FAA Approved Airplane Flight Manual Supplement

ManualsBrandsGarmin ManualsFlight DecksGarmin Software Version 0321.22

Summary of content (55 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 • • DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT The G1000 Integrated Avionics system as installed in this aircraft is eligible for PRNAV in accordance with PRNAV requirements: JAA Administrative & Guidance Material Section One: General Part 3: Temporary Guidance Leaflets, Leaflet No 10: Airworthiness and Operational Approval for Precession RNAV Operations in Designated European Airspace 7
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT downloaded from Garmin G1000 website on the Internet. For information on using the WFDE Prediction Program, refer to Garmin WAAS FDE Prediction Program, part number 190-00643-01, ‘WFDE Prediction Program Instructions’. • North Atlantic (NAT) Minimum Navigational Performance Specifications (MNPS) Airspace per AC 91-49 and AC 120-33.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 4. DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 7. 8. DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT TERRAIN AWARNESS AND WARNING SYSTEM (TAWS) SYSTEM LIMITATIONS NOTE: The terrain display is intended to serve as a situational awareness tool only. It may not provide either the accuracy or fidelity, or both, on which to solely base decisions and plan maneuvers to avoid terrain or obstacles. 1.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 2.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT Note 1: Not applicable to DA 40 F. Manifold Pressure gauge is not installed in the DA 40 F. Note 2: To prevent nuisance alerts during normal takeoffs, the legend “RPM” and digits will not turn red or flash until the RPM exceeds 2780. Note 3: 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 190-00492-12 Rev 6 FAA Approved Cause Pitot heat is not switched on Fault in the pitot heating system Fuel quantity in the left tank is less than 3 US gal
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 2.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 9. DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 3.2.3 ENGINE PROBLEMS IN FLIGHT (h) High Fuel Flow – (DA 40 only) Fuel flow in red sector 1. Fuel pressure .................................... check for red FUEL PRESS LO message • If fuel pressure is low (FUEL PRESS LO message), there is possibly a leak (between the injection system and the injectors). Land at the nearest available airport.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 3.3.3 SMOKE AND FIRE IN FLIGHT (b) Electrical fire with smoke in flight 1. Emergency switch ......................................................................... ON if installed CAUTION Switching OFF the master switch (ALT/BAT) will lead to total loss of all electronic and electric equipment, including the AHRS and attitude display.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 13. Use standby instruments for attitude, airspeed and altitude 14. Refer to Section 3.7.2 (b) of this Supplement, Alternator Failure 15.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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. Circuit breakers ...................................................................................... Check in 2. ALT (alternator) switch ............................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 3.8 AVIONICS EMERGENCIES 3.8.1 PFD OR MFD DISPLAY FAILURE a) DISPLAY BACKUP button on audio panel…RELEASE (button shall be OUT) 3.8.1.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT CAUTION When the essential bus is switched ON, the battery will not be charged unless the essential tie relay bypass (OAM 40-126) is installed. 21. BAT (battery) switch .................................................................................... ON 22. Fuel tank selector .....................................................................
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 9. ALT (alternator) switch ................................................................................. ON 10. Ammeter .................................................................................................... Check 11. Fuel pressure ...................................................... Check no messages illuminated 12.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT (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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT of the missed approach procedure is desired, use the autopilot NAV mode to prevent inadvertent GS coupling. AFTER TAKEOFF – TAWS NORMAL PROCEDURES (If Optional TAWS system is installed) TAWS CAUTION When a TAWS CAUTION occurs, take positive corrective action until the alert ceases.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT (c) PFD OVERHEAT caution AND MFD OVERHEAT caution NOTE The PFD and MFD are both approaching operating temperature limits. The brightness of both displays is automatically reduced to 50% of maximum. 1. Refer to standby attitude, heading, altimeter, and airspeed instruments to maintain aircraft control. 2.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT SECTION 6 WEIGHT AND BALANCE See current weight and balance data.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 pil
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 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 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT G1000/KAP 140 INTERFACE The G1000 system provides heading and course information, lateral and vertical navigation flags and both lateral and vertical course deviation signals to the KAP 140 autopilot. When course deviation signals are available from the G1000, the KAP 140 may be coupled to those signals as described in the autopilot documentation.
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FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F WITH HONEYWELL KAP 140 AUTOPILOT 7.10 FUEL SYSTEM Fuel Quantity Indication Each fuel tank has a capacity probe that ascertains fuel quantity in that tank. Standard Tank configurations have two fuel probes, one in each wing. Long Range Tank configurations have four fuel probes, two in each wing, an outboard tank and an inboard tank.
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Part Information GPN: Description: Part Type: Lifecycle Phase: Rev: 190-00492-12 AFMS,G1000 Integ.