horsepower (e) Rated Speed (rpm) (f) Maximum Manifold Pressure (in. Hg.) (g) Bore (inches) (h) Stroke (inches) (i) Displacement (cubic inches) (j) Compression Ratio (k) Engine Type 1.
PAGE 16
SECTION 1 GENERAL PA-46-350P, MALIBU 1.7 FUEL (2) Alternate Fuels PA-46-350P, MALIBU 1.7 FUEL AVGAS ONLY (a) Fuel Capacity (U.S. gal.) (total) (b) Usable Fuel (U.S. gal.) (total) (c) Fuel (1) Minimum Grade SECTION 1 GENERAL AVGAS ONLY 122 120 100- Green or 100LL Blue Aviation Grade Refer to latest revision of Lycoming Service Instruction 1070, except alcohol is not approved for use in this airplane. 1.9 OIL (a) Fuel Capacity (U.S. gal.) (total) (b) Usable Fuel (U.S. gal.
PAGE 17
PA-46-350P, MALIBU SECTION 1 GENERAL 1.11 MAXIMUM WEIGHTS (a) (b) (c) (d) (e) Maximum Ramp Weight (lb) Maximum Takeoff Weight (lb) Maximum Landing Weight (lb) Maximum Zero Fuel Weight (lb) Maximum Weights in Baggage Compartments (lb) (1) Forward (2) Aft 1.11 MAXIMUM WEIGHTS 4358 4340 4123 4123 100 100 1.13 STANDARD AIRPLANE WEIGHTS 1.15 CABIN AND ENTRY DIMENSIONS (IN.) 49.5 148 47 24 46 13 20 19 x 23 24 x 46 1.19 SPECIFIC LOADING (a) Wing Loading (lbs. per sq. ft.) (b) Power Loading (lbs.
PAGE 18
SECTION 1 GENERAL PA-46-350P, MALIBU SECTION 1 GENERAL PA-46-350P, MALIBU 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY The following definitions are of symbols, abbreviations and terminology used throughout the handbook and those which may be of added operational significance to the pilot. The following definitions are of symbols, abbreviations and terminology used throughout the handbook and those which may be of added operational significance to the pilot.
PAGE 19
SECTION 1 GENERAL PA-46-350P, MALIBU 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) SECTION 1 GENERAL PA-46-350P, MALIBU 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) VLE Maximum Landing Gear Extended Speed is the maximum speed at which an aircraft can be safely flown with the landing gear extended. VLE Maximum Landing Gear Extended Speed is the maximum speed at which an aircraft can be safely flown with the landing gear extended.
PAGE 20
SECTION 1 GENERAL PA-46-350P, MALIBU 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) (b) Meteorological Terminology ISA SECTION 1 GENERAL PA-46-350P, MALIBU 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) (b) Meteorological Terminology International Standard Atmosphere in which: (1) The air is a dry perfect gas; (2) The temperature at sea level is 15° Celsius (59° Fahrenheit); (3) The pressure at sea level is 29.92 inches hg. (1013.
PAGE 21
SECTION 1 GENERAL PA-46-350P, MALIBU 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) (c) Power Terminology SECTION 1 GENERAL PA-46-350P, MALIBU 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) (c) Power Terminology Takeoff Power Maximum power permissible for takeoff. Takeoff Power Maximum power permissible for takeoff. Maximum Continuous Power Maximum power permissible continuously during flight. Maximum Continuous Power Maximum power permissible continuously during flight.
PAGE 22
SECTION 1 GENERAL PA-46-350P, MALIBU 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) (f) Weight and Balance Terminology SECTION 1 GENERAL PA-46-350P, MALIBU 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) (f) Weight and Balance Terminology Reference Datum An imaginary vertical plane from which all horizontal distances are measured for balance purposes. Reference Datum An imaginary vertical plane from which all horizontal distances are measured for balance purposes.
PAGE 23
SECTION 1 GENERAL PA-46-350P, MALIBU 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) SECTION 1 GENERAL PA-46-350P, MALIBU 1.21 SYMBOLS, ABBREVIATIONS AND TERMINOLOGY (Continued) Basic Empty Weight Standard empty weight plus optional equipment. Basic Empty Weight Standard empty weight plus optional equipment. Payload Weight of occupants, cargo and baggage. Payload Weight of occupants, cargo and baggage.
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SECTION 2 LIMITATIONS PA-46-350P, MALIBU SECTION 2 LIMITATIONS PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 2 SECTION 2 LIMITATIONS LIMITATIONS Paragraph No. Page No. Paragraph No. Page No. 2.1 General ..................................................................................... 2-1 2.1 General ..................................................................................... 2-1 2.3 Airspeed Limitations ......................................................
PAGE 25
SECTION 2 LIMITATIONS PA-46-350P, MALIBU 2.1 SECTION 2 LIMITATIONS PA-46-350P, MALIBU SECTION 2 SECTION 2 LIMITATIONS LIMITATIONS GENERAL 2.1 GENERAL This section provides the FAA Approved operating limitations, instrument markings, color coding and basic placards necessary for operation of the airplane and its systems. This section provides the FAA Approved operating limitations, instrument markings, color coding and basic placards necessary for operation of the airplane and its systems.
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SECTION 2 LIMITATIONS 2.3 PA-46-350P, MALIBU AIRSPEED LIMITATIONS (CONTINUED) SPEED KCAS 178 Maximum Flaps Extended Speed (VFE) Do not exceed this speed at the given flap setting. 10° 20° 36° 2.5 2.3 KIAS Maximum Speed for Pneumatic Boot Inflation. 165 130 116 SPEED KIAS KCAS 178 180 167 132 115 Maximum Flaps Extended Speed (VFE) Do not exceed this speed at the given flap setting.
PAGE 27
PA-46-350P, MALIBU 2.7 SECTION 2 LIMITATIONS POWER PLANT LIMITATIONS (a) (b) (c) (d) Number of Engines Engine Manufacturer Engine Model No.
PAGE 28
SECTION 2 LIMITATIONS 2.9 PA-46-350P, MALIBU LEANING LIMITATIONS SECTION 2 LIMITATIONS 2.9 Mixture full RICH at all engine powers above high speed cruise power. 2.
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SECTION 2 LIMITATIONS PA-46-350P, MALIBU 2.13 WEIGHT LIMITS (a) (b) (c) (d) (e) 2.
PAGE 30
SECTION 2 LIMITATIONS 2.21 PA-46-350P, MALIBU KINDS OF OPERATION EQUIPMENT LIST SECTION 2 LIMITATIONS 2.21 PA-46-350P, MALIBU KINDS OF OPERATION EQUIPMENT LIST This airplane may be operated in day or night VFR, day or night IFR and known icing when the appropriate equipment is installed and operable. This airplane may be operated in day or night VFR, day or night IFR and known icing when the appropriate equipment is installed and operable.
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SECTION 2 LIMITATIONS PA-46-350P, MALIBU 2.21 KINDS OF OPERATION EQUIPMENT LIST (Continued) System Number Required 2.21 KINDS OF OPERATION EQUIPMENT LIST (Continued) Types of Operation and Remarks (DAY, NIGHT, VFR, IFR and ICING Conditions) System Number Required Types of Operation and Remarks (DAY, NIGHT, VFR, IFR and ICING Conditions) 3. FLIGHT CONTROLS 3. FLIGHT CONTROLS Flap Position Indicator Elevator and Rudder Trim Position Indicator SECTION 2 LIMITATIONS PA-46-350P, MALIBU 1 1 ea.
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SECTION 2 LIMITATIONS 2.21 KINDS OF OPERATION EQUIPMENT LIST (CONTINUED) System 5. 6. PA-46-350P, MALIBU Number Required SECTION 2 LIMITATIONS 2.21 Types of Operation and Remarks (DAY, NIGHT, VFR, IFR and ICING Conditions) ICE PROTECTION (Continued) KINDS OF OPERATION EQUIPMENT LIST (CONTINUED) System 5.
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SECTION 2 LIMITATIONS PA-46-350P, MALIBU 2.21 KINDS OF OPERATION EQUIPMENT LIST (CONTINUED) System 7. 8. Number Required 2.21 Types of Operation and Remarks (DAY, NIGHT, VFR, IFR and ICING Conditions) INSTRUMENTATION - FLIGHT SECTION 2 LIMITATIONS PA-46-350P, MALIBU KINDS OF OPERATION EQUIPMENT LIST (CONTINUED) System 7.
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SECTION 2 LIMITATIONS 2.21 KINDS OF OPERATION EQUIPMENT LIST (CONTINUED) System 9. PA-46-350P, MALIBU Number Required SECTION 2 LIMITATIONS 2.21 Types of Operation and Remarks (DAY, NIGHT, VFR, IFR and ICING Conditions) LIGHTS EXTERNAL Position Lights a. Left Wing - Red and White 1 ea. b. Right Wing - Green and White KINDS OF OPERATION EQUIPMENT LIST (CONTINUED) System 9.
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SECTION 2 LIMITATIONS PA-46-350P, MALIBU 2.21 KINDS OF OPERATION EQUIPMENT LIST (CONTINUED) System Number Required Types of Operation and Remarks (DAY, NIGHT, VFR, IFR and ICING Conditions) 12. PRESSURIZED FLIGHT SECTION 2 LIMITATIONS PA-46-350P, MALIBU 2.21 KINDS OF OPERATION EQUIPMENT LIST (CONTINUED) System Number Required Types of Operation and Remarks (DAY, NIGHT, VFR, IFR and ICING Conditions) 12.
PAGE 36
SECTION 2 LIMITATIONS 2.23 PA-46-350P, MALIBU FUEL LIMITATIONS SECTION 2 LIMITATIONS 2.23 (a) Minimum Aviation Fuel Grade............................................ 100LL/100 (b) Total Capacity................................................................ 122 U.S. GAL. (c) Unusable Fuel.................................................................... 2 U.S. GAL. The unusable fuel for this airplane has been determined as 1.0 gallon in each wing in critical flight attitudes. (d) Usable Fuel.........
PAGE 37
SECTION 2 LIMITATIONS PA-46-350P, MALIBU 2.33 MAXIMUM SEATING CONFIGURATION 2.33 The maximum seating capacity is 6 (six) persons. SECTION 2 LIMITATIONS PA-46-350P, MALIBU MAXIMUM SEATING CONFIGURATION The maximum seating capacity is 6 (six) persons. 2.34 ICING INFORMATION 2.34 ICING INFORMATION "WARNING" "WARNING" Severe icing may result from environmental conditions outside of those for which the airplane is certified.
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SECTION 2 LIMITATIONS 2.35 PA-46-350P, MALIBU PLACARDS SECTION 2 LIMITATIONS 2.35 In full view of the pilot: PA-46-350P, MALIBU PLACARDS In full view of the pilot: The markings and placards installed in this airplane contain operating limitations which must be complied with when operating this airplane in the normal category. Other operating limitations which must be complied with when operating this airplane in this category are contained in the airplane flight manual.
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PA-46-350P, MALIBU 2.35 SECTION 2 LIMITATIONS PLACARDS (CONTINUED) PA-46-350P, MALIBU 2.35 Near the magnetic compass: SECTION 2 LIMITATIONS PLACARDS (CONTINUED) Near the magnetic compass: CAUTION - COMPASS CAL. MAY BE IN E R RO R W I T H E L E C T. E Q U I P M E N T OTHER THAN AVIONICS ON. CAUTION - COMPASS CAL. MAY BE IN E R RO R W I T H E L E C T. E Q U I P M E N T OTHER THAN AVIONICS ON.
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SECTION 2 LIMITATIONS 2.35 PA-46-350P, MALIBU SECTION 2 LIMITATIONS 2.
PAGE 41
SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 3 SECTION 3 EMERGENCY PROCEDURES EMERGENCY PROCEDURES Paragraph No. 3.1 3.3 3.3a 3.3b 3.3c 3.3d 3.3e 3.3f 3.3g 3.3h 3.3i 3.3j 3.3k 3.3l 3.3m 3.3n 3.3o 3.3p 3.3q 3.3r 3.3s 3.3t 3.3u 3.3v SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU Page No. General .................................................................................... Emergency Procedures Checklist ............................................
PAGE 42
SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES TABLE OF CONTENTS TABLE OF CONTENTS SECTION 3 (cont) SECTION 3 (cont) EMERGENCY PROCEDURES Paragraph No. 3.3w 3.3x 3.3y 3.3z 3.3aa 3.3ab 3.5 3.7 3.8 3.9 3.11 3.13 3.15 3.17 3.19 3.21 3.23 3.24 3.25 3.27 3.29 3.31 3.33 3.35 3.37 3.39 3.41 3.43 EMERGENCY PROCEDURES Page No. Hydraulic System Malfunction (3.49)...................................... Flap System Malfunction (3.51)...............................................
PAGE 43
SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 3 (cont) SECTION 3 (cont) EMERGENCY PROCEDURES EMERGENCY PROCEDURES Paragraph No. 3.45 3.49 3.51 3.53 3.55 3.57 3.59 SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU Page No. Inadvertent Icing Encounter (3.3v) ......................................... Hydraulic System Malfunction (3.3w) .................................... Flap System Malfunction (3.3x) ..............................................
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.1 SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 SECTION 3 EMERGENCY PROCEDURES EMERGENCY PROCEDURES GENERAL 3.1 GENERAL This section provides the recommended procedures for coping with various emergency or critical situations. All of the emergency procedures required by the FAA as well as those necessary for operation of the airplane, as determined by the operating and design features of the airplane, are presented.
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SECTION 3 EMERG PROCEDURES 3.3 PA-46-350P, MALIBU EMERGENCY PROCEDURES CHECKLIST SECTION 3 EMERG PROCEDURES 3.3 PA-46-350P, MALIBU EMERGENCY PROCEDURES CHECKLIST 3.3a ENGINE FIRE DURING START (3.7) 3.3a ENGINE FIRE DURING START (3.7) Starter (crank engine)..................................................................................PUSH Mixture .......................................................................................IDLE CUT-OFF Throttle ............................................
PAGE 46
PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES 3.3b TURBOCHARGER FAILURE (3.8) (Cont’d) 3.3b TURBOCHARGER FAILURE (3.8) (Cont’d) PARTIAL LOSS OF ENGINE POWER PARTIAL LOSS OF ENGINE POWER If the turbocharger wastegate fails in the OPEN position, a partial loss of engine power may result. The following procedure is recommended if a suspected turbocharger or turbocharger wastegate control failure results in a partial loss of engine power.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3c ENGINE POWER LOSS DURING TAKEOFF (3.9) (Cont’d) 3.3c ENGINE POWER LOSS DURING TAKEOFF (3.9) (Cont’d) If sufficient altitude has been gained to attempt a restart: If sufficient altitude has been gained to attempt a restart: Maintain Safe Airspeed Emergency (EMERG) Fuel Pump........................................................Check ON Fuel Selector .......................................................
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3d ENGINE POWER LOSS IN FLIGHT (3.11) (Cont’d) 3.3d ENGINE POWER LOSS IN FLIGHT (3.11) (Cont’d) If power is restored: If power is restored: Induction Air .......................................................................................PRIMARY (Remain in ALTERNATE if induction ice is suspected) Emergency (EMERG) Fuel Pump (Except in case of engine driven pump failure)...................................
PAGE 49
SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3e POWER OFF LANDING (3.13) (Continued) 3.3e POWER OFF LANDING (3.13) (Continued) When committed to landing: When committed to landing: Landing Gear Selector ................................................................AS REQUIRED Throttle ..................................................................................................CLOSED Mixture ......................................................
PAGE 50
SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3f FIRE IN FLIGHT (3.15) (Continued) SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3f FIRE IN FLIGHT (3.15) (Continued) CAUTION CAUTION The cabin pressure dump valve will remain open if the cabin pressure dump/normal switch is positioned to DUMP prior to turning the aircraft electrical system OFF. This provides maximum airflow through the cabin for smoke evacuation. Do not turn the cabin pressure dump/normal switch to NORM.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3h LOSS OF FUEL FLOW (3.19) (Continued) 3.3h LOSS OF FUEL FLOW (3.19) (Continued) Emergency (EMERG) Fuel Pump...................................................................ON Fuel Selector ...............................................................................CHECK on tank containing usable fuel Emergency (EMERG) Fuel Pump...................................................................
PAGE 52
PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES 3.3k TURBINE INLET TEMPERATURE (TIT) INDICATOR FAILURE (3.24) 3.3k TURBINE INLET TEMPERATURE (TIT) INDICATOR FAILURE (3.24) If failure occurs during takeoff, climb, or landing: If failure occurs during takeoff, climb, or landing: Mixture...................................................................................................Full Rich Mixture..........................................................
PAGE 53
SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3l HIGH CYLINDER HEAD TEMPERATURE (3.25) 3.3l HIGH CYLINDER HEAD TEMPERATURE (3.25) If indicated cylinder head temperature reaches 480°F: If indicated cylinder head temperature reaches 480°F: CHT Cycle Push Button ......................................................CYCLE THRU ALL CYLINDERS Power ....................................................................................................
PAGE 54
SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3m ELECTRICAL FAILURES (3.27) (Continued) 3.3m ELECTRICAL FAILURES (3.27) (Continued) Dual Alternator Failure (Zero amps both ammeters or ALTERNATOR #l and #2 INOP lights illuminated - annunciator panel). Dual Alternator Failure (Zero amps both ammeters or ALTERNATOR #l and #2 INOP lights illuminated - annunciator panel).
PAGE 55
SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3m ELECTRICAL FAILURES (3.27) (Continued) Supplemental Heater Control Circuit Failure (Heater Continues to Operate With AUX CBN HEAT and VENT/DEFOG switches OFF): VENT DEFOG Circuit Breaker ..................................................................PULL 3.3m ELECTRICAL FAILURES (3.
PAGE 56
SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES 3.3p SPIN RECOVERY (3.33) 3.3p SPIN RECOVERY (3.33) Rudder .................................................................................FULL OPPOSITE to DIRECTION of ROTATION Control Wheel...............................................................FULL FORWARD while NEUTRALIZING AILERONS Throttle ..................................................................................................
PAGE 57
SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3s PRESSURIZATION SYSTEM MALFUNCTION (3.39) 3.3s PRESSURIZATION SYSTEM MALFUNCTION (3.39) Should the differential pressure rise above 5.5 psi maximum or a structural failure appear imminent, proceed as follows: Should the differential pressure rise above 5.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3t CABIN AIR CONTAMINATION/SMOKE EVACUATION (3.41) (Pressurized) 3.3t CABIN AIR CONTAMINATION/SMOKE EVACUATION (3.41) (Pressurized) NOTE NOTE If pressurized, the following procedure will result in an immediate loss of pressurization and the cabin altitude will rise at an uncontrollable rate.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3u VACUUM SYSTEM FAILURE (3.43) 3.3u VACUUM SYSTEM FAILURE (3.43) Single Vacuum System Failure (Reduced suction pressure and left or right Vacuum Inoperative Annunciators illuminated. Single Vacuum System Failure (Reduced suction pressure and left or right Vacuum Inoperative Annunciators illuminated. Gyro Suction Gauge ...........................
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES 3.3v INADVERTENT ICING ENCOUNTER (3.45) (Continued) 3.3v INADVERTENT ICING ENCOUNTER (3.45) (Continued) Vent/Defog Fan................................................................................................ON Electric Windshield Heat .............................................................LOW or HIGH, as required Vent/Defog Fan.......................................................................
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3y FUEL TANK SUBMERGED PUMP FAILURE (BOOST PUMP light illuminated - annunciator panel) (3.53) 3.3y FUEL TANK SUBMERGED PUMP FAILURE (BOOST PUMP light illuminated - annunciator panel) (3.53) Fuel Selector ...........................................................................................CHECK Boost Pump Circuit Breaker ...................................................
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.3aa ANNUNCIATOR LIGHT PANEL FAILURE (ANNUNCIATOR INOP light illuminated - annunciator panel) (3.57) (Continued) 3.3aa ANNUNCIATOR LIGHT PANEL FAILURE (ANNUNCIATOR INOP light illuminated - annunciator panel) (3.57) (Continued) If annunciator lights illuminate, annunciator panel is functioning properly. ANNUNCIATOR INOP will remain lit.
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PA-46-350P, MALIBU 3.5 SECTION 3 EMERG PROCEDURES AMPLIFIED EMERGENCY PROCEDURES (GENERAL) PA-46-350P, MALIBU 3.5 SECTION 3 EMERG PROCEDURES AMPLIFIED EMERGENCY PROCEDURES (GENERAL) The following paragraphs are presented to supply additional information for the purpose of providing the pilot with a more complete understanding of the recommended course of action and probable cause of an emergency situation.
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SECTION 3 EMERG PROCEDURES 3.8 PA-46-350P, MALIBU TURBOCHARGER FAILURE (3.3b)(CONT’D) SECTION 3 EMERG PROCEDURES 3.8 PA-46-350P, MALIBU TURBOCHARGER FAILURE (3.3b)(CONT’D) COMPLETE LOSS OF ENGINE POWER: COMPLETE LOSS OF ENGINE POWER: If a suspected turbocharger or turbocharger control system failure results in a complete loss of engine power, the following procedure is recommended. Retard the mixture control to the IDLE CUTOFF position.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.9 ENGINE POWER LOSS DURING TAKEOFF (3.3c) PA-46-350P, MALIBU 3.9 SECTION 3 EMERG PROCEDURES ENGINE POWER LOSS DURING TAKEOFF (3.3c) The proper action to be taken if loss of power occurs during takeoff will depend on the circumstances of the particular situation. The proper action to be taken if loss of power occurs during takeoff will depend on the circumstances of the particular situation.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.11 ENGINE POWER LOSS IN FLIGHT (3.3d) 3.11 ENGINE POWER LOSS IN FLIGHT (3.3d) Complete engine power loss is usually caused by fuel flow interruption and power will be restored shortly after fuel flow is restored. The first step is to prepare for a power off landing (refer to paragraph 3.13). An airspeed of 90 KIAS (the power off glide speed) should be maintained.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.13 POWER OFF LANDING (3.3e) 3.13 POWER OFF LANDING (3.3e) If loss of power occurs at altitude, trim the aircraft for best gliding angle, (90 KIAS) and look for a suitable field. If measures taken to restore power are not effective, and if time permits, check your charts for airports in the immediate vicinity; it may be possible to land at one if you have sufficient altitude.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.15 FIRE IN FLIGHT (3.3f) The presence of fire is noted through smoke, smell, and heat in the cabin. It is essential that the source of the fire be promptly identified through instrument readings, character of smoke, or other indications since the action to be taken differs somewhat in each case. Check for the source of the fire first. SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.15 FIRE IN FLIGHT (3.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.15 FIRE IN FLIGHT (3.3f) (Continued) all cases, the heater and defroster should be OFF. If radio communication is not required turn the battery master and alternator switches OFF. If the terrain permits, a landing should be made immediately (refer to Power Off Landing procedure paragraph 3.13).
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.19 LOSS OF FUEL FLOW (3.3h) (Continued) If power is restored, turn OFF the emergency (EMERG) fuel pump (except in the case of an engine driven fuel pump failure). Adjust the mixture control as necessary. 3.19 LOSS OF FUEL FLOW (3.3h) (Continued) If power is restored, turn OFF the emergency (EMERG) fuel pump (except in the case of an engine driven fuel pump failure). Adjust the mixture control as necessary.
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PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES 3.24 TURBINE INLET TEMP (TIT) INDICATOR FAILURE (3.3k) (CONT’D) 3.24 TURBINE INLET TEMP (TIT) INDICATOR FAILURE (3.3k) (CONT’D) If TIT failure occurs prior to setting cruise power, set power per the POH Section 5 power setting table and then lean to the approximate POH power setting table fuel flow +4 GPH. This fuel flow will maintain adequate engine cooling and a TIT value below TIT limits.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.27 ELECTRICAL FAILURES (3.3m) SINGLE ALTERNATOR FAILURE (Zero amps or ALTERNATOR #1 or #2 INOP light illuminated - annunciator panel) 3.27 ELECTRICAL FAILURES (3.3m) SINGLE ALTERNATOR FAILURE (Zero amps or ALTERNATOR #1 or #2 INOP light illuminated - annunciator panel) NOTE NOTE Anytime total tie bus voltage is below 25 Vdc, the LOW BUS VOLTAGE annunciator will illuminate.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.27 ELECTRICAL FAILURES (3.3m) (Continued) DUAL ALTERNATOR FAILURE (Zero amps both ammeters or ALTERNATOR #1 and #2 INOP light illuminated - annunciator panel) 3.27 ELECTRICAL FAILURES (3.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.27 ELECTRICAL FAILURES (3.3m) (Continued) 3.27 ELECTRICAL FAILURES (3.3m) (Continued) SUPPLEMENTAL HEATER CONTROL CIRCUIT FAILURE (Heater Continues to Operate With AUX CBN HEAT and VENT/DEFOG Switches OFF) SUPPLEMENTAL HEATER CONTROL CIRCUIT FAILURE (Heater Continues to Operate With AUX CBN HEAT and VENT/DEFOG Switches OFF) Pull the VENT DEFOG circuit breaker.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.35 ENGINE ROUGHNESS (3.3q) 3.35 ENGINE ROUGHNESS (3.3q) Engine roughness may be caused by dirt in the injector nozzles, induction filter icing, ignition problems, or other causes. Engine roughness may be caused by dirt in the injector nozzles, induction filter icing, ignition problems, or other causes. First adjust the mixture for maximum smoothness.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.39 PRESSURIZATION SYSTEM MALFUNCTION (3.3s) SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.39 PRESSURIZATION SYSTEM MALFUNCTION (3.3s) NOTE If pressurized, the following procedure will result in an immediate loss of pressurization and the cabin altitude will rise at an uncontrollable rate. NOTE If pressurized, the following procedure will result in an immediate loss of pressurization and the cabin altitude will rise at an uncontrollable rate.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES 3.43 VACUUM SYSTEM FAILURE (3.3u) 3.43 VACUUM SYSTEM FAILURE (3.3u) A failure of either vacuum pump is indicated by the illumination of a vacuum failure annunciator, “VACUUM NO. 1 INOP”.or “VACUUM NO. 2 INOP. A failure of either vacuum pump is indicated by the illumination of a vacuum failure annunciator, “VACUUM NO. 1 INOP”.or “VACUUM NO. 2 INOP.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.49 HYDRAULIC SYSTEM MALFUNCTION (3.3w) 3.49 HYDRAULIC SYSTEM MALFUNCTION (3.3w) A hydraulic system malfunction, which causes the hydraulic pump to either run continuously (more than 15-20 seconds), or cycle on and off rapidly (more than 6-8 times), may be detected by the illumination of the HYDRAULIC PUMP amber annunciator light. Pull the HYDRAULIC PUMP POWER circuit breaker to stop operation.
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PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES 3.53 FUEL TANK SUBMERGED PUMP FAILURE (BOOST PUMP light illuminated - annunciator panel) (3.3y) Illumination of the BOOST PUMP annunciator light indicates the selected fuel tank’s submerged fuel boost pump has failed.
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SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU SECTION 3 EMERG PROCEDURES PA-46-350P, MALIBU 3.59 EMERGENCY EXIT (3.3ab) The second window aft of the windshield on the right side of the fuselage is an emergency exit. 3.59 EMERGENCY EXIT (3.3ab) The second window aft of the windshield on the right side of the fuselage is an emergency exit. NOTE NOTE The cabin must be depressurized before attempting to open the emergency exit.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 4 SECTION 4 NORMAL PROCEDURES NORMAL PROCEDURES Paragraph No. Page No. Paragraph No. Page No. 4.1 GENERAL .............................................................................. 4-1 4.1 GENERAL .............................................................................. 4-1 4.3 AIRSPEEDS FOR SAFE OPERATION..................................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5j 4.5k 4.5m 4.5n 4.5o 4.5p 4.5q 4.7 4.9 4.9a 4.9b 4.9c 4.9d 4.9e 4.9f TABLE OF CONTENTS SECTION 4 (cont) SECTION 4 (cont) NORMAL PROCEDURES NORMAL PROCEDURES Page No. Climb Checklist (4.25) ............................................................ MAXIMUM CONTINUOUS POWER CLIMB (4.25a) .................................................................... CRUISE CLIMB (4.25b).....................................................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 4 (cont) SECTION 4 (cont) NORMAL PROCEDURES NORMAL PROCEDURES Paragraph No. Page No. Paragraph No. Page No. 4.11 4.13 4.13a 4.13b 4.13c 4.13d 4.13e 4.15 4.17 4.19 4.21 4.23 4.23a 4.23b 4.23c 4.25 4.25a 4.25b 4.27 4.29 4.31 4.31a 4.31b 4-22 4-23 4-23 4-24 4-24 4-24 4-25 4-26 4-26 4-27 4-28 4-28 4-29 4-29 4-29 4-30 4-30 4-30 4-30 4-33 4-33 4-34 4-34 4.11 4.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 4 (cont) SECTION 4 (cont) NORMAL PROCEDURES NORMAL PROCEDURES Paragraph No. Page No. Paragraph No. Page No. 4.33 4.35 4.37 GO-AROUND (4.5n) .............................................................. AFTER LANDING (4.5o) ...................................................... STOPPING ENGINE (4.5p) ...................................................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 SECTION 4 NORMAL PROCEDURES NORMAL PROCEDURES 4.1 GENERAL 4.1 GENERAL This section provides the normal operating procedures for the PA-46350P, Malibu airplane.
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SECTION 4 NORMAL PROCEDURES 4.3 PA-46-350P, MALIBU AIRSPEEDS FOR SAFE OPERATIONS SECTION 4 NORMAL PROCEDURES 4.3 PA-46-350P, MALIBU AIRSPEEDS FOR SAFE OPERATIONS The following airspeeds are those which are significant to the safe operation of the airplane. These figures are for standard airplanes flown at gross weight under standard conditions at sea level. The following airspeeds are those which are significant to the safe operation of the airplane.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU Y L N WALK-AROUND Figure 4-1 4.5 NORMAL PROCEDURES CHECKLIST 4.5a Preflight Checklists (4.9) COCKPIT (4.9a) Control wheel ......................................................................release restraints Parking Brake .........................................................................................SET Gear Handle..................................................................................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5a Preflight Checklist (Continued) 4.5a Preflight Checklist (Continued) COCKPIT (4.9a) (Continued) COCKPIT (4.9a) (Continued) Annunciator Panel ...........................................................................CHECK Switch Panel ....................................................................................CHECK FUEL PRESS Annunciator .........................................................
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PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.5a Preflight Checklist (4.9) (Continued) 4.5a Preflight Checklist (4.9) (Continued) RIGHT WING (4.9C) (CONTINUED) RIGHT WING (4.9C) (CONTINUED) Fuel Tank Vent .................................................................................CLEAR Tie Down and Chock ....................................................................REMOVE Main Gear Strut ....................................................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5a Preflight Checklist (4.9) (Continued) LEFT WING (4.9) SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5a Preflight Checklist (4.9) (Continued) LEFT WING (4.9) Surface Condition......................................CLEAR of ICE, FROST, SNOW Surface Condition......................................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5a Preflight Checklist (4.9) (Continued) SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5a Preflight Checklist (4.9) (Continued) MISCELLANEOUS (4.9f) (Continued) MISCELLANEOUS (4.9f) (Continued) Exterior Lighting Switches ................................................ON and CHECK Pitot ..................................................................................CHECK - WARM Stall Warning Heat ....................................................
PAGE 92
SECTION 4 NORMAL PROCEDURES 4.5c PA-46-350P, MALIBU Engine Start Checklist (4.13) SECTION 4 NORMAL PROCEDURES 4.5c PA-46-350P, MALIBU Engine Start Checklist (4.13) ENGINE START - GENERAL (4.13a) ENGINE START - GENERAL (4.13a) CAUTION CAUTION Do not attempt flight if there is no indication of alternator output. Do not attempt flight if there is no indication of alternator output. CAUTION CAUTION The STARTER ENGAGE annunciator will illuminate during engine cranking.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5c Engine Start Checklist (4.13) (Continued) SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5c Engine Start Checklist (4.13) (Continued) NORMAL START - COLD ENGINE (4.13b) (Continued) NORMAL START - COLD ENGINE (4.13b) (Continued) NOTE NOTE The amount of prime depends on engine temperature. Familiarity and practice will enable the operator to estimate the amount of prime required. The amount of prime depends on engine temperature.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5c Engine Start Checklist (4.13) (Continued) SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5c Engine Start Checklist (4.13) (Continued) ENGINE START WITH EXTERNAL POWER SOURCE (4.13e) ENGINE START WITH EXTERNAL POWER SOURCE (4.13e) Battery Master Switch ............................................................................OFF Alternators ..............................................................................................
PAGE 95
PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES SECTION 4 NORMAL PROCEDURES 4.5d Before Taxiing Checklist (4.15) 4.5d Before Taxiing Checklist (4.15) BEFORE TAXIING (4.15) BEFORE TAXIING (4.15) CAUTION Do not operate engine above 1200 RPM with cabin doors open. Throttle ............................................................................1000 to 1200 RPM Radio Master Switch ................................................................................ON Environmental System ...................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5f Ground Check Checklist (4.19) (Continued) GROUND CHECK (4.19) (Continued) PA-46-350P, MALIBU 4.5f Ground Check Checklist (4.19) (Continued) GROUND CHECK (4.19) (Continued) NOTE Refer to paragraph 4.50, Icing Information, prior to any flight operations. (Takeoff, cruise, landing, etc.) If flight into icing conditions (in visible moisture below +5°C) is anticipated, conduct a preflight check of the ice protection systems per Supplement No.
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PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.5g Before Takeoff Checklist (4.21) (Continued) PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.5g Before Takeoff Checklist (4.21) (Continued) BEFORE TAKEOFF (4.21) (Continued) Seat Backs .........................................................................................ERECT Seats ..............................................ADJUSTED& LOCKED IN POSITION Armrests ....................................................................................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5h Takeoff Checklist (4.23) (Continued) SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5h Takeoff Checklist (4.23) (Continued) 0° FLAP TAKEOFF PERFORMANCE (4.23b) Flaps ......................................................................................................0° Trim....................................................................................................SET Brakes ..................................................................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5i Climb Checklist (Continued) SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5i Climb Checklist (Continued) CRUISE CLIMB (4.25b) CRUISE CLIMB (4.25b) Manifold Pressure ....................................................................35 IN. HG Propeller Speed........................................................................2500 RPM Mixture.........................................................................................
PAGE 100
SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5k Descent Checklist (4.29) (Continued) REDUCED POWER DESCENT (4.29) SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5k Descent Checklist (4.29) (Continued) REDUCED POWER DESCENT (4.29) Throttle..................................................................AT or ABOVE 20 in. Hg. Mixture.......................................................................MAINTAIN 1350 TIT Propeller Speed .............................................................
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PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.5m Approach And Landing Checklist (4.31) (Continued) SHORT FIELD TECHNIQUE (4.31b) 4.5m Approach And Landing Checklist (4.31) (Continued) SHORT FIELD TECHNIQUE (4.31b) Flaps........................................................................................FULL DOWN Airspeed...........................................................................................78 KIAS Throttle .......................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5p Stopping Engine Checklist (4.37) SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.5p Stopping Engine Checklist (4.37) STOPPING ENGINE (4.37) STOPPING ENGINE (4.37) Radios and Electrical Equipment ..........................................................OFF External Lights ......................................................................................OFF Air Conditioner ........................................................................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.7 AMPLIFIED NORMAL PROCEDURES (GENERAL) 4.7 AMPLIFIED NORMAL PROCEDURES (GENERAL) The following paragraphs are provided to supply detailed information and the explanation of the normal procedures for operation of the airplane. The following paragraphs are provided to supply detailed information and the explanation of the normal procedures for operation of the airplane. 4.9 PREFLIGHT CHECK (4.5a) 4.
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SECTION 4 NORMAL PROCEDURES 4.9 PA-46-350P, MALIBU PREFLIGHT CHECK (4.5a) (Continued) SECTION 4 NORMAL PROCEDURES 4.9 PA-46-350P, MALIBU PREFLIGHT CHECK (4.5a) (Continued) 4.9b Empennage (4.5a) 4.9b Empennage (4.5a) Begin the walk-around at the left side of the aft fuselage. Check the condition of any antennas located on the fuselage. All surfaces of the empennage must be clear of ice, frost, snow or other extraneous substances. Fairings and access covers should be attached properly.
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PA-46-350P, MALIBU 4.9 SECTION 4 NORMAL PROCEDURES PREFLIGHT CHECK (4.5a) (Continued) PA-46-350P, MALIBU 4.9 SECTION 4 NORMAL PROCEDURES PREFLIGHT CHECK (4.5a) (Continued) 4.9d Nose Section (4.5a) 4.9d Nose Section (4.5a) Check the general condition of the nose section; look for oil or fluid leakage and that the cowling is secure. Drain the fuel filter sump located on the lower fuselage aft of the cowling. Check the windshield and clean if necessary.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.9 PREFLIGHT CHECK (4.5a) (Continued) 4.9 PREFLIGHT CHECK (4.5a) (Continued) 4.9f Miscellaneous (4.5a) 4.9f Miscellaneous (4.5a) Enter the cockpit and, if installed, check oxygen masks and hoses. Enter the cockpit and, if installed, check oxygen masks and hoses. Turn the battery master switch ON and retract the flaps. Check the interior lights by turning ON the necessary switches.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.11 BEFORE STARTING ENGINE (4.5b) (Continued) If the flight is to be made unpressurized, the cabin pressurization control should be pulled out to dump bleed air overboard and the cabin pressure dump/normal switch should be in the DUMP position in order to provide maximum cabin airflow.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.13 ENGINE START (4.5c) (Continued) 4.13 ENGINE START (4.5c) (Continued) 4.13bNormal Start - Cold Engine (4.5c) 4.13bNormal Start - Cold Engine (4.5c) Open the throttle lever approximately 1/2 inch. Turn the battery master switch ON, and check that the emergency (EMERG) fuel pump is OFF. Move the mixture control to full RICH for approximately four seconds then to idle cut-off. The engine is now primed.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.13 ENGINE START (4.5c) (Continued) 4.13 ENGINE START (4.5c) (Continued) 4.13e Engine Start With External Power Source (4.5c) 4.13e Engine Start With External Power Source (4.5c) An optional feature allows the operator to use an external power source to crank the engine without having to gain access to the airplane’s battery.
PAGE 110
SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.15 BEFORE TAXIING (4.5d) SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.15 BEFORE TAXIING (4.5d) CAUTION CAUTION Do not operate engine above 1200 rpm with cabin doors open. Do not operate engine above 1200 rpm with cabin doors open. Warm up the engine at 1000 to 1200 rpm. Avoid prolonged idling at low rpm, as this practice may result in fouled spark plugs. Turn the radio master switch ON, and set environmental system as desired.
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PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.19 GROUND CHECK (4.5f) PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.19 GROUND CHECK (4.5f) CAUTION Alternate air is unfiltered. Use of alternate air during ground or flight operations when dust or other contaminants are present may result in damage from particle ingestion. CAUTION Alternate air is unfiltered.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.21 BEFORE TAKEOFF (4.5g) 4.21 BEFORE TAKEOFF (4.5g) Ensure that the battery master, emergency fuel pump, and alternator switches are all ON. Check all of the flight instruments and set as required. Check all engine gauges to verify the engine indications are with the normal operating range. Check that the cabin pressurization controls are properly set.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.23 TAKEOFF (4.5h) (Continued) 4.23 TAKEOFF (4.5h) (Continued) 4.23a Normal Technique (4.5h) 4.23a Normal Technique (4.5h) When the available runway length is well in excess of that required and obstacle clearance is no factor, the normal takeoff technique may be used. The flaps should be in the 0° to 10° position and the pitch trim set slightly aft of neutral.
PAGE 114
SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.25 CLIMB (4.5i) 4.25 CLIMB (4.5i) 4.25a Maximum Continuous Power Climb (4.5i) 4.25a Maximum Continuous Power Climb (4.5i) The best rate of climb at gross weight and maximum continuous power will be obtained at 110 KIAS. The best angle of climb may be obtained at 81 KIAS. The recommended procedure for climb is to use maximum continuous power with the mixture full RICH.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.27 CRUISE (4.5J) (CONTINUED) 4.27 CRUISE (4.5J) (CONTINUED) The cruising speed is determined by many factors, including power setting, altitude, temperature, loading, and equipment installed on the airplane. When leveling off at cruise altitude, the pilot may reduce to a cruise power setting in accordance with the *Power Setting Table in Section 5 of this manual.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.27 CRUISE (4.5j) (Continued) 4.27 CRUISE (4.5j) (Continued) During cruise, use the following procedure to maintain lateral balance, and stay within the fuel imbalance limitations of 2.23: During cruise, use the following procedure to maintain lateral balance, and stay within the fuel imbalance limitations of 2.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.29 DESCENT (4.5k) 4.29 DESCENT (4.5k) The recommended procedure for descent is to leave the engine controls at the cruise settings and increase the airspeed to give the desired rate of descent. Monitor the manifold pressure and adjust to maintain the cruise setting. Leave the mixture leaned to the cruise setting. This will prevent rapid engine cooling which may damage the engine.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.31 APPROACH AND LANDING (4.5m) (Continued) SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.31 APPROACH AND LANDING (4.5m) (Continued) NOTE NOTE During landing gear operation, it is normal for the HYDRAULIC PUMP annunciator light to illuminate until full system pressure is restored. During landing gear operation, it is normal for the HYDRAULIC PUMP annunciator light to illuminate until full system pressure is restored.
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PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.33 GO-AROUND (4.5n) 4.33 GO-AROUND (4.5n) To initiate a go-around from a landing approach, the mixture should be set to full RICH, the propeller control should be at full INCREASE, and the throttle should be advanced to full power while the pitch attitude is increased to obtain the balked landing climb speed of 80 KIAS.
PAGE 120
SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.39 MOORING (4.5q) 4.39 MOORING (4.5q) If necessary, the airplane should be moved on the ground with the aid of the nose wheel tow bar. If necessary, the airplane should be moved on the ground with the aid of the nose wheel tow bar. The parking brake should be set and the aileron and elevator controls should be secured by looping the safety belt through the control wheel and pulling it snug.
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PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.45 CABIN PRESSURIZATION SYSTEM 4.45 CABIN PRESSURIZATION SYSTEM Cabin pressurization system controls, gauges and switches are located to the right of the pilots control wheel shaft. (Refer to Section 7, Figure 7-39.) Cabin pressurization system controls, gauges and switches are located to the right of the pilots control wheel shaft. (Refer to Section 7, Figure 7-39.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.45 CABIN PRESSURIZATION SYSTEM (Continued) 4.45 CABIN PRESSURIZATION SYSTEM (Continued) For flight below an airplane altitude of 12,500 feet, the cabin altitude control should be left at the takeoff setting.
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.47 SUPPLEMENTAL ELECTRIC HEATER 4.47 SUPPLEMENTAL ELECTRIC HEATER AFTER ENGINE START AFTER ENGINE START BATT MASTER Switch .................................................................................ON Alternator Switches ......................................................................................OFF VENT DEFOG Switch .........................................................................
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SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES PA-46-350P, MALIBU 4.49 NOISE LEVEL 4.49 NOISE LEVEL The corrected noise level of this aircraft with a two blade propeller is 74.7 dB(A). as measured per FAR 36 Appendix F. For the three blade propeller, the corrected noise level of this aircraft is 79.7 dB(A) as measured per FAR 36 Appendix G. The corrected noise level of this aircraft with a two blade propeller is 74.7 dB(A). as measured per FAR 36 Appendix F.
PAGE 125
PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.50 ICING INFORMATION PA-46-350P, MALIBU SECTION 4 NORMAL PROCEDURES 4.50 ICING INFORMATION "THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN-FLIGHT ICING" "THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN-FLIGHT ICING" Visible rain at temperatures below 0 degrees Celsius ambient air temperature. Visible rain at temperatures below 0 degrees Celsius ambient air temperature.
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SECTION 5 PERFORMANCE PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 5 SECTION 5 PERFORMANCE PERFORMANCE Paragraph No. 5.1 5.2 5.3 5.5 5.7 SECTION 5 PERFORMANCE PA-46-350P, MALIBU Page No. General ..................................................................................... Aircraft Configuration.............................................................. Introduction - Performance and Flight Planning...................... Flight Planning Example .......................
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SECTION 5 PERFORMANCE PA-46-350P, MALIBU 5.1 SECTION 5 PERFORMANCE PA-46-350P, MALIBU SECTION 5 SECTION 5 PERFORMANCE PERFORMANCE GENERAL 5.1 GENERAL All of the required (FAA regulations) and complementary performance information is provided by this section. All of the required (FAA regulations) and complementary performance information is provided by this section.
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SECTION 5 PERFORMANCE 5.3 PA-46-350P, MALIBU INTRODUCTION - PERFORMANCE AND FLIGHT PLANNING (CONT.) SECTION 5 PERFORMANCE 5.3 PA-46-350P, MALIBU INTRODUCTION - PERFORMANCE AND FLIGHT PLANNING (CONT.) The information provided by paragraph 5.5 (Flight Planning Example) outlines a detailed flight plan using performance charts in this section. Each chart includes its own example to show how it is used. The information provided by paragraph 5.
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PA-46-350P, MALIBU 5.5 SECTION 5 PERFORMANCE FLIGHT PLANNING EXAMPLE PA-46-350P, MALIBU 5.5 (a) Aircraft Loading SECTION 5 PERFORMANCE FLIGHT PLANNING EXAMPLE (a) Aircraft Loading The first step in planning the flight is to calculate the airplane weight and center of gravity by utilizing the information provided by Section 6 (Weight and Balance) of this handbook.
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SECTION 5 PERFORMANCE 5.5 PA-46-350P, MALIBU FLIGHT PLANNING EXAMPLE (CONT) SECTION 5 PERFORMANCE 5.5 (b) Takeoff and Landing PA-46-350P, MALIBU FLIGHT PLANNING EXAMPLE (CONT) (b) Takeoff and Landing Now that the aircraft loading has been determined, all aspects of the takeoff and landing must be considered. Now that the aircraft loading has been determined, all aspects of the takeoff and landing must be considered.
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SECTION 5 PERFORMANCE PA-46-350P, MALIBU 5.5 FLIGHT PLANNING EXAMPLE (CONT) SECTION 5 PERFORMANCE PA-46-350P, MALIBU 5.5 FLIGHT PLANNING EXAMPLE (CONT) NOTE NOTE The remainder of the performance charts used in this flight plan example assume a no wind condition. The effect of winds aloft must be considered by the pilot when computing climb, cruise and descent performance. The remainder of the performance charts used in this flight plan example assume a no wind condition.
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SECTION 5 PERFORMANCE 5.5 PA-46-350P, MALIBU FLIGHT PLANNING EXAMPLE (cont) (d) Descent SECTION 5 PERFORMANCE 5.5 PA-46-350P, MALIBU FLIGHT PLANNING EXAMPLE (cont) (d) Descent The descent data will be determined prior to the cruise data to provide the descent distance for establishing the total cruise distance. The descent data will be determined prior to the cruise data to provide the descent distance for establishing the total cruise distance.
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PA-46-350P, MALIBU 5.5 SECTION 5 PERFORMANCE FLIGHT PLANNING EXAMPLE (cont) SECTION 5 PERFORMANCE PA-46-350P, MALIBU 5.5 FLIGHT PLANNING EXAMPLE (cont) Calculate the cruise fuel consumption for the cruise power setting from the information provided by the Textron Lycoming Manual and the Cruise Performance Table (refer to page 5-26).
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SECTION 5 PERFORMANCE PA-46-350P, MALIBU 5.5 FLIGHT PLANNING EXAMPLE (cont) SECTION 5 PERFORMANCE PA-46-350P, MALIBU 5.5 FLIGHT PLANNING EXAMPLE (cont) The flight time required for the flight planning example is shown below: The flight time required for the flight planning example is shown below: (1) Total Flight Time (c)(4) plus (d)(2) plus (e)(6), (0.235 hrs plus 0.395 hrs plus 1.33 hrs) (14.1 min. plus 23.7 min. plus 79.6 min.) 1.96 hrs/117.4 min.
PAGE 135
SECTION 5 PERFORMANCE PA-46-350P, MALIBU 5.7 5.7 PERFORMANCE GRAPHS PERFORMANCE GRAPHS LIST OF FIGURES LIST OF FIGURES Figure No. 5-1 5-3 5-5 5-7 5-9 5-11 5-13 5-15 5-17 5-19 5-21 5-23 5-24 5-25 5-26 5-27 5-29 5-31 5-33 5-35 5-37 5-39 5-41 Page No. Airspeed Calibration ................................................................ Angle of Bank Vs. Stall Speed................................................. Temperature Conversion ..........................................................
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PA-46-350P, MALIBU AIRSPEED CALIBRATION Figure 5-1 ISSUED: FEBRUARY 23, 1999 SECTION 5 PERFORMANCE REPORT: VB-1710 5-11 PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-11 Y NL O CE EN T ER IGH EF FL R R OR FO T F NO AIRSPEED CALIBRATION Figure 5-1 ISSUED: FEBRUARY 23, 1999
PAGE 137
SECTION 5 PERFORMANCE PA-46-350P, MALIBU ISSUED: FEBRUARY 23, 1999 ANGLE OF BANK VS. STALL SPEED Figure 5-3 REPORT: VB-1710 5-12 SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y NL O CE EN T ER IGH EF FL R R OR FO T F NO ISSUED: FEBRUARY 23, 1999 ANGLE OF BANK VS.
PAGE 138
PA-46-350P, MALIBU SECTION 5 PERFORMANCE SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y L N O E C N E HT R E LIG F E F R R R O FO T F NO TEMPERATURE CONVERSION Figure 5-5 ISSUED: FEBRUARY 23, 1999 TEMPERATURE CONVERSION Figure 5-5 REPORT: VB-1710 5-13 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 5-13
PAGE 139
SECTION 5 PERFORMANCE PA-46-350P, MALIBU SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y L N O E C N E HT R E LIG F E F R R R O FO T F NO PRESSURE ALTITUDE VS OUTSIDE AIR TEMPERATURE Figure 5-7 REPORT: VB-1710 5-14 ISSUED: FEBRUARY 23, 1999 PRESSURE ALTITUDE VS OUTSIDE AIR TEMPERATURE Figure 5-7 REPORT: VB-1710 5-14 ISSUED: FEBRUARY 23, 1999
PAGE 140
PA-46-350P, MALIBU TEMPERATURE RISE DUE TO RAM RECOVERY Figure 5-9 ISSUED: FEBRUARY 23, 1999 SECTION 5 PERFORMANCE REPORT: VB-1710 5-15 PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-15 Y NL O CE EN T ER IGH EF FL R R OR FO T F NO TEMPERATURE RISE DUE TO RAM RECOVERY Figure 5-9 ISSUED: FEBRUARY 23, 1999
PAGE 141
SECTION 5 PERFORMANCE PA-46-350P, MALIBU SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y L N O E C N E HT R E LIG F E F R R R O FO T F NO WIND COMPONENTS Figure 5-11 REPORT: VB-1710 5-16 ISSUED: FEBRUARY 23, 1999 WIND COMPONENTS Figure 5-11 REPORT: VB-1710 5-16 ISSUED: FEBRUARY 23, 1999
PAGE 142
PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-17 TAKEOFF GROUND ROLL, 0° FLAPS Figure 5-13 ISSUED: FEBRUARY 23, 1999 PA-46-350P, MALIBU SECTION 5 PERFORMANCE Y NL O CE EN T ER IGH EF FL R R OR FO T F NO REPORT: VB-1710 5-17 TAKEOFF GROUND ROLL, 0° FLAPS Figure 5-13 ISSUED: FEBRUARY 23, 1999
PAGE 143
SECTION 5 PERFORMANCE PA-46-350P, MALIBU ISSUED: FEBRUARY 23, 1999 TAKEOFF GROUND ROLL, 20° FLAPS Figure 5-15 REPORT: VB-1710 5-18 SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y NL O CE EN T ER IGH EF FL R R OR FO T F NO ISSUED: FEBRUARY 23, 1999 TAKEOFF GROUND ROLL, 20° FLAPS Figure 5-15 REPORT: VB-1710 5-18
PAGE 144
PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-19 TAKEOFF DISTANCE OVER 50 FT. OBSTACLE, 0° FLAPS Figure 5-17 ISSUED: FEBRUARY 23, 1999 PA-46-350P, MALIBU SECTION 5 PERFORMANCE Y NL O CE EN T ER IGH EF FL R R OR FO T F NO REPORT: VB-1710 5-19 TAKEOFF DISTANCE OVER 50 FT.
PAGE 145
SECTION 5 PERFORMANCE PA-46-350P, MALIBU ISSUED: FEBRUARY 23, 1999 TAKEOFF DISTANCE OVER 50 FT. OBSTACLE, 20° FLAPS Figure 5-19 REPORT: VB-1710 5-20 SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y NL O CE EN T ER IGH EF FL R R OR FO T F NO ISSUED: FEBRUARY 23, 1999 TAKEOFF DISTANCE OVER 50 FT.
PAGE 146
PA-46-350P, MALIBU RATE OF CLIMB Figure 5-21 ISSUED: FEBRUARY 23, 1999 SECTION 5 PERFORMANCE REPORT: VB-1710 5-21 PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-21 Y NL O CE EN T ER IGH EF FL R R OR FO T F NO RATE OF CLIMB Figure 5-21 ISSUED: FEBRUARY 23, 1999
PAGE 147
SECTION 5 PERFORMANCE PA-46-350P, MALIBU ISSUED: FEBRUARY 23, 1999 REVISED: SEPTEMBER 20, 1999 MAXIMUM CONTINUOUS POWER TIME, FUEL, AND DISTANCE TO CLIMB (110 KIAS) Figure 5-23 REPORT: VB-1710 5-22 SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y NL O CE EN T ER IGH EF FL R R OR FO T F NO ISSUED: FEBRUARY 23, 1999 REVISED: SEPTEMBER 20, 1999 MAXIMUM CONTINUOUS POWER TIME, FUEL, AND DISTANCE TO CLIMB (110 KIAS) Figure 5-23 REPORT: VB-1710 5-22
PAGE 148
PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-23 MAXIMUM CONTINUOUS POWER TIME, FUEL, AND DISTANCE TO CLIMB (125 KIAS) Figure 5-24 ISSUED: FEBRUARY 23, 1999 REVISED: SEPTEMBER 20, 1999 PA-46-350P, MALIBU SECTION 5 PERFORMANCE Y NL O CE EN T ER IGH EF FL R R OR FO T F NO REPORT: VB-1710 5-23 MAXIMUM CONTINUOUS POWER TIME, FUEL, AND DISTANCE TO CLIMB (125 KIAS) Figure 5-24 ISSUED: FEBRUARY 23, 1999 REVISED: SEPTEMBER 20, 1999
PAGE 149
SECTION 5 PERFORMANCE PA-46-350P, MALIBU ISSUED: FEBRUARY 23, 1999 REVISED: SEPTEMBER 20, 1999 CRUISE CLIMB TIME, FUEL, AND DISTANCE TO CLIMB Figure 5-25 REPORT: VB-1710 5-24 SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y NL O CE EN T ER IGH EF FL R R OR FO T F NO ISSUED: FEBRUARY 23, 1999 REVISED: SEPTEMBER 20, 1999 CRUISE CLIMB TIME, FUEL, AND DISTANCE TO CLIMB Figure 5-25 REPORT: VB-1710 5-24
PAGE 150
PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-25 MAXIMUM MANIFOLD PRESSURE Vs. PRESSURE ALTITUDE Figure 5-26 ISSUED: FEBRUARY 23, 1999 PA-46-350P, MALIBU SECTION 5 PERFORMANCE Y NL O CE EN T ER IGH EF FL R R OR FO T F NO REPORT: VB-1710 5-25 MAXIMUM MANIFOLD PRESSURE Vs.
PAGE 151
SECTION 5 PERFORMANCE PA-46-350P, MALIBU SECTION 5 PERFORMANCE POWER SETTING TABLE REFERENCE FIG. 5-27 POWER SETTING TABLE REFERENCE FIG. 5-27 ASSOCIATED CONDITIONS ASSOCIATED CONDITIONS RPM Man. Press. Approx. Fuel Flow @ 20,000 ft TIT High Speed Cruise 2500 32" Hg 20 GPH Lean to Peak Normal Cruise 2500 2400 29” Hg 30" Hg 18 GPH Economy Cruise 2400 2200 25" Hg 26" Hg Long Range Cruise 2200 20" Hg RPM Man. Press. Approx.
PAGE 152
PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-27 CRUISE SPEED VS. ALTITUDE Figure 5-27 ISSUED: FEBRUARY 23, 1999 PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-27 Y NL O CE EN T ER IGH EF FL R R OR FO T F NO CRUISE SPEED VS.
PAGE 153
SECTION 5 PERFORMANCE REPORT: VB-1710 5-28 ISA RANGE Figure 5-29 PA-46-350P, MALIBU ISSUED: FEBRUARY 23, 1999 REVISED: SEPTEMBER 20, 1999 SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y NL ISSUED: FEBRUARY 23, 1999 REVISED: SEPTEMBER 20, 1999 ISA RANGE Figure 5-29 O CE EN T ER IGH EF FL R R OR FO T F NO REPORT: VB-1710 5-28
PAGE 154
PA-46-350P, MALIBU ISA ENDURANCE Figure 5-31 ISSUED: FEBRUARY 23, 1999 SECTION 5 PERFORMANCE REPORT: VB-1710 5-29 PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-29 Y NL O CE EN T ER IGH EF FL R R OR FO T F NO ISA ENDURANCE Figure 5-31 ISSUED: FEBRUARY 23, 1999
PAGE 155
SECTION 5 PERFORMANCE PA-46-350P, MALIBU ISSUED: FEBRUARY 23, 1999 FUEL, TIME, AND DISTANCE TO DESCEND Figure 5-33 REPORT: VB-1710 5-30 SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y NL O CE EN T ER IGH EF FL R R OR FO T F NO ISSUED: FEBRUARY 23, 1999 FUEL, TIME, AND DISTANCE TO DESCEND Figure 5-33 REPORT: VB-1710 5-30
PAGE 156
PA-46-350P, MALIBU GLIDE TIME AND DISTANCE Figure 5-35 ISSUED: FEBRUARY 23, 1999 SECTION 5 PERFORMANCE REPORT: VB-1710 5-31 PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-31 Y NL O CE EN T ER IGH EF FL R R OR FO T F NO GLIDE TIME AND DISTANCE Figure 5-35 ISSUED: FEBRUARY 23, 1999
PAGE 157
SECTION 5 PERFORMANCE REPORT: VB-1710 5-32 BALKED LANDING CLIMB Figure 5-37 PA-46-350P, MALIBU ISSUED: FEBRUARY 23, 1999 SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y NL ISSUED: FEBRUARY 23, 1999 BALKED LANDING CLIMB Figure 5-37 O CE EN T ER IGH EF FL R R OR FO T F NO REPORT: VB-1710 5-32
PAGE 158
PA-46-350P, MALIBU SECTION 5 PERFORMANCE REPORT: VB-1710 5-33 LANDING DISTANCE OVER 50 FT. OBSTACLE Figure 5-39 ISSUED: FEBRUARY 23, 1999 REVISED: SEPTEMBER 20, 1999 PA-46-350P, MALIBU SECTION 5 PERFORMANCE Y NL O CE EN T ER IGH EF FL R R OR FO T F NO REPORT: VB-1710 5-33 LANDING DISTANCE OVER 50 FT.
PAGE 159
SECTION 5 PERFORMANCE REPORT: VB-1710 5-34 LANDING GROUND ROLL Figure 5-41 PA-46-350P, MALIBU ISSUED: FEBRUARY 23, 1999 REVISED: SEPTEMBER 20, 1999 SECTION 5 PERFORMANCE PA-46-350P, MALIBU Y NL ISSUED: FEBRUARY 23, 1999 REVISED: SEPTEMBER 20, 1999 LANDING GROUND ROLL Figure 5-41 O CE EN T ER IGH EF FL R R OR FO T F NO REPORT: VB-1710 5-34
PAGE 160
SECTION 6 WEIGHT AND BALANCE PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 6 SECTION 6 WEIGHT AND BALANCE WEIGHT AND BALANCE Paragraph No. 6.1 6.3 6.5 6.7 6.9 SECTION 6 WEIGHT AND BALANCE PA-46-350P, MALIBU Page No. General .................................................................................... 6-1 Airplane Weighing Procedure .................................................. 6-2 Weight and Balance Data and Record ......................................
PAGE 161
SECTION 6 WEIGHT AND BALANCE PA-46-350P, MALIBU 6.1 SECTION 6 WEIGHT AND BALANCE PA-46-350P, MALIBU SECTION 6 SECTION 6 WEIGHT AND BALANCE WEIGHT AND BALANCE GENERAL 6.1 In order to achieve the performance and flying characteristics which are designed into the airplane, it must be flown with the weight and center of gravity (C.G.) position within the approved operating range (envelope).
PAGE 162
SECTION 6 WEIGHT AND BALANCE 6.1 PA-46-350P, MALIBU SECTION 6 WEIGHT AND BALANCE 6.1 GENERAL (Continued) PA-46-350P, MALIBU GENERAL (Continued) The basic empty weight and C.G. location are recorded in the Weight and Balance Data Form (Figure 6-5) and the Weight and Balance Record (Figure 6-7). The current values should always be used. Whenever new equipment is added or any modification work is done, the mechanic responsible for the work is required to compute a new basic empty weight and C.G.
PAGE 163
SECTION 6 WEIGHT AND BALANCE PA-46-350P, MALIBU 6.3 AIRPLANE WEIGHING PROCEDURE (Continued) SECTION 6 WEIGHT AND BALANCE PA-46-350P, MALIBU 6.3 AIRPLANE WEIGHING PROCEDURE (Continued) CAUTION CAUTION Whenever the fuel system is completely drained and fuel is replenished, it will be necessary to run the engine for a minimum of three minutes at 1000 rpm on each tank to ensure that no air exists in the fuel supply lines.
PAGE 164
SECTION 6 WEIGHT AND BALANCE 6.3 PA-46-350P, MALIBU AIRPLANE WEIGHING PROCEDURE (Continued) Scale Reading Scale Position and Symbol Tare SECTION 6 WEIGHT AND BALANCE 6.
PAGE 165
SECTION 6 WEIGHT AND BALANCE PA-46-350P, MALIBU 6.3 AIRPLANE WEIGHING PROCEDURE (Continued) 6.3 (2) The basic empty weight center of gravity (as weighed including optional equipment, full oil and unusable fuel) can be determined by the following formula: C.G. Arm = N (A) + (R + L) (B) T AIRPLANE WEIGHING PROCEDURE (Continued) (2) The basic empty weight center of gravity (as weighed including optional equipment, full oil and unusable fuel) can be determined by the following formula: C.G.
PAGE 166
SECTION 6 WEIGHT AND BALANCE 6.5 PA-46-350P, MALIBU WEIGHT AND BALANCE DATA AND RECORD (Continued) SECTION 6 WEIGHT AND BALANCE 6.
PAGE 167
SECTION 6 WEIGHT AND BALANCE WEIGHT AND BALANCE DATA AND RECORD (Continued) PA-46-350P, MALIBU 6.5 REPORT: VB-1710 6-7 WEIGHT AND BALANCE RECORD Figure 6-7 ISSUED: FEBRUARY 23, 1999 SECTION 6 WEIGHT AND BALANCE WEIGHT AND BALANCE DATA AND RECORD (Continued) PA-46-350P, MALIBU 6.
PAGE 168
PA-46-350P, MALIBU WEIGHT AND BALANCE DATA AND RECORD (Continued) SECTION 6 WEIGHT AND BALANCE 6.5 ISSUED: FEBRUARY 23, 1999 WEIGHT AND BALANCE RECORD (cont) Figure 6-7 (cont) REPORT: VB-1710 6-8 PA-46-350P, MALIBU WEIGHT AND BALANCE DATA AND RECORD (Continued) SECTION 6 WEIGHT AND BALANCE 6.
PAGE 169
PA-46-350P, MALIBU SECTION 6 WEIGHT AND BALANCE PA-46-350P, MALIBU SECTION 6 WEIGHT AND BALANCE 6.7 GENERAL LOADING RECOMMENDATIONS For all airplane configurations, it is the responsibility of the pilot in command to make sure that the airplane always remains within the allowable weight vs. center of gravity while in flight. 6.7 The following general loading recommendation is intended only as a guide.
PAGE 170
SECTION 6 WEIGHT AND BALANCE 6.9 PA-46-350P, MALIBU WEIGHT AND BALANCE DETERMINATION FOR FLIGHT SECTION 6 WEIGHT AND BALANCE 6.9 PA-46-350P, MALIBU WEIGHT AND BALANCE DETERMINATION FOR FLIGHT (a) Add the weight of all items to be loaded, except fuel, to the basic empty weight to determine zero fuel weight. (a) Add the weight of all items to be loaded, except fuel, to the basic empty weight to determine zero fuel weight.
PAGE 171
PA-46-350P, MALIBU 6.9 SECTION 6 WEIGHT AND BALANCE WEIGHT AND BALANCE DETERMINATION FOR FLIGHT (Continued) Basic Empty Weight Pilot and Front Passenger Passengers (Center Seats) Passengers (Rear Seats) Baggage (Forward) (100 Lb Limit) Baggage (Aft) (100 Lb Limit) Zero Fuel Weight (4123 Lb Max.) Fuel (120 Gal./720 Lb Max. Usable) Ramp Weight (4358 Lb Max.) Fuel Allowance for Engine Start, Taxi, & Runup (3 Gal./18 Lb Max.) Takeoff Weight (4340 Lb Max.) Weight (Lb) 3156.5 320 340 140 0 80 4036.5 321.
PAGE 172
SECTION 6 WEIGHT AND BALANCE 6.9 PA-46-350P, MALIBU WEIGHT AND BALANCE DETERMINATION FOR FLIGHT (Continued) Weight (Lb) Basic Empty Weight Pilot and Front Passenger Passengers (Center Seats) Passengers (Rear Seats) Baggage (Forward) (100 Lb Limit) Baggage (Aft) (100 Lb Limit) Zero Fuel Weight (4123 Lb Max.) Fuel (120 Gal./720 Lb Max. Usable) Ramp Weight (4358 Lb Max.) Fuel Allowance for Engine Start, Taxi, & Runup (3 Gal./18 Lb Max.) Takeoff Weight (4340 Lb Max.) Arm Aft of Datum (Inches) 150.31 150.
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SECTION 6 WEIGHT AND BALANCE PA-46-350P, MALIBU 6.9 WEIGHT AND BALANCE DETERMINATION FOR FLIGHT (Continued) SECTION 6 WEIGHT AND BALANCE PA-46-350P, MALIBU 6.
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SECTION 6 WEIGHT AND BALANCE 6.9 PA-46-350P, MALIBU WEIGHT AND BALANCE DETERMINATION FOR FLIGHT (Continued) SECTION 6 WEIGHT AND BALANCE 6.9 PA-46-350P, MALIBU WEIGHT AND BALANCE DETERMINATION FOR FLIGHT (Continued) Y L N O E C N E HT R E LIG F E F R R R O FO T F NO C.G. Location (Inches aft of datum) C.G. Location (Inches aft of datum) C.G. RANGE AND WEIGHT GRAPH Figure 6-15 C.G.
PAGE 175
SECTION 7 DESCR / OPERATION PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 7 SECTION 7 DESCRIPTION AND OPERATION OF THE AIRPLANE AND ITS SYSTEMS DESCRIPTION AND OPERATION OF THE AIRPLANE AND ITS SYSTEMS Paragraph Page No. No. Paragraph Page No. No. 7.1 7.3 7.5 7.6 7.7 7.8 7.9 7.11 7.13 7.15 7.17 7.19 7.21 7.23 7.25 7.27 7.29 7.31 7.33 7.35 7.37 7.39 7.41 7.43 SECTION 7 DESCR / OPERATION PA-46-350P, MALIBU The Airplane................................................................
PAGE 176
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.1 SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 SECTION 7 DESCRIPTION AND OPERATION OF THE AIRPLANE AND ITS SYSTEMS DESCRIPTION AND OPERATION OF THE AIRPLANE AND ITS SYSTEMS THE AIRPLANE 7.1 THE AIRPLANE The PA-46-350P Malibu is a single engine, all metal, retractable landing gear, low wing, turbocharged airplane. It has a pressurized cabin with seating for six occupants and two separate luggage compartments.
PAGE 177
SECTION 7 DESCR/OPERATION 7.3 PA-46-350P, MALIBU THE AIRFRAME (Continued) SECTION 7 DESCR/OPERATION 7.3 PA-46-350P, MALIBU THE AIRFRAME (Continued) The wing is in effect a three section structure. The center section built-up main spar extends through the lower fuselage and outboard of each main landing gear. This section has a forward spar and a rear spar which are pin jointed at the fuselage sides. The main landing gear retracts inward into recesses located aft of the main spar.
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PA-46-350P, MALIBU 7.5 SECTION 7 DESCR/OPERATION ENGINE AND PROPELLER (Continued) PA-46-350P, MALIBU 7.5 SECTION 7 DESCR/OPERATION ENGINE AND PROPELLER (Continued) manifold pressure. Accessories include a starter, two magnetos, a propeller governor, two belt driven alternators, two gear driven vacuum pumps, a belt driven air conditioner compressor, an oil filter, and an air/oil separator in the crankcase breather system. manifold pressure.
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SECTION 7 DESCR/OPERATION 7.5 PA-46-350P, MALIBU ENGINE AND PROPELLER (continued) SECTION 7 DESCR/OPERATION 7.
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PA-46-350P, MALIBU 7.5 SECTION 7 DESCR/OPERATION ENGINE AND PROPELLER (continued) PA-46-350P, MALIBU 7.5 SECTION 7 DESCR/OPERATION ENGINE AND PROPELLER (continued) from overboost damage by limiting manifold pressure to 42.0 in. Hg. In the event of a controller malfunction, there is a pressure relief valve on the induction manifold which will relieve manifold pressure and prevent an overboost. from overboost damage by limiting manifold pressure to 42.0 in. Hg.
PAGE 181
SECTION 7 DESCR/OPERATION 7.7 PA-46-350P, MALIBU ENGINE CONTROLS (Continued) SECTION 7 DESCR/OPERATION 7.
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SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.5 ENGINE AND PROPELLER (Continued) SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.5 ENGINE AND PROPELLER (Continued) Oil temperature and pressure information is available from separate gauges located as part of the engine gauge stack. Engine crankcase gases are discharged to an air/oil separator behind the left rear cylinder, and then vented out the left exhaust stack.
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SECTION 7 DESCR/OPERATION 7.6 PA-46-350P, MALIBU AIR INDUCTION SYSTEM (Continued) SECTION 7 DESCR/OPERATION 7.6 PA-46-350P, MALIBU AIR INDUCTION SYSTEM (Continued) The engine air induction system receives ram air through forward facing ram air louvers located on the lower cowl below the propeller. Air enters these louvers and flows through a removable air filter mounted adjacent to the louvers. The filter removes dust and other foreign matter from the induction air.
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SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.7 ENGINE CONTROLS (Continued) SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.
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SECTION 7 DESCR/OPERATION 7.7 PA-46-350P, MALIBU ENGINE CONTROLS (Continued) SECTION 7 DESCR/OPERATION 7.7 PA-46-350P, MALIBU ENGINE CONTROLS (Continued) The friction adjustment lever, located on the far left of the control quadrant, may be adjusted to increase or decrease the friction holding the throttle, propeller and mixture controls.
PAGE 186
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION Each analog indicator also has a red status light which illuminates when a red line limitation exceedance has occurred. Each fuel quantity indicator has an amber "low fuel" status light in place of red, which illuminates with 5 gallons or less of usable fuel indicated. Each analog indicator also has a red status light which illuminates when a red line limitation exceedance has occurred.
PAGE 187
SECTION 7 DESCR/OPERATION 7.8 PA-46-350P, MALIBU TRANSICOIL ELECTRONIC MODULE INSTRUMENT SYSTEM (EMIS) (CONT'D) SECTION 7 DESCR/OPERATION 7.8 PA-46-350P, MALIBU TRANSICOIL ELECTRONIC MODULE INSTRUMENT SYSTEM (EMIS) (CONT'D) After the self-test is complete, the EDI will automatically display the MAP, RPM, TIT, FF and OAT in the LCD windows. NOTE: Any exceedances that have previously been recorded must be called up manually by the operator.
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SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU Y L N O E C N E HT R E LIG F E F R R R O FO T F NO FIGURE 7-7 FIGURE 7-7 Transicoil Electronic Module Instrument System (EMIS) Transicoil Electronic Module Instrument System (EMIS) ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 7-13 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 7-13
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SECTION 7 DESCR/OPERATION 7.8 PA-46-350P, MALIBU TRANSICOIL ELECTRONIC MODULE INSTRUMENT SYSTEM (EMIS) (CONT'D) SECTION 7 DESCR/OPERATION 7.8 PA-46-350P, MALIBU TRANSICOIL ELECTRONIC MODULE INSTRUMENT SYSTEM (EMIS) (CONT'D) Note: During fuel loading entry sequence, the three digits must display 120 gallons or less at all times to permit fuel load entry into the EDI.
PAGE 190
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION As percent power is changed, a suggested approximate value for manifold pressure and fuel flow will be displayed. If a different RPM is desired, the set button can be depressed to toggle the active parameter to the RPM display, and the up/down arrow buttons can be used to vary the RPM in 100 RPM increments. This variation in RPM changes expected values of MAP and Fuel Flow accordingly.
PAGE 191
SECTION 7 DESCR/OPERATION 7.8 PA-46-350P, MALIBU TRANSICOIL ELECTRONIC MODULE INSTRUMENT SYSTEM (EMIS) (CONT'D) SECTION 7 DESCR/OPERATION 7.8 PA-46-350P, MALIBU TRANSICOIL ELECTRONIC MODULE INSTRUMENT SYSTEM (EMIS) (CONT'D) CAUTION: When the memory for limitation exceedance recording is full, no new exceedancies will be recorded (the memory can accommodate a total of 238 exceedance events for all indicators).
PAGE 192
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION The push button functions used to review the limitation exceedance events in the exceedance review mode "PEAK DISPLAY" are" 1. Down Arrow - This button will cause the EDI display to post all the exceedance events for the indicator under examination. Each time the down arrow button is pressed, the posted data will change to the next peak exceedance for the same indicator. 2.
PAGE 193
SECTION 7 DESCR/OPERATION 7.8 PA-46-350P, MALIBU TRANSICOIL ELECTRONIC MODULE INSTRUMENT SYSTEM (EMIS) (CONT'D) SECTION 7 DESCR/OPERATION 7.8 PA-46-350P, MALIBU TRANSICOIL ELECTRONIC MODULE INSTRUMENT SYSTEM (EMIS) (CONT'D) An example of a limitation exceedance review operation would consist of depressing the "E" and "N" buttons simultaneously to enter the review mode for the Peak Display. At this time, two possible display presentations will be posted based on the status of the EDI exceedance memory.
PAGE 194
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION Y L N Instrument Mode - Aircraft on the Ground Figure 7-9 Instrument Mode - Aircraft in Flight Figure 7-11 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 7-19 O E Con the Ground N Instrument Mode - Aircraft T E R Figure 7-9 H E LIG F E F R R R O FO T F NO Instrument Mode - Aircraft in Flight Figure 7-11 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 7-19
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SECTION 7 DESCR/OPERATION 7.8 PA-46-350P, MALIBU TRANSICOIL ELECTRONIC MODULE INSTRUMENT SYSTEM (EMIS) (CONT'D) SECTION 7 DESCR/OPERATION 7.
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SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU Y L N O E C N E HT R E LIG F E F R R R O FO T F NO Fuel Loading Mode Figure 7-17 Fuel Loading Mode Figure 7-17 Exceedance Review Mode Figure 7-19 ISSUED: FEBRUARY 23, 1999 Exceedance Review Mode Figure 7-19 REPORT: VB-1710 7-21 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 7-21
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SECTION 7 DESCR/OPERATION 7.8 PA-46-350P, MALIBU TRANSICOIL ELECTRONIC MODULE INSTRUMENT SYSTEM (EMIS) (CONT'D) SECTION 7 DESCR/OPERATION 7.
PAGE 198
SECTION 7 DESCR/OPERATION 7.9 PA-46-350P, MALIBU HYDRAULIC SYSTEM SECTION 7 DESCR/OPERATION 7.9 PA-46-350P, MALIBU HYDRAULIC SYSTEM The hydraulic system (refer to Figure 7-21) provides the power to retract and extend the landing gear. The hydraulic system (refer to Figure 7-21) provides the power to retract and extend the landing gear. The electric motor driven hydraulic pump assembly is located aft of the rear baggage compartment and is accessible through the baggage compartment aft closeout panel.
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SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.9 HYDRAULIC SYSTEM (Continued) SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.
PAGE 200
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.11 LANDING GEAR 7.11 LANDING GEAR The aircraft is equipped with hydraulically operated, fully retractable, tricycle landing gear. The aircraft is equipped with hydraulically operated, fully retractable, tricycle landing gear. Locking-type actuators are used for main and nose gears. The actuator assembly provides mechanical gear-down locking at the fully extended position and is hydraulically unlocked.
PAGE 201
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.11 LANDING GEAR (continued) The landing gear is held in the DOWN position by spring loaded mechanical locking mechanisms built into each of the three actuating cylinders. The individual gear safe light switches are also mechanically operated when each mechanism is in the LOCKED position. With the hydraulic pump and system operating normally, hydraulic pressure is also trapped in the DOWN side of the system.
PAGE 202
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.11 LANDING GEAR (Continued) 7.
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PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.11 LANDING GEAR (Continued) PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.11 LANDING GEAR (Continued) CAUTION: When flying in extreme cold where the aircraft has been cold soaked for hours, the gear may not indicate down and locked for 10 to 15 seconds while aircraft temperatures are stabilizing.
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SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.13 BRAKE SYSTEM (Continued) 7.13 BRAKE SYSTEM (Continued) The parking brake knob is located just below the left control column. To set the parking brake, first depress and hold the toe brake pedals and then pull the parking brake knob. To release the parking brake, first depress and hold the toe brake pedals and then push in on the parking brake knob.
PAGE 205
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.17 FUEL SYSTEM Fuel is stored in two main integral wing tanks (see Figure 7-27), located outboard of the mid-wing splice. Fuel quantity held by each wing tank is 60 usable gallons with one gallon of unusable fuel, for a total of 122 gallons. The minimum fuel grade is 100 or 100LL aviation grade.
PAGE 206
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.17 FUEL SYSTEM (Continued) SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.17 FUEL SYSTEM (Continued) CAUTION For proper mid range accuracy, fuel quantity readings should be taken when the aircraft is in coordinated level flight at zero degrees bank angle. (Pitch, roll and yaw.) Failure to observe fuel quantity in this manner will result in erroneous readings due to wing cross section, low dihedral angle and fuel tank geometry.
PAGE 207
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.17 FUEL SYSTEM (Continued) 7.
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SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.17 FUEL SYSTEM (Continued) Should the fuel boost pump in the fuel tank being used fail to produce sufficient pressure, the BOOST PUMP light on the annunciator panel will illuminate. In this event, confirm that the fuel selector is properly seated in the detent for the selected tank. If the selector is properly seated, and the annunciator remains lit, select the opposite tank.
PAGE 209
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.17 FUEL SYSTEM (Continued) 7.17 FUEL SYSTEM (Continued) When beginning flight operations with an equal amount of fuel in each tank, start, taxi, takeoff, and climb on the left tank. When beginning operations with unequal amounts of fuel in each tank, care must be taken not to exceed the fuel imbalance limitations specified in paragraph 2.23(e).
PAGE 210
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.19 ELECTRICAL SYSTEM (Continued) SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.
PAGE 211
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.19 ELECTRICAL SYSTEM (Continued) 7.19 ELECTRICAL SYSTEM (Continued) When the Battery Master switch, located on the main switch panel, is turned ON, the battery solenoid contactor closes, enabling current to flow from the battery to both the starter solenoid contactor and the tie bus located on the lower left section of the pilot’s instrument panel (Figures 7-37b and 7- 39).
PAGE 212
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.19 ELECTRICAL SYSTEM (continued) SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.19 ELECTRICAL SYSTEM (continued) Left Overhead Switch Panel Right Overhead Switch Panel Left Overhead Switch Panel Right Overhead Switch Panel MAIN ELECTRICAL SWITCH PANEL (Overhead) Figure 7-31 A main bus and a nonessential bus (Figure 7-35), with associated circuit breakers, are located on the pilot’s left side panels.
PAGE 213
PA-46-350P, MALIBU 7.19 SECTION 7 DESCR/OPERATION ELECTRICAL SYSTEM (Continued) PA-46-350P, MALIBU 7.
PAGE 214
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.19 ELECTRICAL SYSTEM (Continued) SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.
PAGE 215
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.19 ELECTRICAL SYSTEM (Continued) 7.
PAGE 216
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.21 INSTRUMENT PANEL 7.21 INSTRUMENT PANEL The instrument panel is designed to accommodate the customary advanced flight instruments and the normally required power plant instruments. The pilots artificial horizon is vacuum operated, while the directional gyro and turn coordinator are electrically operated.
PAGE 217
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.21 INSTRUMENT PANEL (Continued) 7.21 INSTRUMENT PANEL (Continued) An annunciator panel, located at the top of the left radio stack. Monitored system includes: An annunciator panel, located at the top of the left radio stack. Monitored system includes: VACUUM NO. 1 INOP, VACUUM NO. 2 INOP, OIL PRESSURE, HYDRAULIC PUMP, PITOT HEAT OFF/INOP, FUEL IMBALANCE, ALTERNATOR NO.
PAGE 218
SECTION 7 DESCR/OPERATION REPORT: VB-1710 7-44 INSTRUMENT PANEL Figure 7-39 PA-46-350P, MALIBU ISSUED: FEBRUARY 23, 1999 SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU Y NL ISSUED: FEBRUARY 23, 1999 INSTRUMENT PANEL Figure 7-39 O CE EN T ER IGH EF FL R R OR FO T F NO REPORT: VB-1710 7-44
PAGE 219
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.21 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11 12 13. 14. 15. 16. a b . c d e f 17. 18. 19. 20. 21. INSTRUMENT PANEL (Continued) Gyro Slaving Control Digital Clock Stall Test Switch Airspeed Indicator Turn and Bank Indicator RMI/ADF Indicator Avionics Switches Attitude Indicator Flt Director Horizontal Situation Indicator Altitude Preselect Pressure Altimeter (encoding) Vertical Speed Indicator Cabin Pressure Controller Triple Indicator a. Cabin Vertical Speed b.
PAGE 220
SECTION 7 DESCR/OPERATION 7.23 PA-46-350P, MALIBU PITOT STATIC SYSTEM SECTION 7 DESCR/OPERATION 7.23 PA-46-350P, MALIBU PITOT STATIC SYSTEM Pitot pressure for the airspeed indicator is sensed by a heated pitot head installed on the bottom of the left wing and is carried through lines within the wing and fuselage to the gauge on the instrument panel (refer to Figure 7-39).
PAGE 221
PA-46-350P, MALIBU 7.23 PITOT STATIC SYSTEM (Continued) SECTION 7 DESCR/OPERATION REPORT: VB-1710 7-47 PITOT AND STATIC PRESSURE SYSTEMS Figure 7-41 ISSUED: FEBRUARY 23, 1999 PA-46-350P, MALIBU 7.
PAGE 222
SECTION 7 DESCR/OPERATION 7.25 PA-46-350P, MALIBU ENVIRONMENTAL SYSTEM (Refer to Figure 7-43) SECTION 7 DESCR/OPERATION 7.25 PA-46-350P, MALIBU ENVIRONMENTAL SYSTEM (Refer to Figure 7-43) The environmental system consists of: The environmental system consists of: (a) (b) (c) (d) (e) (f) (a) (b) (c) (d) (e) (f) A compressor bleed air and conditioning system. The ventilating air system. A supplemental electric cabin heater. An air conditioning system. The cabin air distribution system.
PAGE 223
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION The supplemental electric heater consists of a resistance type heat element, a dual hermetically sealed bimetallic type overtemperature protection, a power relay, and a 35 amp in line current limiter fuse. Its function is to provide additional heat for maintaining desired cabin comfort during ground or flight operations under temperature conditions when fully heated bleed air or ventilating air is inadequate.
PAGE 224
SECTION 7 DESCR/OPERATION 7.25 PA-46-350P, MALIBU ENVIRONMENTAL SYSTEM (Continued) SECTION 7 DESCR/OPERATION 7.25 PA-46-350P, MALIBU ENVIRONMENTAL SYSTEM (Continued) The AIR COND and BLOWER HI & LO switches, located as part of the environmental switch panel in the center of the instrument panel, are used to control the air conditioning system.
PAGE 225
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.25 ENVIRONMENTAL SYSTEM (Continued) PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.
PAGE 226
SECTION 7 DESCR/OPERATION 7.27 PA-46-350P, MALIBU BLEED AIR, CONDITIONING AND PRESSURIZATION SYSTEM SECTION 7 DESCR/OPERATION 7.27 PA-46-350P, MALIBU BLEED AIR, CONDITIONING AND PRESSURIZATION SYSTEM Air for cabin pressure is obtained from the engine turbocharger induction air system through two sonic venturi tubes. Bleed air is routed through the bleed air heat exchanger for the temperature conditioning to provide the desired cabin comfort level.
PAGE 227
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.27 BLEED AIR, CONDITIONING AND PRESSURIZATION SYSTEM (Continued) PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.27 BLEED AIR, CONDITIONING AND PRESSURIZATION SYSTEM (Continued) Y L N PRESSURIZATION CONTROL SCHEMATIC Figure 7-45 Below the cabin pressure controller, a triple indicator simplifies monitoring the system’s operation.
PAGE 228
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.27 BLEED AIR, CONDITIONING AND PRESSURIZATION SYSTEM (Continued) SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.27 BLEED AIR, CONDITIONING AND PRESSURIZATION SYSTEM (Continued) Y L N O E C N E HT R E LIG F E F R R R O FO T F NO CABIN ALTITUDE VS. AIRPLANE ALTITUDE Figure 7-47 REPORT: VB-1710 7-54 ISSUED: FEBRUARY 23, 1999 CABIN ALTITUDE VS.
PAGE 229
PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.27 BLEED AIR, CONDITIONING AND PRESSURIZATION SYSTEM (Continued) 7.27 BLEED AIR, CONDITIONING AND PRESSURIZATION SYSTEM (Continued) For unpressurized flight the CABIN PRESS control should be pulled fully out. Setting the CABIN PRESS/DUMP/NORM switch to DUMP will provide maximum airflow through the cabin. Cabin temperature will continue to be controlled by the CABIN TEMP control.
PAGE 230
SECTION 7 DESCR/OPERATION 7.29 PA-46-350P, MALIBU VACUUM SYSTEM (Continued) SECTION 7 DESCR/OPERATION 7.29 PA-46-350P, MALIBU VACUUM SYSTEM (Continued) Upon completion of the flight, all system abnormalities or malfunctions should be checked by a mechanic, and necessary repairs made, prior to further pressurized flight or flight under IFR.
PAGE 231
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.29 VACUUM SYSTEM (Continued) 7.
PAGE 232
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.31 CABIN FEATURES 7.31 CABIN FEATURES The front seats are adjustable fore and aft and vertically. Pivoting armrests are provided on the inboard side of each seat. The front seats are adjustable fore and aft and vertically. Pivoting armrests are provided on the inboard side of each seat. Shoulder harnesses with inertia reels are standard equipment for all seats.
PAGE 233
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.31 CABIN FEATURES (Continued) PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION 7.31 CABIN FEATURES (Continued) Y L N EMERGENCY EXIT Figure 7-51 Optional passenger oxygen generators and masks are available and, if installed, are located in a drawer under the right aft facing seat. Crew oxygen is located under the copilot’s seat, readily available to either crew member. An annunciator light illuminates when any of the three generators have been activated.
PAGE 234
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.33 BAGGAGE AREA 7.33 BAGGAGE AREA The airplane has two separate baggage areas each with a 100-pound capacity. A 13-cubic-foot forward baggage compartment, located just aft of the firewall, is accessible through a 19 x 23 inch door on the left side of the fuselage. An aft baggage compartment, which is accessible from inside the cabin, is located behind the back seats.
PAGE 235
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.39 EMERGENCY LOCATOR TRANSMITTER 7.39 EMERGENCY LOCATOR TRANSMITTER The Emergency Locator Transmitter (ELT) meets the requirements of FAR 91.52. It operates on self-contained batteries and is located in the aft fuselage section. It is accessible through a cover on the bottom right side. The Emergency Locator Transmitter (ELT) meets the requirements of FAR 91.52.
PAGE 236
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.39 EMERGENCY LOCATOR TRANSMITTER (Continued) 7.39 EMERGENCY LOCATOR TRANSMITTER (Continued) ARTEX ELT OPERATION (Cont'd) ARTEX ELT OPERATION (Cont'd) The transmitter can be activated manually at any time by placing either the remote switch or the ELT switch to the ON position. The transmitter can be activated manually at any time by placing either the remote switch or the ELT switch to the ON position.
PAGE 237
SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU SECTION 7 DESCR/OPERATION PA-46-350P, MALIBU 7.43 RADAR* 7.43 RADAR* A weather radar system can be installed in the airplane. The basic components of this installation are a Receiver-Transmitter Antenna and a cockpit indicator. The function of the weather radar system is to detect weather conditions along the flight path and to visually display a continuous weather outline on the cockpit indicator.
PAGE 238
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 8 SECTION 8 AIRPLANE HANDLING, SERVICING, AND MAINTNEANCE AIRPLANE HANDLING, SERVICING, AND MAINTNEANCE Paragraph No. 8.1 8.3 8.5 8.7 8.9 8.11 8.13 8.15 8.17 8.19 8.21 8.23 8.25 8.27 8.29 8.31 8.33 8.35 8.36 SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU Page No. General ..................................................................................... Airplane Inspection Periods ...........................
PAGE 239
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 SECTION 8 AIRPLANE HANDLING, SERVICING, AND MAINTENANCE AIRPLANE HANDLING, SERVICING, AND MAINTENANCE 8.1 GENERAL 8.1 GENERAL This section provides guidelines relating to the handling, servicing, and maintenance of the Malibu Mirage. For complete maintenance instructions, refer to the PA-46-350P Maintenance Manual.
PAGE 240
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.1 GENERAL (CONTINUED) SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.1 GENERAL (CONTINUED) WARNING WARNING Use only genuine PIPER parts or PIPER approved parts obtained from PIPER approved sources, in connection with the maintenance and repair of PIPER airplanes. Use only genuine PIPER parts or PIPER approved parts obtained from PIPER approved sources, in connection with the maintenance and repair of PIPER airplanes.
PAGE 241
PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT 8.1 GENERAL (CONTINUED) 8.1 GENERAL (CONTINUED) Every owner should stay in close contact with an authorized Piper Service Center or Piper’s Customer Services Department to obtain the latest information pertaining to their airplane, and to avail themselves of Piper’s support systems.
PAGE 242
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.3 AIRPLANE INSPECTION PERIODS 8.3 AIRPLANE INSPECTION PERIODS WARNING WARNING All inspection intervals, replacement time limits, overhaul time limits, the method of inspection, life limits, cycle limits, etc., recommended by PIPER are solely based on the use of new, remanufactured or overhauled PIPER approved parts.
PAGE 243
PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT 8.3 AIRPLANE INSPECTION PERIODS (CONTINUED) 8.3 AIRPLANE INSPECTION PERIODS (CONTINUED) A spectrographic analysis of the engine oil is available from several sources. This inspection, if performed properly, provides a good check of the internal condition of the engine. To be accurate, induction air filters must be cleaned or changed regularly, and oil samples must be taken and sent in at regular intervals.
PAGE 244
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.7 AIRPLANE ALTERATIONS (CONTINUED) The owner or pilot is required to ascertain that the following aircraft papers are in order and in the aircraft. 8.7 AIRPLANE ALTERATIONS (CONTINUED) The owner or pilot is required to ascertain that the following aircraft papers are in order and in the aircraft. (a) To be displayed in the aircraft at all times: (1) Aircraft Airworthiness Certificate Form FAA-8100-2.
PAGE 245
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.9 GROUND HANDLING (CONTINUED) by not less than fifteen feet, and a qualified person should ride in the pilot’s seat to maintain control by use of the brakes. (b) Taxiing SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.9 GROUND HANDLING (CONTINUED) by not less than fifteen feet, and a qualified person should ride in the pilot’s seat to maintain control by use of the brakes.
PAGE 246
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.9 GROUND HANDLING (CONTINUED) SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.9 GROUND HANDLING (CONTINUED) CAUTION CAUTION Care should be taken when setting brakes that are overheated or during cold weather when accumulated moisture may freeze a brake. Care should be taken when setting brakes that are overheated or during cold weather when accumulated moisture may freeze a brake.
PAGE 247
PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT 8.9 GROUND HANDLING (CONTINUED) PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT 8.9 GROUND HANDLING (CONTINUED) (6) Install a pitot head cover if available. Be sure to remove the pitot head cover before flight. (7) Cabin and baggage door should be locked when the air- plane is unattended. (6) Install a pitot head cover if available. Be sure to remove the pitot head cover before flight.
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SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU ISSUED: FEBRUARY 23, 1999 BRAKE SYSTEM Figure 8-1 8.13 BRAKE SERVICE (CONTINUED) REPORT: VB-1710 8-8 SECTION 8 HAND/SERV/MAINT 8.
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PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT 8.13 BRAKE SERVICE (CONTINUED) 8.13 BRAKE SERVICE (CONTINUED) located behind the aft access panel in the forward baggage compartment. If the entire system must be refilled, fill with fluid under pressure from the brake end of the system. This will eliminate air from the system. located behind the aft access panel in the forward baggage compartment.
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SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.17 LANDING GEAR SERVICE (CONTINUED) 8.17 LANDING GEAR SERVICE (CONTINUED) In jacking the aircraft for landing gear or other service, two hydraulic jacks and a tail stand should be used. At least 400 pounds of ballast should be placed on the base of the tail stand before the airplane is jacked up.
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SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.21 OIL REQUIREMENTS 8.21 OIL REQUIREMENTS The oil capacity of the Textron Lycoming TI0-540-AE2A engine is 12 quarts with an inflight minimum quantity of approximately 2.75 quarts. Maximum endurance flights should begin with 12 quarts of oil. For all shorter flights, it is recommended that oil be added if the quantity falls to 10 quarts.
PAGE 252
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.23 FUEL SYSTEM SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.23 FUEL SYSTEM (a) Servicing Fuel System (a) Servicing Fuel System At every 100 hour inspection or after an extended downtime, the fuel filter strainer must be cleaned. The fuel filter strainer is located below the floor on the lower right side of the forward baggage compartment.
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SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.23 FUEL SYSTEM (CONTINUED) SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.23 FUEL SYSTEM (CONTINUED) The operation of the aircraft is approved with an anti-icing additive in the fuel. When an anti-icing additive is used it must meet the specification MIL-1-27686, must be uniformly blended with the fuel while refueling, must not exceed .15% by volume of the refueled quantity, and to ensure its effectiveness should be blended at not less than .10% by volume.
PAGE 254
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.23 FUEL SYSTEM (CONTINUED) SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.23 FUEL SYSTEM (CONTINUED) Observe all safety precautions required when handling gasoline. Fill the fuel tanks through the filler located on the forward slope of the wing. Each wing holds a maximum of 60 U.S. gallons. When using less than the standard 120 gallon capacity, fuel should be distributed equally between each side.
PAGE 255
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.23 FUEL SYSTEM (CONTINUED) SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.23 FUEL SYSTEM (CONTINUED) Y L N FUEL TANK DRAIN Figure 8-3 (e) Emptying Fuel System Drain the bulk of fuel at sump tanks. Set fuel selector on left or right tank. Push in sump drain valves and twist turn to lock open. Remaining fuel may be drained through the filter drain. Close sump drain valves before refueling.
PAGE 256
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.25 TIRE INFLATION 8.25 TIRE INFLATION For maximum service, keep tires inflated to the proper pressure: 50 psi for the nose tire and 55 psi for the main tires. All wheels and tires are balanced before original installation, and the relationship of tire, tube, and wheel should be maintained upon reinstallation.
PAGE 257
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.33 LUBRICATION SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.33 LUBRICATION For lubricating instructions, a chart showing lubrication points and types of lubricants to be used, and lubrication methods, refer to the PA-46-350P Maintenance Manual. For lubricating instructions, a chart showing lubrication points and types of lubricants to be used, and lubrication methods, refer to the PA-46-350P Maintenance Manual. 8.35 8.
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SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.35 CLEANING (CONTINUED) SECTION 8 HAND/SERV/MAINT 8.35 CLEANING (CONTINUED) (b) Cleaning Landing Gear Before cleaning the landing gear, place a plastic cover or similar material over the wheel and brake assembly. (b) Cleaning Landing Gear Before cleaning the landing gear, place a plastic cover or similar material over the wheel and brake assembly. CAUTION Do not brush the micro switches. (1) Place a pan under the gear to catch waste.
PAGE 259
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.35 CLEANING (CONTINUED) (d) Cleaning Windshield and Windows 8.35 CLEANING (CONTINUED) (d) Cleaning Windshield and Windows CAUTION CAUTION Use only mild soap and water when cleaning the heated windshield. Use of ANY other cleaning agent or material may cause distortion or damage to windshield coatings. Use only mild soap and water when cleaning the heated windshield.
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SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.35 CLEANING (CONTINUED) SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.35 CLEANING (CONTINUED) (2) For simple stains (e.g. coffee, cola) clean headliner with a sponge and a common household suds detergent (e.g. Tide). Dirty grease stains should be first spot cleaned with a lighter fluid containing Naphtha to remove the solvent soluble matter. Any stain residue should then be shampooed with a household upholstery cleaner (e.g.
PAGE 261
PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT 8.35 CLEANING (CONTINUED) PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT 8.35 CLEANING (CONTINUED) airplane. If difficulty is encountered with the water freezing on boots, direct a blast of warm air along the region being cleaned using a portable ground heater. airplane. If difficulty is encountered with the water freezing on boots, direct a blast of warm air along the region being cleaned using a portable ground heater.
PAGE 262
SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT PA-46-350P, MALIBU 8.36 CLEANING AND MAINTENANCE OF RELIEF TUBE SYSTEM 8.36 CLEANING AND MAINTENANCE OF RELIEF TUBE SYSTEM When the aircraft is equipped with a relief tube system, the corrosive effects of urine or other liquids poured through the system are extreme and require much attention to the cleanliness of this system both inside and outside of the aircraft.
PAGE 263
PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT (b) Exterior PA-46-350P, MALIBU SECTION 8 HAND/SERV/MAINT (b) Exterior Exterior bottom painted surfaces of the aircraft must be cleaned from the firewall to the tip of the tail including the bottom of the tail surfaces, at termination of each flight when the relief tube system has been used. Cleaning should occur in accordance with paragraph 8.
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SECTION 9 SUPPLEMENTS PA-46-350P, MALIBU SECTION 9 SUPPLEMENTS PA-46-350P, MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 9 SECTION 9 SUPPLEMENTS SUPPLEMENTS Paragraph/Supplement No. Page No. Paragraph/Supplement No. Page No. 9.1 General .................................................................................... 9-1 9.1 General .................................................................................... 9-1 1 Emergency Oxygen System .................................
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SECTION 9 SUPPLEMENTS PA-46-350P, MALIBU 16 17 18 19 20 21 22 23 24 TABLE OF CONTENTS SECTION 9 SECTION 9 SUPPLEMENTS SUPPLEMENTS (continued) (continued) Page No. Garmin GNS 430 VHF Comm/ Nav/GPS ...............................................................(8 Pages) S-TEC System 55 Autopilot..................................................... Garmin GNS 530 VHF Comm/ Nav/GPS ...............................................................(8 Pages) Garmin GTX 327 Transponder......................
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SECTION 9 SUPPLEMENTS PA-46-350P, MALIBU 9.1 SECTION 9 SUPPLEMENTS PA-46-350P, MALIBU SECTION 9 SECTION 9 SUPPLEMENTS SUPPLEMENTS GENERAL 9.1 GENERAL This section provides information in the form of supplements which are necessary for efficient operation of the airplane when it is equipped with one or more of the various optional systems and equipment not approved with the standard airplane.
PAGE 267
SECTION 9 SUPPLEMENT 1 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 1 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 1 FOR EMERGENCY OXYGEN SYSTEM SUPPLEMENT NO. 1 FOR EMERGENCY OXYGEN SYSTEM This supplement must be attached to the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual when the Emergency Oxygen System is installed per Piper Drawing No. 83985-2.
PAGE 268
SECTION 9 SUPPLEMENT 1 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 1 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL This supplement supplies information necessary for the operation of the airplane when the optional Emergency Oxygen System is installed in accordance with FAA Approved Piper Data. This supplement supplies information necessary for the operation of the airplane when the optional Emergency Oxygen System is installed in accordance with FAA Approved Piper Data.
PAGE 269
SECTION 9 SUPPLEMENT 1 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 1 PA-46-350P, MALIBU SECTION 3 - EMERGENCY PROCEDURES SECTION 3 - EMERGENCY PROCEDURES In the event that the emergency oxygen system is needed, proceed as follows: In the event that the emergency oxygen system is needed, proceed as follows: Mask compartment(s) .................................................................................OPEN Mask......................................................................
PAGE 270
SECTION 9 SUPPLEMENT 1 PA-46-350, MALIBU SECTION 9 SUPPLEMENT 1 PA-46-350, MALIBU SECTION 4 - NORMAL PROCEDURES SECTION 4 - NORMAL PROCEDURES Prior to each flight, turn on the master switch and check that the amber OXYGEN annunciator light is not illuminated. If the annunciator is illuminated, one or more of the oxygen generators should be replaced. In addition, check the oxygen masks and hoses for accessibility and condition.
PAGE 271
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 1 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 1 The crew assembly is located under the copilot’s seat and contains one two-man oxygen generator and two masks mounted on a sliding tray. The tray is accessible from the aisle between the pilot’s and copilot’s seats and is pulled out from under the seat to expose the two masks. Each mask is connected to the generator with a clear plastic tube and lanyard.
PAGE 272
SECTION 9 SUPPLEMENT 1 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 1 PA-46-350P, MALIBU Y L N O E C N E HT R E LIG F E F R R R O FO T F NO OXYGEN SYSTEM INSTALLATION Figure 7-1. REPORT: VB-1710 9-8, 6 of 6 ISSUED: FEBRUARY 23, 1999 OXYGEN SYSTEM INSTALLATION Figure 7-1.
PAGE 273
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 2 SECTION 9 SUPPLEMENT 2 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 2 FOR PROPELLER HEAT, HEATED WINDSHIELD AND WING ICE DETECTION LIGHT SUPPLEMENT NO.
PAGE 274
SECTION 9 SUPPLEMENT 2 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 2 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL This supplement supplies information necessary for the operation of the airplane when the optional propeller heat, heated windshield, and wing ice detection light are installed in accordance with FAA Approved Piper data.
PAGE 275
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 2 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 2 When in visible moisture at temperatures at or below +5°C and icing conditions are anticipated, turn on the windshield heat LO switch. If low windshield heat is inadequate or if icing is encountered at temperatures at or below -15°C, turn on the windshield heat HI switch.
PAGE 276
SECTION 9 SUPPLEMENT 2 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 2 PA-46-350P, MALIBU PROPELLER HEAT PROPELLER HEAT Electrothermal propeller heat pads are bonded to a portion of the leading edges of the propeller blades. The system is controlled by an ON-OFF type PROP HEAT switch (Figure 2-1) situated in the switch panel located above the right radio stack.
PAGE 277
SECTION 9 SUPPLEMENT 2 PA-46-350P, MALIBU ELECTRIC HEATED WINDSHIELD SECTION 9 SUPPLEMENT 2 PA-46-350P, MALIBU ELECTRIC HEATED WINDSHIELD WARNING Flight into known or forecast icing is not approved. If icing is encountered, take avoidance action immediately. WARNING Flight into known or forecast icing is not approved. If icing is encountered, take avoidance action immediately. The electrically heated left windshield is controlled by two switches in the switch panel.
PAGE 278
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 3 FOR ICE PROTECTION SYSTEM (APPROVED FOR FLIGHT INTO KNOWN ICING CONDITIONS) SUPPLEMENT NO.
PAGE 279
SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL This supplement supplies information necessary for the operation of the airplane when the optional Ice Protection System is installed in accordance with FAA Approved Piper data. This supplement supplies information necessary for the operation of the airplane when the optional Ice Protection System is installed in accordance with FAA Approved Piper data.
PAGE 280
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 SECTION 3 - EMERGENCY PROCEDURES SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 3 - EMERGENCY PROCEDURES WARNING The malfunction of any required deice equipment requires immediate action to exit icing conditions. Depending on the severity of the icing encounter, failure to take immediate positive action can lead to performance losses severe enough to make level flight impossible.
PAGE 281
SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SINGLE VACUUM PUMP FAILURE IN ICING CONDITIONS (Reduced suction pressure and left or right vacuum inoperative annunciator illuminate) SINGLE VACUUM PUMP FAILURE IN ICING CONDITIONS (Reduced suction pressure and left or right vacuum inoperative annunciator illuminate) Gyro Suction Gauge.................................Check (within normal operating range) Operative Pump vacuum inoperative annunciator ...................
PAGE 282
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 SURFACE DEICE MALFUNCTION SURFACE DEICE MALFUNCTION If SURFACE DE-ICE annunciator light remains illuminated more than 30 seconds, pull the surface deice circuit breaker. Immediate action should be taken to exit icing conditions. If SURFACE DE-ICE annunciator light remains illuminated more than 30 seconds, pull the surface deice circuit breaker. Immediate action should be taken to exit icing conditions.
PAGE 283
SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU After 30 seconds, the flash rate is reduced, indicating the heater is in the “off” cycle. The green lamp will continue to flash at the slower flash rate as long as the aircraft is on the ground or until the pilot deselects “prop heat” on the switch panel. SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU After 30 seconds, the flash rate is reduced, indicating the heater is in the “off” cycle.
PAGE 284
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 IN FLIGHT Icing conditions of any kind should be avoided whenever possible, since any minor malfunction which may occur is potentially more serious in icing conditions. Continuous attention of the pilot is required to monitor the rate of ice build-up in order to effect the boot cycle at the optimum time.
PAGE 285
SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU Both alternator ammeters should be monitored whenever the deice equipment is in use. An excessive indication shows an excessive electrical load, which may cause a battery discharging condition that could eventually lead to battery depletion. Nonessential electrical equipment should be turned off to correct or prevent this condition. Both alternator ammeters should be monitored whenever the deice equipment is in use.
PAGE 286
SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 5 - PERFORMANCE SECTION 5 - PERFORMANCE Climb speed should be increased to 130 knots when icing conditions are encountered during climb. Climb speed should be increased to 130 knots when icing conditions are encountered during climb. Cruise speeds are reduced approximately 5 knots when the surface boots are installed. Cruise speeds are reduced approximately 5 knots when the surface boots are installed.
PAGE 287
SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 6 - WEIGHT AND BALANCE SECTION 6 - WEIGHT AND BALANCE Factory installed optional equipment is included in the licensed weight and balance data in Section 6 of the Airplane Flight Manual. Factory installed optional equipment is included in the licensed weight and balance data in Section 6 of the Airplane Flight Manual.
PAGE 288
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 deice flow valves for approximately six seconds. The boot solenoid valves are activated and air pressure is released to the boots, sequentially inflating the surface deicers. A SURFACE DE-ICE indicator light, located on the annunciator panel illuminates when the boots inflate. When the cycle is complete, the deicer solenoid valves permit automatic overboard exhaustion of pressurized air.
PAGE 289
SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU ELECTRICALLY HEATED WINDSHIELD ELECTRICALLY HEATED WINDSHIELD The electrically heated left windshield is heated by current from the aircraft electrical system. It is controlled by WSHLD HI and WSHLD LO switches located on the switch panel. Circuit protection is provided by the windshield CONTROL and POWER circuit breakers in the ICE PROTECTION section of pilot’s aft circuit breaker panel.
PAGE 290
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 HEATED PITOT HEAD HEATED PITOT HEAD A heated AN type head is installed under the the wing. It is controlled by an ON-OFF type PITOT HEAT switch located on the switch panel and is protected by a PITOT HEAT circuit breaker located in the ICE PROTECTION section of the pilot's aft circuit breaker panel. A heated AN type head is installed under the the wing.
PAGE 291
SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU Y L N O E C N E HT R E LIG F E F R R R O FO T F NO DEICE SWITCH PANEL Figure 7-1 DEICE SWITCH PANEL Figure 7-1 REPORT: VB-1710 9-28, 14 of 16 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 9-28, 14 of 16 ISSUED: FEBRUARY 23, 1999
PAGE 292
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 3 SECTION 9 SUPPLEMENT 3 PA-46-350P, MALIBU Y L N O E C N E HT R E LIG F E F R R R O FO T F NO MAIN SWITCH PANEL (OVERHEAD LEFT & RIGHT) Figure 7-2 ISSUED: FEBRUARY 23, 1999 MAIN SWITCH PANEL (OVERHEAD LEFT & RIGHT) Figure 7-2 REPORT: VB-1710 15 of 16, 9-29 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 15 of 16, 9-29
PAGE 293
SECTION 9 SUPPLEMENT 4 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 4 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 4 SUPPLEMENT NO. 4 FOR FOR B.F. GOODRICH B.F. GOODRICH INTEGRATED ICE DETECTION SYSTEM INTEGRATED ICE DETECTION SYSTEM This supplement must be attached to the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual when the B.F.
PAGE 294
SECTION 9 SUPPLEMENT 4 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 4 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL This supplement supplies information necessary for the operation of the airplane when the B.F. Goodrich Integrated Ice Detection System is installed in accordance with FAA Approved Piper Data. This supplement supplies information necessary for the operation of the airplane when the B.F.
PAGE 295
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 4 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 4 IN FLIGHT (Cont’d) IN FLIGHT (Cont’d) If the ice is removed from the empennage following inflation, the “deice” annunciator will extinguish. If less than 90% of the ice cap located over the sensor within the right horizontal deicer has been removed, the select deice annunciator will remain illuminated.
PAGE 296
SECTION 9 SUPPLEMENT 4 PA-46-350P, MALIBU SECTION 5 - PERFORMANCE SECTION 9 SUPPLEMENT 4 PA-46-350P, MALIBU SECTION 5 - PERFORMANCE No change. No change. SECTION 6 - WEIGHT AND BALANCE SECTION 6 - WEIGHT AND BALANCE Factory installed optional equipment is included in the licensed weight and balance data in Section 6 of the Pilots Operating Handbook and Airplane Flight Manual.
PAGE 297
SECTION 9 SUPPLEMENT 5 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 5 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK PILOT’S OPERATING HANDBOOK SUPPLEMENT NO. 5 FOR KING 150 SERIES FLIGHT CONTROL SYSTEM SUPPLEMENT NO. 5 FOR KING 150 SERIES FLIGHT CONTROL SYSTEM This supplement has been DELETED as the FAA Approved Operational Supplement to the Bendix/King 150 Series Flight Control System as installed per STC SA1778CE-D. Bendix/King is responsible to supply and revise the operational supplement.
PAGE 298
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 6 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 6 PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 6 FOR KING KAS 297B VERTICAL SPEED AND ALTITUDE SELECTOR SUPPLEMENT NO.
PAGE 299
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 7 SECTION 9 SUPPLEMENT 7 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT 7 FOR 3M (SERIES II) STORMSCOPE, WX-1000/WX-1000+ SUPPLEMENT 7 FOR 3M (SERIES II) STORMSCOPE, WX-1000/WX-1000+ This supplement must be attached to the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual when the optional WX1000/WX-1000+ Stormscope System is in
PAGE 300
SECTION 9 SUPPLEMENT 7 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 7 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL This supplement supplies information necessary for the operation of the airplane when the optional WX-1000 or WX-1000+ Stormscope system is installed in accordance with FAA Approved Piper data.
PAGE 301
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 7 SECTION 5 - PERFORMANCE PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 7 SECTION 5 - PERFORMANCE No change. No change. SECTION 6 - WEIGHT AND BALANCE SECTION 6 - WEIGHT AND BALANCE Factory installed optional equipment is included in the licensed weight and balance data in the Equipment List attached to the Pilot’s Operating Handbook.
PAGE 302
SECTION 9 SUPPLEMENT 7 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 7 PA-46-350P, MALIBU Y L N O E C N E HT R E LIG F E F R R R O FO T F NO WX-1000 STORMSCOPE Figure 7-1 REPORT: VB-1710 9-42, 4 of 4 ISSUED: FEBRUARY 23, 1999 WX-1000 STORMSCOPE Figure 7-1 REPORT: VB-1710 9-42, 4 of 4 ISSUED: FEBRUARY 23, 1999
PAGE 303
SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 8 FOR BENDIX/KING EHI 40 SUPPLEMENT NO. 8 FOR BENDIX/KING EHI 40 This supplement must be attached to the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual when the optional Bendix/King EHI 40 EHSI system is installed per approved Piper drawings.
PAGE 304
SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL This supplement describes the components and operation of, and operational procedures for the Bendix/King EHI 40 Electronic Horizontal Situation Indicator (EHSI). The EHI 40 system utilizes the ED 461 display unit for display and control of navigation data and sensor selection.
PAGE 305
SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 1 - GENERAL (Continued) NAV NM RNAV STBY TST VAR VOR PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 SECTION 1 - GENERAL (Continued) Navigation Nautical Miles Area Navigation Standby Test Variation Very High Frequency Omni Range NAV NM RNAV STBY TST VAR VOR Navigation Nautical Miles Area Navigation Standby Test Variation Very High Frequency Omni Range SECTION 2 - LIMITATIONS SECTION 2 - LIMITATIONS When installed in conjunction with navigation receivers
PAGE 306
SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 3 - EMERGENCY PROCEDURES SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 3 - EMERGENCY PROCEDURES CAUTION CAUTION Following failure of a red gun in a display tube, red warning flags will not be visible. Following failure of a red gun in a display tube, red warning flags will not be visible. SMALL RED SG ANNUNCIATION SMALL RED SG ANNUNCIATION Small red SG annunciation indicates an internal self-test failure.
PAGE 307
SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 3 - EMERGENCY PROCEDURES (continued) SECTION 3 - EMERGENCY PROCEDURES (continued) RED HDG ANNUNCIATION RED HDG ANNUNCIATION Red HDG annunciation indicates a failure in the compass system by removing the lubber line and replacing it with a red HDG flag. Simultaneously, the course pointer head and tail will declutter leaving the d-bar.
PAGE 308
SECTION 9 SUPPLEMENTM 8 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 3 - EMERGENCY PROCEDURES (continued) SECTION 3 - EMERGENCY PROCEDURES (continued) HEADING OR COURSE KNOB FAILURE HEADING OR COURSE KNOB FAILURE Red flags will appear on the heading bug, or on the head and tail of the course pointer as appropriate. Autopilot will not couple HDG, NAV, or APR, but can be used for attitude or altitude hold.
PAGE 309
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 SECTION 3 - EMERGENCY PROCEDURES (continued) SECTION 3 - EMERGENCY PROCEDURES (continued) YELLOW DU ANNUNCIATION YELLOW DU ANNUNCIATION Yellow DU annunciation indicates a failure of the EHSI cooling fan. If a fan failure occurs in flight, monitor the display presentation for an abnormal appearance which will indicate impending failure. System heating can be reduced by lowering the brightness of the presentation.
PAGE 310
SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES (continued) SECTION 4 - NORMAL PROCEDURES (continued) INFLIGHT OPERATION INFLIGHT OPERATION CAUTION CAUTION Make transition from HSI presentations to conventional CDI presentations (MAP format) with caution. CDI left-right deviation may appear reversed when traveling outbound on a TO indication or inbound on a FROM indication.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 SECTION 5 - PERFORMANCE PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 SECTION 5 - PERFORMANCE No changes. No changes. SECTION 6 - WEIGHT AND BALANCE SECTION 6 - WEIGHT AND BALANCE Factory installed optional equipment is included in the licensed weight and balance data in Section 6 of the Pilot's Operating Handbook. Factory installed optional equipment is included in the licensed weight and balance data in Section 6 of the Pilot's Operating Handbook.
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) SECTION 7 - DESCRIPTION AND OPERATION (Continued) OPERATING CONTROLS OPERATING CONTROLS Figures 7-1 illustrates all operating controls for the EHI 40 systems. This figure may be referred to as the controls are in the following paragraphs. Figures 7-1 illustrates all operating controls for the EHI 40 systems.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 SECTION 7 - DESCRIPTION AND OPERATION (Continued) 3. NUMBER 1 SYSTEM BEARING POINTER SELECT - The bearing pointer select button works similar to the NAV sensor select button. A press of the bearing pointer button sequentially selects the next available sensor for display. The bearing pointer select list contains only those sensors which are associated with the bearing.
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) 5. ARC SECTORED MODE SELECTION - The ARC mode provides the pilot a large scale view of the CDI by presenting an approximate 85 degree sector display of the compass. SECTION 9 SUPPLEMENT 8 SECTION 7 - DESCRIPTION AND OPERATION (Continued) 5. ARC SECTORED MODE SELECTION - The ARC mode provides the pilot a large scale view of the CDI by presenting an approximate 85 degree sector display of the compass.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 SECTION 7 - DESCRIPTION AND OPERATION (Continued) 7. 8. RANGE SELECTION PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) 7. RANGE SELECTION RANGE DOWN - A press of the RANGE DOWN button selects the next lower range to be displayed while in the NAV MAP mode of operation. Once the lowest selectable range is reached, the RANGE UP button must be used for a range change.
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) 10. HEADING SELECT KNOB - Rotation of the HEADING SELECT knob allows the heading bug on the EHSI to be rotated to the desired heading. 10. HEADING SELECT KNOB - Rotation of the HEADING SELECT knob allows the heading bug on the EHSI to be rotated to the desired heading. The ED 461 provides a HEADING SYNC feature.
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU Y L N O E C N E HT R E LIG F E F R R R O FO T F NO ED 461 EHI CONTROLS Figure 7-1 ED 461 EHI CONTROLS Figure 7-1 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 15 of 26 9-57 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 15 of 26 9-57
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) SECTION 7 - DESCRIPTION AND OPERATION (Continued) EHSI DISPLAYS EHSI DISPLAYS Standard EHI 40 displays, which may be referred to as key points of the display, are discussed in the following paragraphs (refer to figure 7-5): Standard EHI 40 displays, which may be referred to as key points of the display, are discussed in the following paragraphs (refer to figure 7-5):
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 SECTION 7 - DESCRIPTION AND OPERATION (Continued) 4. 5. Heading Select Bug PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 SECTION 7 - DESCRIPTION AND OPERATION (Continued) 4. Heading Select Bug A notched orange heading bug is manually rotated around the compass scale by the heading select knob on the control panel. A digital readout of the selected heading is displayed in the lower right hand corner. Once set, the heading bug rotates with the compass card.
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) 7. SECTION 9 SUPPLEMENT 8 SECTION 7 - DESCRIPTION AND OPERATION (Continued) Course Deviation Scale (continued) 7.
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) 9. Distance and Ground Speed Display (continued) SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) 9. Distance and Ground Speed Display (continued) When the selected bearing pointer source has DME data associated with it, the distance information will be displayed below the bearing pointer source annunciator.
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) 11. Bearing Pointer Display - The rotating blue single bar #1 RMI Pointer points in the direction of the selected sensor ground station or waypoint. 11. Bearing Pointer Display - The rotating blue single bar #1 RMI Pointer points in the direction of the selected sensor ground station or waypoint.
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) Y L N O E C N E HT R E LIG F E F R R R O FO T F NO ED 461 DISPLAY UNIT Figure 7-5 ISSUED: FEBRUARY 23, 1999 ED 461 DISPLAY UNIT Figure 7-5 REPORT: VB-1710 21 of 26 9-63 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 21 of 26 9-63
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) Y L N O E C N E HT R E LIG F E F R R R O FO T F NO ED 461 DISPLAY UNIT Figure 7-5 (cont) ED 461 DISPLAY UNIT Figure 7-5 (cont) REPORT: VB-1710 9-64 22 of 26 ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 9-64 22 of 26 ISSUED: FEBRUARY 23, 1999
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) SECTION 7 - DESCRIPTION AND OPERATION (Continued) MAP DISPLAY (refer to figure 7-7) MAP DISPLAY (refer to figure 7-7) The EHI 40 provides two basic types of map; a 360 degree map display about the aircraft and an approximately 85 degree sectored map display in front of the aircraft. Options to be displayed on the map include waypoints and navaids.
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) 4. Course Deviation Display - The stationary white deviation scale along the bottom of display provides reference for the course deviation bar to indicate position of airplane in relation to selected navigation course.
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) 9. MAP Weather Radar Information - Four data lines are reserved below the primary NAV sensor source annunciator to display radar informaion. SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) 9. MAP Weather Radar Information - Four data lines are reserved below the primary NAV sensor source annunciator to display radar informaion.
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SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 8 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) SECTION 7 - DESCRIPTION AND OPERATION (Continued) ARC (EXPANDED) EHSI DISPLAY (refer to figure 7-9) ARC (EXPANDED) EHSI DISPLAY (refer to figure 7-9) The expanded (ARC) format provides an enlarged display for increased resolution to NAV data due to the enlarged compass scale presentations.
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SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 9 FOR BENDIX/KING RDR 2000 VERTICAL PROFILE WEATHER RADAR SYSTEM SUPPLEMENT NO.
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SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL This supplement supplies information necessary for the operation of the airplane when the optional Bendix/King RDR 2000 Vertical Profile Weather Radar System is installed in accordance with FAA Approved Piper data.
PAGE 331
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 9 SECTION 5 - PERFORMANCE PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 9 SECTION 5 - PERFORMANCE When the radar pod is installed: When the radar pod is installed: a. b. c. a. b. c. The rate of climb is decreased approximately 50 fpm. The cruise speed is decreased approximately 2 knots. The cruise range is decreased approximately 1% due to the decrease in cruise speed. The rate of climb is decreased approximately 50 fpm.
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SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU Operation and Controls SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU Operation and Controls Y L N RDR 2000 CONTROLS AND INDICATOR Figure 7-1 REPORT: VB-1710 9-72 4 of 10 ISSUED: FEBRUARY 23, 1999 O E C N E HT R E LIG F E F R R R O FO T F RDRO AND INDICATOR N 2000 CONTROLS Figure 7-1 REPORT: VB-1710 9-72 4 of 10 ISSUED: FEBRUARY 23, 1999
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 9 SECTION 9 SUPPLEMENT 9 Operation and Controls (cont.) Operation and Controls (cont.) CONTROL/ DISPLAY PA-46-350P, MALIBU FUNCTION CONTROL/ DISPLAY FUNCTION BRT Control Adjusts brightness of the display for varying cockpit light conditions. BRT Control Adjusts brightness of the display for varying cockpit light conditions. Wx/Wxa Button When pressed, alternately selects between the Wx (weather) and Wxa (weather alert) modes of operation.
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SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU Operation and Controls (cont.) CONTROL/ DISPLAY SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU Operation and Controls (cont.) FUNCTION CONTROL/ DISPLAY FUNCTION GAIN Control Knob Manual gain control becomes active only when ground-mapping (MAP) is selected. Gain is internally set in all other modes. GAIN Control Knob Manual gain control becomes active only when ground-mapping (MAP) is selected. Gain is internally set in all other modes.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 9 FUNCTION Radar Function Selector Switch (cont.) 5. OFF position removes primary power from the radar indicator and the sensor. The antenna is parked in the down position. RNG Selector Button When pressed clears the display and advances the indicator to the next higher range. Selected range is displayed in upper right corner of the last range mark (Figure 7-1) and distance to other range rings is displayed along the right edge.
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SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU Operation and Controls (cont.) CONTROL/ DISPLAY FUNCTION 2. Continuously holding the TRK button will result in the system slicing in twodegree increments. REPORT: VB-1710 9-76 8 of 10 PA-46-350P, MALIBU Operation and Controls (cont.) 1. Prior to engaging VP, the appropriate button (left or right) is used to place the track line at the desired azimuth angle to be vertically scanned (sliced).
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 9 Operation and Controls (cont.) Operation and Controls (cont.) Y L N 1. Vertical PROFILE mode annunciation 2. Left or right track annunciation. O E C N E HT R E LIG F E F R R R O VERTICAL PROFILE MODE (RDR 2000 FO T F Figure 7-3 OPROFILE mode annunciation 1. Vertical N 2. Left or right track annunciation. 3. Degrees of track left or right of aircraft nose. 3. Degrees of track left or right of aircraft nose. 4.
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SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU Operation and Controls (cont.) SECTION 9 SUPPLEMENT 9 PA-46-350P, MALIBU Operation and Controls (cont.) Y L N TEST PATTERN Figure 7-5 Detail description on the function and use of the various controls and displays are outlined in the Bendix/King RDR 2000 Vertical Profile Weather Radar System Pilot's Guide, P/N 006-08755-0000, latest revision.
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SECTION 9 SUPPLEMENT 10 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 10 PA-46-350P, MALIBU PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT 10 FOR ARGUS 7000CE MOVING MAP DISPLAY SUPPLEMENT 10 FOR ARGUS 7000CE MOVING MAP DISPLAY This supplement must be attached to the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual when the optional Argus 7000CE Moving Map Display of Eventide, Inc.
PAGE 340
SECTION 9 SUPPLEMENT 10 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 10 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL This supplement supplies information necessary for the operation of the airplane when the optional Argus 7000CE Moving Map Display is installed. The display must be operated within the limitations herein specified. The information contained within this supplement is to be used in conjunction with the complete handbook.
PAGE 341
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 10 PA-46-350P, MALIBU conducting a precision approach to, or departure from, a landing facility. SECTION 9 SUPPLEMENT 10 conducting a precision approach to, or departure from, a landing facility. f. When using the ADF bearing pointer for navigation in the map and plan submode, the range must be limited to 40 nm or less, and the pointer must be discernible. f.
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SECTION 9 SUPPLEMENT 10 PA-46-350P, MALIBU SECTION 5 - PERFORMANCE SECTION 9 SUPPLEMENT 10 PA-46-350P, MALIBU SECTION 5 - PERFORMANCE No change. No change. SECTION 6 - WEIGHT AND BALANCE SECTION 6 - WEIGHT AND BALANCE Factory installed optional equipment is included in the licensed weight and balance data in the Equipment List attached to the Pilot's Operating Handbook.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 10 SECTION 7 - DESCRIPTION AND OPERATION (Continued) b. SECTION 9 SUPPLEMENT 10 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) (2) In addition, the Software Program VERsion will appear on the Disclaimer Page, which will remain in view until any functional push button is depressed. The current VERsion is 5.0.
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SECTION 9 SUPPLEMENT 10 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) SECTION 9 SUPPLEMENT 10 SECTION 7 - DESCRIPTION AND OPERATION (Continued) 40 nm to 1 nm distance to the destination waypoint. All other navigation information is similar to that of the DEParture and ENRoute modes. Orientation and direction of flight of the moving arrow or symbolic aircraft is with respect to Gyroscopic Directional HSI heading, or GPS computed track. c. SELect and INFOrmation Procedures.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 10 SECTION 7 - DESCRIPTION AND OPERATION (Continued) d. ADF Bearing Pointer and Digital ADF Bearing Procedures. SECTION 9 SUPPLEMENT 10 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (Continued) d. ADF Bearing Pointer and Digital ADF Bearing Procedures. (1) In the DEParture or ENRoute modes, when ADF is selected, the bearing pointer and/or tail will appear on the perimeter of the Compass Rose.
PAGE 346
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 11 SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 11 FOR BENDIX/KING KLN 90B GPS NAVIGATION SYSTEM WITH KAP/KFC 150 or 225 AUTOPILOT SYSTEMS SUPPLEMENT NO.
PAGE 347
SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL The KLN 90B GPS panel mounted unit contains the GPS sensor, the navigation computer, a CRT display, and all controls required to operate the unit. It also houses the data base cartridge which plugs directly into the back of the unit.
PAGE 348
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 11 SECTION 2 - LIMITATIONS SECTION 2 - LIMITATIONS A. The KLN 90B GPS Pilot’s Guide, P/N 006-08773-0000, dated December, 1994 (or later applicable revision) must be immediately available to the flight crew whenever navigation is predicated on the use of the system. The Operational Revision Status (ORS) of the Pilot’s Guide must match the ORS level annunciated on the Self Test page. A.
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SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU SECTION 3 - EMERGENCY PROCEDURES ABNORMAL PROCEDURES SECTION 3 - EMERGENCY PROCEDURES ABNORMAL PROCEDURES A. If the KLN 90B GPS information is not available or invalid, utilize remaining operational navigation equipment as required. B. If a “RAIM NOT AVAILABLE” message is displayed while conducting an instrument approach, terminate the approach. Execute a missed approach if required. C.
PAGE 350
SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES (CONT'D) 3. SECTION 4 - NORMAL PROCEDURES (CONT'D) Waypoint (WPT) annunciator - Prior to reaching a waypoint in the active flight plan, the KLN 90B GPS will provide navigation along a curved path segment to ensure a smooth transition between two adjacent legs in the flight plan. This feature is called turn anticipation.
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SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES (CONT'D) SECTION 9 SUPPLEMENT 11 SECTION 4 - NORMAL PROCEDURES (CONT'D) NOTE Manual HSI course centering in OBS using the control knob can be difficult, especially at long distances. Centering the dbar can best be accomplished by pressing [ D ] and then manually setting the HSI pointer to the course value prescribed in the KLN 90B displayed message. 6. 7. C.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES (CONT'D) SECTION 4 - NORMAL PROCEDURES (CONT'D) E. E. APPROACH MODE SEQUENCING AND RAIM PREDICTION SECTION 9 SUPPLEMENT 11 APPROACH MODE SEQUENCING AND RAIM PREDICTION NOTE The special use airspace alert will automatically be disabled prior to flying an instrument approach to reduce the potential for message congestion.
PAGE 353
SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES (CONT'D) 4. Select Super NAV 5 page to fly the approach procedure. a. SECTION 9 SUPPLEMENT 11 SECTION 4 - NORMAL PROCEDURES (CONT'D) 4. If receiving radar vectors, or need to fly a procedure turn or holding pattern, fly in OBS until inbound to the FAF. Select Super NAV 5 page to fly the approach procedure. a. NOTE: OBS navigation is TO-FROM (like a VOR) without waypoint sequencing. b.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 11 SECTION 4 - NORMAL PROCEDURES (CONT'D) PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 11 SECTION 4 - NORMAL PROCEDURES (CONT'D) 8. Missed Approach: a, Climb b. Navigate to the MAP (in APR ARM if APR ACTV is not available). NOTE: There is no automatic LEG sequencing at the MAP. c. After climbing in accordance with the published missed approach procedure, press [ D ], verify or change the desired holding fix and press ENT.
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SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES (CONT'D) SECTION 9 SUPPLEMENT 11 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES (CONT'D) • Waypoint suffixes in the flight plan: • Waypoint suffixes in the flight plan: i - IAF f - FAF m - MAP h - missed approach holding fix. i - IAF f - FAF m - MAP h - missed approach holding fix.
PAGE 356
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 11 SECTION 4 - NORMAL PROCEDURES (CONT'D PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES (CONT'D • APR ARM to APR ACTV is automatic provided: • APR ARM to APR ACTV is automatic provided: a. You are in APR ARM (normally automatic). b. You are in LEG model! c. The FAF is the active ; waypoint d. Within 2 n.m. of the FAF. e. Outside of the FAF. f. Inbound to the FAF. g. RAIM is available. a. You are in APR ARM (normally automatic). b. You are in LEG model! c.
PAGE 357
SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 12 FOR BENDIX/KING KX 155A COMM/NAV SYSTEM SUPPLEMENT NO.
PAGE 358
SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU SECTION 1 GENERAL SECTION 1 GENERAL This supplement supplies information necessary for the operation of the airplane when the Bendix/King KX 155A Comm/Nav System is installed in accordance with FAA approved Piper data. This supplement supplies information necessary for the operation of the airplane when the Bendix/King KX 155A Comm/Nav System is installed in accordance with FAA approved Piper data.
PAGE 359
SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 12 SECTION 7 DESCRIPTION & OPERATION SECTION 7 DESCRIPTION & OPERATION GENERAL GENERAL All controls required to operate the KX 155A/165A are located on the unit front panel. (See Figure 3-1.) All controls required to operate the KX 155A/165A are located on the unit front panel. (See Figure 3-1.) Y L N FIGURE 3-1 KX 155A CONTROL FUNCTIONS COMM TRANSCEIVER Rotate the VOL knob clockwise from the OFF position.
PAGE 360
SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU COMM TRANSCEIVER (CONT'D) COMM TRANSCEIVER (CONT'D) The outer knob will change the MHz portion of the standby display. At one band-edge (118 or 136 MHz) the following 1 MHz change will wrap around to the other band-edge. The inner knob will change the kHz portion of the standby display. It will change in steps of 50 kHz when the knob is pushed in, and 25 kHz when the knob is pulled out. For 8.
PAGE 361
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 12 The KX 155A also has provision to program 32 channels. Pressing the CHAN button for 2 or more seconds will cause the unit to enter the channel program mode. Upon entering the channel program mode,”PG” is displayed next to the channel number and the channel number will flash indicating that it can be programmed. The desired channel can be selected by turning the comm kHz knob.
PAGE 362
SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU NAV RECEIVER (CONT'D) NAV RECEIVER (CONT'D) The inner knob operates in 50 kHz steps. The NAV receiver’s lower and upper frequency limits are 108.00 MHz and 117.95 MHz. Exceeding the upper limit of frequency band will automatically return to the lower limit and vice versa. The inner knob operates in 50 kHz steps. The NAV receiver’s lower and upper frequency limits are 108.00 MHz and 117.95 MHz.
PAGE 363
SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU FIGURE 3-3 NAV DISPLAY; ACTIVE LOCALIZER FREQUENCY/CDI FORMAT When the received signal is too weak to ensure accuracy the display will “flag”. See Figure 3-4. FIGURE 3-4 VOR FLAG DISPLAY ISSUED: FEBRUARY 23, 1999 REPORT: VB-1710 7 of 12, 9-105 SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU FIGURE 3-3 NAV DISPLAY; ACTIVE LOCALIZER FREQUENCY/CDI FORMAT Y L N When the received signal is too weak to ensure accuracy the display will “flag”. See Figure 3-4.
PAGE 364
SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU NAV RECEIVER (CONT'D) NAV RECEIVER (CONT'D) Depressing the mode button will cause the NAV display to go from the ACTIVE/CDI format to the ACTIVE/BEARING format.
PAGE 365
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 12 Another push of the mode button will cause the NAV display to go from the ACTIVE/BEARING format to the ACTIVE/RADIAL format as shown in Figure 3-7. In the RADIAL mode, the increment/decrement knob channels the ACTIVE frequency window and depressing the frequency transfer button will cause the ACTIVE frequency to be placed in blind storage and the STANDBY frequency (in blind storage) to be displayed in the ACTIVE window display.
PAGE 366
SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU NAV RECEIVER (CONT'D) NAV RECEIVER (CONT'D) Another push of the mode button will cause the unit to go into the TIMER mode. See Figure 3-9. When the unit is turned on the elapsed timer begins counting upwards from zero. The timer can be stopped and reset to zero by pushing the NAV frequency transfer button for 2 seconds or more causing the ET on the display to flash.
PAGE 367
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 12 SECTION 9 SUPPLEMENT 12 PA-46-350P, MALIBU PILOT CONFIGURATION PILOT CONFIGURATION This mode can be accessed by pressing and holding the Nav Mode Button for more than 2 seconds and then pressing the Nav Frequency Transfer Button for an additional 2 seconds, while continuing to hold the Nav Mode Button. When the Pilot Config Mode is entered the unit will show the “SWRV” mnemonic which is the unit software revision level.
PAGE 368
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 13 SECTION 9 SUPPLEMENT 13 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK PILOT’S OPERATING HANDBOOK SUPPLEMENT NO. 13 FOR PRECISE FLIGHT SPEEDBRAKE 2000 SUPPLEMENT NO. 13 FOR PRECISE FLIGHT SPEEDBRAKE 2000 This supplement has been DELETED as the FAA Approved Operational Supplement to the Precise Flight SPEEDBRAKE2000 System as installed in this aircraft per STC SA00520SE. Precise Flight Inc. is responsible to supply and revise the operational supplement.
PAGE 369
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 14 SECTION 9 SUPPLEMENT 14 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK PILOT’S OPERATING HANDBOOK SUPPLEMENT NO. 14 FOR BENDIX/KING KFC 225 FLIGHT CONTROL SYSTEM SUPPLEMENT NO. 14 FOR BENDIX/KING KFC 225 FLIGHT CONTROL SYSTEM This supplement has been DELETED as the FAA Approved Operational Supplement to the Bendix/King KFC 225 Series Flight Control System as installed per STC SA00656WI-D.
PAGE 370
SECTION 9 SUPPLEMENT 15 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 15 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 15 FOR GARMIN GNS 430 VHF COMMUNICATION TRANSCEIVER/VOR/ILS RECEIVER/GPS RECEIVER SUPPLEMENT NO.
PAGE 371
SECTION 9 SUPPLEMENT 15 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 15 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL The GNS 430 System is a fully integrated, panel mounted instrument, which contains a VHF Communications Transceiver, a VOR/ILS receiver, and a Global Positioning System (GPS) Navigation computer. The system consists of a GPS antenna, GPS receiver, VHF VOR/LOC/GS antenna, VOR/lLS receiver, VHF COMM antenna and a VHF Communications transceiver.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 15 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 15 SECTION 2 - LIMITATIONS SECTION 2 - LIMITATIONS A. The GARMIN GNS 430 Pilot’s Guide, p/n 190-00140-00, Rev. A, dated October 1998, or later appropriate revision, must be immediately available to the flight crew whenever navigation is predicated on the use of the system. A. The GARMIN GNS 430 Pilot’s Guide, p/n 190-00140-00, Rev.
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SECTION 9 SUPPLEMENT 15 PA-46-350P, MALIBU SECTION 2 - LIMITATIONS (continued) E. SECTION 9 SUPPLEMENT 15 PA-46-350P, MALIBU SECTION 2 - LIMITATIONS (continued) 2. Accomplishment of ILS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved for GPS overlay with the GNS 430’s GPS receiver is not authorized. 2. Accomplishment of ILS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved for GPS overlay with the GNS 430’s GPS receiver is not authorized. 3.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 15 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 15 SECTION 3 - EMERGENCY PROCEDURES SECTION 3 - EMERGENCY PROCEDURES ABNORMAL PROCEDURES ABNORMAL PROCEDURES A. If GARMIN GNS 430 navigation information is not available or invalid, utilize remaining operational navigation equipment as required. A. If GARMIN GNS 430 navigation information is not available or invalid, utilize remaining operational navigation equipment as required. B.
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SECTION 9 SUPPLEMENT 15 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES SECTION 9 SUPPLEMENT 15 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES WARNING WARNING Familiarity with the enroute operation of the GNS 430 does not constitute proficiency in approach operations. Do not attempt approach operations in IMC prior to attaining proficiency in the use of the GNS 430 approach feature. Familiarity with the enroute operation of the GNS 430 does not constitute proficiency in approach operations.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 15 SECTION 5 - PERFORMANCE SECTION 9 SUPPLEMENT 15 PA-46-350P, MALIBU SECTION 5 - PERFORMANCE No change. No change. SECTION 6 - WEIGHT AND BALANCE SECTION 6 - WEIGHT AND BALANCE Factory installed optional equipment is included in the licensed weight and balance data in Section 6 of the basic Pilot’s Operating Handbook.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 16 SECTION 9 SUPPLEMENT 16 PA-46-350P, MALIBU PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 16 FOR S-TEC SYSTEM 55 TWO AXIS AUTOMATIC FLIGHT GUIDANCE SYSTEM WITH TRIM MONITOR SUPPLEMENT NO.
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SECTION 9 SUPPLEMENT 17 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 17 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 17 FOR GARMIN GNS 530 VHF COMMUNICATION TRANSCEIVER/VOR/ILS RECEIVER/GPS RECEIVER SUPPLEMENT NO.
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SECTION 9 SUPPLEMENT 17 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 17 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL The GNS 530 System is a fully integrated, panel mounted instrument, which contains a VHF Communications Transceiver, a VOR/ILS Receiver, and a Global Positioning System (GPS) Navigation computer. The system consists of a GPS Antenna, GPS Receiver, VHF VOR/LOC/GS Antenna, VOR/ILS Receiver, VHF COMM Antenna and a VHF Communications Transceiver.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 17 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 17 SECTION 2 - LIMITATIONS SECTION 2 - LIMITATIONS A. The GARMIN GNS 530 Pilot’s Guide, p/n 190-00181-00, Rev. A, dated November 1999, or later appropriate revision, must be immediately available to the flight crew whenever navigation is predicated on the use of the system. A. The GARMIN GNS 530 Pilot’s Guide, p/n 190-00181-00, Rev.
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SECTION 9 SUPPLEMENT 17 PA-46-350P, MALIBU SECTION 2 - LIMITATIONS (continued) F. SECTION 9 SUPPLEMENT 17 PA-46-350P, MALIBU SECTION 2 - LIMITATIONS (continued) 2. Accomplishment of ILS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved for GPS overlay with the GNS 530’s GPS receiver is not authorized. 2. Accomplishment of ILS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved for GPS overlay with the GNS 530’s GPS receiver is not authorized. 3.
PAGE 382
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 17 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 17 SECTION 3 - EMERGENCY PROCEDURES SECTION 3 - EMERGENCY PROCEDURES ABNORMAL PROCEDURES ABNORMAL PROCEDURES A. If GARMIN GNS 530 navigation information is not available or invalid, utilize remaining operational navigation equipment as required. A. If GARMIN GNS 530 navigation information is not available or invalid, utilize remaining operational navigation equipment as required. B.
PAGE 383
SECTION 9 SUPPLEMENT 17 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES WARNING Familiarity with the enroute operation of the GNS 530 does not constitute proficiency in approach operations. Do not attempt approach operations in IMC prior to attaining proficiency in the use of the GNS 530 approach features. A. DETAILED OPERATING PROCEDURES Normal operating procedures are described in the GARMIN GNS 530 Pilot’s Guide, p/n 190-00181-00, Rev. A, dated November 1999, or later appropriate revision.
PAGE 384
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 17 SECTION 9 SUPPLEMENT 17 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES (continued) SECTION 4 - NORMAL PROCEDURES (continued) E. AUTOMATIC LOCALIZER COURSE CAPTURE E. AUTOMATIC LOCALIZER COURSE CAPTURE By default, the GNS 530 automatic localizer course capture feature is enabled.
PAGE 385
SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 18 FOR GARMIN GTX 327 TRANSPONDER SUPPLEMENT NO. 18 FOR GARMIN GTX 327 TRANSPONDER This supplement must be attached to the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual when the Garmin GTX 327 Transponder is installed per the Equipment List.
PAGE 386
SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL This supplement supplies information necessary for the operation of the airplane when the Garmin GTX 327 Transponder is installed in accordance with FAA approved Piper data. This supplement supplies information necessary for the operation of the airplane when the Garmin GTX 327 Transponder is installed in accordance with FAA approved Piper data.
PAGE 387
SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES SECTION 4 - NORMAL PROCEDURES BEFORE TAKEOFF: BEFORE TAKEOFF: • To transmit Mode C (Altitude Reporting) code in flight: • To transmit Mode C (Altitude Reporting) code in flight: • Mode Selection Key - ALT • Code Selector Keys - SELECT assigned code. • Mode Selection Key - ALT • Code Selector Keys - SELECT assigned code.
PAGE 388
SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION SECTION 7 - DESCRIPTION AND OPERATION The GTX 327 transponder is powered on by pressing the STBY, ALT or ON keys, or by a remote avionics master switch (if applicable). After power on, a start-up page will be displayed while the unit performs a self test.
PAGE 389
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 18 SECTION 7 - DESCRIPTION AND OPERATION (continued) SECTION 7 - DESCRIPTION AND OPERATION (continued) GTX 327 Configuration Mode (continued) GTX 327 Configuration Mode (continued) To use the GTX 327 Configuration Mode: 1. Press and hold the FUNC key while powering on the unit using the STBY, ON, or ALT key (or using an avionics master switch). 2. Press the FUNC key to sequence through the configuration pages. 3.
PAGE 390
SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (continued) SECTION 7 - DESCRIPTION AND OPERATION (continued) Code Selection (continued) Code Selection (continued) Important Codes: 1200 - The VFR code for any altitude in the US (Refer to ICAO standards elsewhere) 7000 - The VFR code commonly used in Europe (Refer to ICAO standards) 7500 - Hijack code (Aircraft is subject to unlawful interference) 7600 - Loss of communication
PAGE 391
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 18 SECTION 7 - DESCRIPTION AND OPERATION (continued) Keys for Other GTX 327 Functions (continued) PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 18 SECTION 7 - DESCRIPTION AND OPERATION (continued) Keys for Other GTX 327 Functions (continued) PRESSURE ALT: Displays the altitude data supplied to the GTX 327 in feet, hundreds of feet (i.e., flight level), or meters, depending on configuration.
PAGE 392
SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (continued) Altitude Trend Indicator SECTION 7 - DESCRIPTION AND OPERATION (continued) Altitude Trend Indicator When the “PRESSURE ALT” page is displayed, an arrow may be displayed to the right of the altitude, indicating that the altitude is increasing or decreasing. One of two sizes of arrows may be displayed depending on the rate of climb/descent.
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PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 18 SECTION 9 SUPPLEMENT 18 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (continued) Automatic ALT/STBY Mode Switching SECTION 7 - DESCRIPTION AND OPERATION (continued) Automatic ALT/STBY Mode Switching If the GTX 327 is configured for automatic standby switching, the mode will automatically change to ALT when a squat switch senses that the aircraft has become airborne.
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SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 19 SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 19 PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 19 FOR AVIDYNE 5RR-MFC-SERIES FLIGHTMAX FLIGHT SITUATION DISPLAY SUPPLEMENT NO.
PAGE 395
SECTION 9 SUPPLEMENT 19 SECTION 9 PA-46-350P, MALIBU SECTION 1 - GENERAL SUPPLEMENT 19 PA-46-350P, MALIBU SECTION 1 - GENERAL NOTE FlightMax 700 FSD is a radar indicator only and does not have functionality for Navigator, Lightning, Charts, or Traffic. The FlightMax 700 FSD is a radar indicator only for the RDR-2000 Vertical Profile Weather Radar System. NOTE FlightMax 700 FSD is a radar indicator only and does not have functionality for Navigator, Lightning, Charts, or Traffic.
PAGE 396
SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 19 SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 19 SECTION 3 - EMERGENCY PROCEDURES SECTION 3 - EMERGENCY PROCEDURES There is no change to the aircraft emergency procedures with this equipment installed. There is no change to the aircraft emergency procedures with this equipment installed. SECTION 4 - NORMAL PROCEDURES SECTION 4 - NORMAL PROCEDURES Normal operating procedures for all FSD functions are shown in the FlightMax 700/750 Series User’s Manual, 600-0032.
PAGE 397
SECTION 9 SUPPLEMENT 19 SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 19 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED) SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED) AVIDYNE NAVIGATOR (FlightMax 750 FSD only) (continued) AVIDYNE NAVIGATOR (FlightMax 750 FSD only) (continued) Navigator displays real-time navigation data such as distance and bearing to waypoints and nearby airports, cross-track error against a planned route of flight, and estimated time of arrival at a destination.
PAGE 398
SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 19 SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 19 SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED) SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED) AVIDYNE LIGHTNING (FlightMax 750 FSD only) AVIDYNE LIGHTNING (FlightMax 750 FSD only) Avidyne Lightning displays weather avoidance data gathered by an airborne thunderstorm sensor, the BF Goodrich Avionics Systems Stormscope® WX-500 Weather Mapping System.
PAGE 399
SECTION 9 SECTION 9 SUPPLEMENT 19 PA-46-350P, MALIBU SUPPLEMENT 19 PA-46-350P, MALIBU SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED) SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED) AVIDYNE CHARTS (FlightMax 750 FSD only) AVIDYNE CHARTS (FlightMax 750 FSD only) Avidyne Charts is a moving map display. Interfacing with an onboard, external GPS, Avidyne Charts shows aircraft position on the 3 by 4 inch display. Avidyne Charts gives access to digitized versions of VFR and IFR ENROUTE charts.
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SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 19 SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 19 SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED) SECTION 7 - DESCRIPTION AND OPERATION (CONTINUED) DATABASE UPDATES DATABASE UPDATES Avidyne Navigator is intended for use as an enhanced human interface to a variety of certified GPS receivers. As with certified receivers, the database of Avidyne Navigator is a critical component and must be kept current.
PAGE 401
SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 20 SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 20 PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 20 FOR B.F. GOODRICH SKYWATCH TRAFFIC ADVISORY SYSTEM MODEL SKY497 SUPPLEMENT NO. 20 FOR B.F.
PAGE 402
SECTION 9 SUPPLEMENT 20 SECTION 9 PA-46-350P, MALIBU SECTION 1 - GENERAL SUPPLEMENT 20 PA-46-350P, MALIBU SECTION 1 - GENERAL The SKYWATCH system is an on-board traffic advisory system which monitors a radius of nominally 6 nautical miles about the aircraft by interrogating any “intruding” aircraft transponder, and determines if a potential conflict exists with other aircraft.
PAGE 403
SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 20 SECTION 2 - LIMITATIONS SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 20 SECTION 2 - LIMITATIONS Information shown on the display is provided to the pilot as an aid to visually acquiring traffic. Pilot’s should maneuver their aircraft based only on ATC guidance or positive visual acquisition of the conflicting traffic. Maneuver should be consistent with ATC instructions. No maneuvers should be made based only on a Traffic Advisory.
PAGE 404
SECTION 9 SECTION 9 SUPPLEMENT 20 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES (continued) SUPPLEMENT 20 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES (continued) SELF TEST (continued) SELF TEST (continued) If “TRAFFIC ADVISORY SYSTEM TEST FAILED” is heard or the SKY497 FAILED screen appears, the SKYWATCH system should be turned OFF. If “TRAFFIC ADVISORY SYSTEM TEST FAILED” is heard or the SKY497 FAILED screen appears, the SKYWATCH system should be turned OFF.
PAGE 405
SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 20 SECTION 4 - NORMAL PROCEDURES (continued) SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 20 SECTION 4 - NORMAL PROCEDURES (continued) ABNORMAL PROCEDURES ABNORMAL PROCEDURES If “TRAFFIC ADVISORY SYSTEM TEST FAILED” is heard or the SKY497 FAILED screen appears, the SKYWATCH system should be turned OFF. If “TRAFFIC ADVISORY SYSTEM TEST FAILED” is heard or the SKY497 FAILED screen appears, the SKYWATCH system should be turned OFF.
PAGE 406
SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 21 SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 21 PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 21 FOR BF GOODRICH AEROSPACE WX-500 STORMSCOPE - SERIES II WEATHER MAPPING SENSOR SUPPLEMENT NO.
PAGE 407
SECTION 9 SECTION 9 SUPPLEMENT 21 PA-46-350P, MALIBU SUPPLEMENT 21 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL This supplement provides information necessary for the operation of the aircraft with the BF Goodrich WX-500 Stormscope. This supplement provides information necessary for the operation of the aircraft with the BF Goodrich WX-500 Stormscope. WARNING WARNING Never use your Stormscope system to attempt to penetrate a thunderstorm.
PAGE 408
SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 21 SECTION 9 PA-46-350P, MALIBU SUPPLEMENT 21 SECTION 4 - NORMAL PROCEDURES SECTION 4 - NORMAL PROCEDURES Normal operating procedures are described in the BF Goodrich Aerospace WX-500 Stormscope Users Guide, p/n 009-11501-001, Rev. A, dated September 10, 1997, or later appropriate revision. Normal operating procedures are described in the BF Goodrich Aerospace WX-500 Stormscope Users Guide, p/n 009-11501-001, Rev.
PAGE 409
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 22 SECTION 9 SUPPLEMENT 22 PA-46-350P, MALIBU PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 22 FOR MEGGITT ELECTRONIC FLIGHT DISPLAY SYSTEM (EFIS) INSTALLED ON A PIPER PA-46-350P (PILOT SIDE ONLY) SUPPLEMENT NO.
PAGE 410
PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 23 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 23 PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 23 FOR BENDIX/KING KMH 880 MULTI-HAZARD AWARENESS SYSTEM SUPPLEMENT NO.
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SECTION 9 SUPPLEMENT 24 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 24 PA-46-350P, MALIBU PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT NO. 24 FOR GARMIN GTX 330 TRANSPONDER SUPPLEMENT NO. 24 FOR GARMIN GTX 330 TRANSPONDER This supplement must be attached to the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual when the Garmin GTX 330 Transponder is installed per the Equipment List.
PAGE 412
SECTION 9 SUPPLEMENT 24 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 24 PA-46-350P, MALIBU SECTION 1 - GENERAL SECTION 1 - GENERAL This supplement supplies information necessary for the operation of the airplane when the Garmin GTX 330 Transponder is installed in accordance with FAA approved Piper data. This supplement supplies information necessary for the operation of the airplane when the Garmin GTX 330 Transponder is installed in accordance with FAA approved Piper data.
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SECTION 9 SUPPLEMENT 24 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 24 PA-46-350P, MALIBU SECTION 4 - NORMAL PROCEDURES SECTION 4 - NORMAL PROCEDURES BEFORE TAKEOFF: BEFORE TAKEOFF: To transmit Mode C (Altitude Reporting) code in flight: To transmit Mode C (Altitude Reporting) code in flight: • Mode Selection Key - ALT • Code Selector Keys - SELECT assigned code. • Mode Selection Key - ALT • Code Selector Keys - SELECT assigned code.
PAGE 414
SECTION 9 SUPPLEMENT 24 PA-46-350P, MALIBU SECTION 9 SUPPLEMENT 24 PA-46-350P, MALIBU SECTION 5 - PERFORMANCE SECTION 5 - PERFORMANCE No change. No change. SECTION 6 - WEIGHT AND BALANCE SECTION 6 - WEIGHT AND BALANCE Factory installed optional equipment is included in the licensed weight and balance data in section 6 of the Airplane Flight Manual. Factory installed optional equipment is included in the licensed weight and balance data in section 6 of the Airplane Flight Manual.
PAGE 415
SECTION 10 OPERATING TIPS PA-46-350P , MALIBU TABLE OF CONTENTS TABLE OF CONTENTS SECTION 10 SECTION 10 OPERATING TIPS OPERATING TIPS Paragraph No. 10.1 10.3 SECTION 10 OPERATING TIPS PA-46-350P , MALIBU Page No. General ..................................................................................... Operating Tips .......................................................................... 10-1 10-1 Paragraph No. 10.1 10.3 Page No. General ................................................
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SECTION 10 OPERATING TIPS PA-46-350P, MALIBU SECTION 10 OPERATING TIPS PA-46-350P, MALIBU SECTION 10 SECTION 10 OPERATING TIPS OPERATING TIPS 10.1 GENERAL 10.1 GENERAL This section provides operating tips of particular value in the operation of the Malibu. This section provides operating tips of particular value in the operation of the Malibu. 10.3 OPERATING TIPS 10.
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SECTION 10 OPERATING TIPS PA-46-350P, MALIBU SECTION 10 OPERATING TIPS PA-46-350P, MALIBU 10.3 OPERATING TIPS (continued) 10.3 OPERATING TIPS (continued) (g) In an effort to avoid accidents, pilots should obtain and study the safety related information made available in FAA publications, such as regulations, advisory circulars, Aviation News, AIM and safety aids.