FAA Approved Airplane Flight Manual Supplement

ManualsBrandsGarmin ManualsFlight DecksGarmin Software Version 0321.22

Summary of content (66 pages)

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Garmin Ltd. Or its subsidiaries c/o Garmin International 1200 E.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F Table of Contents SECTION 1 GENERAL ................................................................................. 1-1 SECTION 2 LIMITATIONS ......................................................................... 2-1 SECTION 3 EMERGENCY PROCEDURES .............................................. 3-1 SECTION 4A NORMAL PROCEDURES .
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F SECTION 1 GENERAL G1000 The G1000 Integrated Avionics System is a fully integrated flight, engine, communication, navigation and surveillance instrumentation system.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F Operational Approvals G1000 GPS NAVIGATION SYSTEM, GIA 63 INSTALLED GIA 63 units are standard and provide position information in accordance with TSO-C129a class A1.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F • The G1000 Integrated Avionics system as installed in this aircraft is eligible for B-RNAV in accordance with AMJ20X2.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F • The G1000 WFDE predication program works in combination with the Garmin AT, Inc. Route Planning Software, version 1.2, or later approved version. The route planning and WFDE prediction program can be downloaded from Garmin G1000 website on the Internet.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F ELECTRONIC FLIGHT BAG The G1000 Integrated Avionics System as installed in this aircraft has been approved as a Hardware Class 3, Software Type B Electronic Flight Bag (EFB) in accordance with AC 120-76B when using current FliteChart or ChartView data. Additional operational approvals may be required.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F SECTION 2 LIMITATIONS 2.1 INTRODUCTION GENERAL LIMITATIONS 1. 2. The Garmin G1000 Cockpit Reference Guide (CRG) must be immediately available to the flight crew. The required CRG is referenced to the System Software Version number. The System Software Version number is displayed at the top right side of the MFD Power-up page.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 4. The ADF aural identifier must be monitored any time the ADF is used as the primary source of navigation. 5. Do not use SafeTaxi or Chartview functions as the basis for ground maneuvering. SafeTaxi and Chartview functions do not comply with the requirements of AC 20-159 and are not qualified to be used as an airport moving map display (AMMD).
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 7. IFR non-precision approach approval using the GPS/SBAS sensor is limited to published approaches within the U.S. National Airspace System. Approaches to airports in other airspace are not approved unless authorized by the appropriate governing authority. 8.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 6. ILS approaches using the GFC 700 autopilot/flight director are limited to Category I approaches only. TERRAIN AWARNESS AND WARNING SYSTEM (TAWS) SYSTEM LIMITATIONS NOTE: The terrain display is intended to serve as a situational awareness tool only.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F TRAFFIC AVOIDANCE SYSTEM LIMITATIONS Use of the MAP - TRAFFIC MAP to maneuver the airplane for traffic avoidance without outside visual reference is prohibited. The Traffic Information System (TIS) is intended as an aid for the pilot to visually locate traffic.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 2.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 2.5 ENGINE INSTRUMENT MARKINGS Engine instrument markings and their color code significance are shown in the table below. NOTE When an indication lies in the upper or lower prohibited range, the legend for that display will change to the color of the prohibited range and will flash. Indication Manifold Pressure In.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F Note 2: Not applicable to DA 40 F. Manifold Pressure gauge is not installed in the DA 40 F. Note 3: To prevent nuisance alerts during normal takeoffs, the legend “RPM” and digits will not turn red or flash until the RPM exceeds 2780. Note 4: Fuel Pressure Gauge is optional for DA 40 aircraft. 2.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F Caution annunciations – Yellow Annunciation PITOT OFF PITOT FAIL L FUEL LOW R FUEL LOW LOW VOLTS PFD FAN FAIL MFD FAN FAIL GIA FAN FAIL PFD OVERHEAT MFD OVERHEAT GIA1 OVERHEAT GIA2 OVERHEAT 190-00492-10 Rev 8 FAA Approved Cause Pitt heat is not switched on Fault in the pitot heating system Fuel quantity in the left tank is less than 3 US gal (+1
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 2.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 2.15 Limitation Placard Below the MFD, next to the fuel quantity indication: Standard Tanks Fuel qty. Indication: max 17 US gal Max. difference LH/RH tank: 10 US gal For use of max. tank capacity see AFM Long Range Tanks Fuel qty. Indication: max 24 US gal Refer to AFM to use entire tank capacity Max.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F SECTION 3 EMERGENCY PROCEDURES GENERAL 1. If Garmin G1000 GPS navigation information is not available or invalid, utilize remaining operational navigation equipment as required. 2. If the G1000 system reverts to Dead Reckoning mode (indicated by DR displayed on the HSI), the moving map will continue to be displayed.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT 9. DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F In an in-flight emergency, depressing and holding the COM transfer button for 2 seconds will tune the emergency frequency of 121.500 MHz. If the display is available, it will also show it in the "Active" frequency window. 10.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F GFC 700 EMERGENCY PROCEDURES Some emergency situations require immediate memorized corrective action. These numbered steps are printed in boxes within the emergency procedures and should be accomplished without the aid of the checklist.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F AUTOPILOT DISCONNECT (Red AP flashing on PFD) 1. AP DISC Switch ........................................................ DEPRESS AND RELEASE (to cancel disconnect tone) 2. Pitch Trim ..........................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F AUTOPILOT OUT OF TRIM (Yellow ←AIL, AIL→, ↑ELE, or ↓ELE on PFD) For ↑ELE, or ↓ELE Indication: WARNING DO NOT ATTEMPT TO OVERPOWER THE AUTOPILOT IN THE EVENT OF A PITCH MISTRIM. THE AUTOPILOT SERVOS WILL OPPOSE PILOT INPUT AND WILL CAUSE PITCH TRIM TO RUN OPPOSITE THE DIRECTION OF PILOT INPUT.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F For ←AIL, AIL→ Indication: 1. Rudder Trim ........................................ VERIFY slip/skid indicator is centered NOTE Observe the maximum fuel imbalance limitation. If annunciation remains: 2. Control Stick ..............................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F FAILURE OF THE PREFLIGHT TEST (Red boxed PFT on PFD) 1. AFCS Circuit Breaker .........................................................................PULL WARNING DO NOT ATTEMPT TO ENGAGE THE AUTOPILOT OR OPERATE THE MANUAL ELECTRIC TRIM UNTIL THE CAUSE OF THE MALFUNCTION HAS BEEN CORRECTED.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F (g) High Fuel Flow – (DA 40 F only) 1. Fuel Quantity ................................................................... Check and Monitor 2. Power Setting ........................................................................................ Check Land as soon as practical. Consider the reduced range and endurance due to possible loss of fuel.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F If smoke or fumes decrease: 9. Land at the nearest suitable airport as soon as possible If smoke or fumes persist: 10. ALT (alternator) switch ................................................................................. ON 11. ESS BUS switch ........................................................................................... OFF 12.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 3.7.1 ICING Unintentional flight into icing conditions 1. Leave the icing area (by changing altitude or turning back, in order to reach zones with a higher ambient temperature). 2. Pitot heating ............................................................................................. ON 3. Cabin heat ..............................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 3.7.2 FAILURES IN THE ELECTRICAL SYSTEM (b) Alternator failure An alternator failure is indicated by a red ALTERNATOR message and an ammeter indication of 0 Amps. 1. 2. Circuit breakers ...................................................................................... Check in ALT (alternator) switch ..............................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F For cases in which the battery capacity is not sufficient to reach a suitable airport, an emergency battery is installed to power the standby attitude gyro and floodlight. This battery is switched on with the HORIZON EMERGENCY Switch. It provides power for 1 hour and 30 minutes when the floodlight is switched on. 3.8 AVIONICS EMERGENCIES 3.8.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 3.8.2 AHRS FAILURE NOTE A failure of the Attitude and Heading Reference System (AHRS) is indicated by removal of the sky/ground presentation and a red X and a yellow “AHRS FAILURE” shown on the PFD. The digital heading presentation will be replaced with a yellow “HDG” and the compass rose digits will be removed.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 3.8.5 ERRONEOUS OR LOSS OF WARNING/CAUTION ANNUNCIATORS NOTE Loss of an annunciator may be indicated when engine or fuel displays show an abnormal or emergency situation and the annunciator is not present. An erroneous annunciator may be identified when an annunciator appears which does not agree with other displays or system information. 1.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F SECTION 4A NORMAL PROCEDURES NOTE Readability of the PFD and MFD displays may be degraded when wearing polarized sunglasses. 1. DETAILED OPERATING PROCEDURES Normal operating procedures for the G1000 and GFC 700 are described in the Garmin G1000 Cockpit Reference Guide and the Garmin G1000 Pilot's Guide. PRE-FLIGHT INSPECTION I.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F NOTE FOR STANDARD TANKS, when the fuel quantity indicator reads 17 US gal the correct fuel quantity must be determined with the fuel quantity measuring device. If this measurement is not carried out, the fuel quantity available for flight planning is 17 US gal.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 19. Avionics master switch ................................................................................. OFF 20. Essential Bus switch .....................................................................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F When engine starts: 7. 8. 9. Mixture control lever ....................................................... rapidly move to RICH Oil pressure ..................................................................... green arc within 15 sec Electrical fuel pump ......................................................................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 11. Fuel pressure ...................................................... Check no messages illuminated 12. Annunciator section of PFD ...................................................................... Check (b) Engine will not start after injection (”flooded engine”) Warm engine 1. 2. 3. 4. Strobe light (ACL) .....................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F STARTING ENGINE (DA 40 F only) (a) Cold engine 1. 2. 3. 4. 5. Strobe light (ACL) ......................................................................................... ON Mixture ............................................................................................. fully RICH Electrical fuel pump ............................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F When engine starts: 7. Oil pressure ...................................................................... green arc within 15 sec 8. Throttle .......................................................................................... set 1000 RPM 9. Electrical fuel pump ..................................................................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F (c) Engine will not start after priming (”flooded engine”) 1. 2. 3. 4. Strobe light (ACL) ......................................................................................... ON Electrical fuel pump ...................................................................................... OFF Mixture .................................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F BEFORE TAXIING 1. 2. 3. Avionics master switch .................................................................................. ON Electrical equipment .....................................................................On as required Flaps...............................................................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F BEFORE TAKE-OFF 1. 2. 3. 4. 5. Position airplane into wind if possible Parking brake ................................................................................................... set Safety harnesses .......................................................................... on and fastened Rear door .............................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 18. RPM lever (DA 40 only) ...................................... pull back until a drop of max. 500 RPM is reached – HIGH RPM; Cycle 3 times 18a Carburetor Heat (DA 40 F only) ...................................................check function 18b Throttle (DA 40 F only) ................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F AFTER TAKEOFF – GFC 700 NORMAL PROCEDURES WARNING IT IS THE RESPONSIBILITY OF THE PILOT IN COMMAND TO MONITOR THE AUTOPILOT WHEN IT IS ENGAGED. THE PILOT SHOULD BE PREPARED TO IMMEDIATELY DISCONNECT THE AUTOPILOT AND TO TAKE PROMPT CORRECTIVE ACTION IN THE EVENT OF UNEXPECTED OR UNUSUAL AUTOPILOT BEHAVIOR.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F CLIMB, CRUISE and DESCENT: Vertical Speed (VS): 1. Altitude Preselect ........................................................... SET to desired altitude 2. Mode Controller ............................................. SELECT VS on mode controller 3. Vertical Speed Reference ....ADJUST using NOSE UP and NOSE DN buttons 4.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F NOTE In ALT mode, the autopilot will maintain the reference altitude shown in the autopilot window of the PFD regardless of the altitude in the altitude preselect window or the altimeter’s barometric pressure setting. If the altimeter setting is changed, the autopilot will climb or descend to maintain the reference altitude.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F APPROACH: VOR 1. Navigation Source............................ SELECT VOR using CDI button on PFD 2. Course Bearing Pointer ................................................. SET using course knob 3. Intercept Heading .................ESTABLISH in HDG or ROL mode (if required) 4. Mode Controller ...........................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 7. Airspeed .................... MAINTAIN 80 KIAS OR GREATER (Recommended) GPS: LPV, LNAV/VNAV, LNAV+V (If equipped with optional GIA 63W GIA units) 1. Navigation Source............................. SELECT GPS using CDI button on PFD 2. Approach ........................................................ LOAD in FMS and ACTIVATE 3. Intercept Heading ....
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 7. Autopilot ......................................................................RE-ENGAGE if desired NOTE If the missed approach procedure requires tracking the localizer outbound from the airport, use NAV mode to prevent inadvertent coupling to glideslope.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F SECTION 4B ABNORMAL PROCEDURES 4B.3 FAILURES IN THE ELECTRICAL SYSTEM (a) Low voltage caution (LOW VOLTS) This caution is indicated when the normal on-board (bus) voltage (28V) drops below 24V. Possible reasons are: -A fault in the power supply -RPM is too low (i) Low voltage caution on the ground: 1. 2. 3. Engine speed .............................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F AVIONICS COOLING FAN FAILURES NOTE These caution messages are indicated when a cooling fan has failed. The avionics may overheat, especially in hot temperatures. (a) PFD FAN FAIL caution ON GROUND: 1. Do not takeoff in night or in instrument meteorological conditions. IN FLIGHT: 1. Monitor for PFD OVERHEAT caution message.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F PFD, MFD, AND GIA OVERHEAT (a) PFD OVERHEAT caution NOTE The PFD is approaching its operating temperature limit. Display brightness is automatically reduced to 50% of maximum. 1. Cross check PFD attitude, heading, altimeter, and airspeed with standby instruments. 2.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT 1. DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F Refer to standby attitude, heading, altimeter, and airspeed instruments to maintain aircraft control. 2. If either the PFD or MFD fails or is unusable, pull the circuit breaker of the affected device and select Display Reversionary Mode using the red DISPLAY BACKUP button on the audio panel. 3. Land as soon as practical at a suitable airport.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F SECTION 5 PERFORMANCE No change. Refer to the Aircraft Flight Manual.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F SECTION 6 WEIGHT AND BALANCE Refer to the Aircraft Flight Manual and see current weight and balance data.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F SECTION 7 SYSTEM DESCRIPTIONS G1000 SYSTEM The Garmin G1000 Integrated Avionics System consists of a Primary Flight Display (PFD), a Multi-Function Display (MFD), an Audio Panel, and Attitude and Heading Reference System (AHRS), an Air Data Computer (ADC), and the sensors and computers to process flight and engine information for display to the pilot.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F Advisory messages related to G1000 system status are shown in white and are accompanied by a white flashing ADVISORY alert. Refer to the G1000 Pilot’s Guide and Cockpit Reference Guide for descriptions of the messages and recommended actions (if applicable).
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F GFC 700 The GFC 700 Automatic Flight Control System (AFCS) is a 2 axis autopilot and flight director system which provides the pilot with the following features: • Altitude Preselect and Altitude Hold (ALT) • Flight Level Change with Airspeed Hold (FLC) • Vertical Speed Hold (VS) • Navigation tracking for VOR (NAV) and GPS (GPS) • Heading Hol
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F The GFC 700 autopilot contains an electric pitch trim system which is used by the autopilot for automatic pitch trim during autopilot operation and by the pilot for manual electric pitch trim when the autopilot is not engaged. The manual electric pitch trim system is operated by a split switch on the left control stick.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F Loss of instruments or components of the G1000 system will affect the GFC 700 AFCS as follows: • • • • • • • • Loss of the AHRS will cause the autopilot to disconnect. The autopilot and flight director will be inoperative. Manual electric trim will be available. Loss of the heading function of the AHRS will result in loss of the HDG mode.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM WITH GARMIN GFC 700 AUTOPILOT DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F and flashing alert may be cancelled by pressing the AP DISC switch or the left side of the MET switch. Refer to the Garmin G1000 Pilot’s Guide for the Diamond DA 40, for a complete description of the GFC 700 system and operating procedures. 7.
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Part Information GPN: Description: Part Type: Lifecycle Phase: Rev: 190-00492-10 AFMS,G1000 Integ.