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Garmin G1000 Manual Supplement

Integrated avionics system
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  • Page 2 This page is intentionally blank. 190-00492-10 Rev 5 Diamond DA 40 / DA 40F Page 2 of 65...
  • Page 3 Garmin International 1200 E. 151 Street Olathe, KS 66062 USA 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 LOG OF REVISIONS...
  • Page 4 This page is intentionally blank. 190-00492-10 Rev 5 Diamond DA 40 / DA 40F Page 4 of 65...

  • Page 5: Table Of Contents

    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 I GENERAL......................7 (NOT FAA APPROVED) SECTION II LIMITATIONS ....................14...
  • Page 6 This page is intentionally blank. 190-00492-10 Rev 5 Diamond DA 40 / DA 40F Page 6 of 65...

  • Page 7: Section I

    If the optional TAWS function is installed in the G1000, the pilot will receive appropriate aural warnings and cautions for terrain and obstacles. The pilot should refer to the DA 40/DA 40F Pilot’s Guide for the terrain warning and caution messages and system information.
  • Page 8 Each GIA 63 computes an independent navigation solution based on its GPS sensor. The G1000 will use the GPS sensor with the highest signal quality and will automatically revert to the other sensor if the active sensor fails or if the secondary sensor is determined to be more accurate.
  • Page 9 DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F • 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 7.1 Required Functions.
  • Page 10 DIAMOND MODEL DA 40 F G1000 GPS/SBAS NAVIGATION SYSTEM, GIA 63W INSTALLED, G1000 SYSTEM SW 0321.17OR LATER USING GPS SW 3.0 OR LATER The Garmin G1000 GPS/SBAS receivers, GIA 63W, incorporating SW version 3.0 or later approved version and GA35 (PN 013-00235-00) antennas are approved under TSO-C145a/TSO-C146a equipment Class 3 and installed in accordance with AC 20-138A.
  • Page 11 Each GIA 63W computes an independent navigation solution based on its GPS sensor. The G1000 will use the GPS sensor with the highest signal quality and will automatically revert to the other sensor if the active sensor fails or if the secondary sensor is determined to be more accurate.
  • Page 12 Each GIA 63W computes an independent navigation solution based on its GPS sensor. The G1000 will use the GPS sensor with the highest signal quality and will automatically revert to the other sensor if the active sensor fails or if the secondary sensor is determined to be more accurate.
  • Page 13 ELECTRONIC FLIGHT BAG The G1000 Integrated Avionics System as installed in this aircraft has been approved as a Hardware Class 3, Software Type C Electronic Flight Bag (EFB) in accordance with AC 120-76A when using current FliteChart or ChartView data.

  • Page 14: Limitations

    P/N 190-00324-09, Revision A, or later appropriate revision. 0321.19 2. The G1000 installation in the DA 40 requires the following or later FAA approved LRU software versions. Approved LRU software versions are referenced to the System Software Version number. The LRU serial numbers displayed on the screen are for convenience only and should be disregarded in determining the LRU software revision.
  • Page 15 5. Navigation must not be predicated upon the use of the TAWS, Terrain or Obstacle data displayed by the G1000. 6. TAWS must be inhibited prior to the Final Approach Fix (FAF) when conducting an instrument approach that terminates in a circling to land or side step maneuver.
  • Page 16 Aviation database or verifies each waypoint for accuracy by reference to current approved data. 2. “GPS”, “or GPS”, and “RNAV (GPS)” instrument approaches using the G1000 System are prohibited unless the pilot verifies and uses the current Aviation database. GPS based instrument approaches must be flown in accordance with an approved instrument approach procedure that is loaded from the Aviation database.
  • Page 17 Not all published approaches are in the AVIATION database. The flight crew must ensure that the planned approach is in the database. 6. Use of the G1000 VOR/ILS receiver to fly approaches not approved for GPS requires VOR/ILS navigation data to be present on the display.
  • Page 18 DIAMOND MODEL DA 40 F G1000 GPS/SBAS NAVIGATION SYSTEM, GIA 63W INSTALLED, G1000 SYSTEM SW 0369.13 USING GPS SW 2.40 1. The Garmin G1000 GPS/SBAS receivers, GIA 63W, incorporating SW version 2.40 do not comply with US 14 CFR Part 91, SFAR 97 requirements for TSO-C145a/TSO-C146a equipment.
  • Page 19 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F GFC 700 LIMITATIONS 1. The GFC 700 AFCS preflight test must be successfully completed prior to use of the autopilot, flight director or manual electric trim. Use of the autopilot or manual electric trim system is prohibited if the preflight test is not satisfactorily completed.
  • Page 20 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F CHARTVIEW LIMITATIONS If the optional ChartView function is installed with GDU software version 8.02 and ChartView database cycle 0709 and prior, the following limitation applies: At airport locations outside the United States within ±1.5°...
  • Page 21 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 2.3 AIRSPEED MARKINGS Marking Significance Low speed awareness – stall is Red band 20 KIAS – 53 KIAS imminent speed awareness –...
  • Page 22 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.
  • Page 23 The following tables show the color and significance of the warning, caution, and advisory messages which may appear on the G1000 displays. NOTE The G1000 Cockpit Reference Guide and the G1000 Pilot’s Guide contain detailed descriptions of the annunciator system and all warnings, cautions and advisories.
  • Page 24 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F Advisory annunciations – White Annunciation Cause PFD FAN FAIL The cooling fan for the PFD is inoperative. MFD FAN FAIL The cooling fan for the MFD is inoperative.
  • Page 25 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.

  • Page 26: Emergency Procedures

    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.
  • Page 27 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 9. 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"...
  • Page 28 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.
  • Page 29 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F AUTOPILOT DISCONNECT (Yellow AP flashing on PFD) 1. AP DISC Switch ............DEPRESS AND RELEASE (to cancel disconnect tone) 2. Pitch Trim ..........RETRIM if necessary, using the trim wheel...
  • Page 30 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.
  • Page 31 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.
  • Page 32 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.
  • Page 33 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F (DA 40 F only) (g) High Fuel Flow – 1. Fuel Quantity ..............Check and Monitor 2. Power Setting..................Check Land as soon as practical.
  • Page 34 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.
  • Page 35 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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).
  • Page 36 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.
  • Page 37 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.
  • Page 38 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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”...
  • Page 39 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.

  • Page 40: Section Iva

    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.

  • Page 41: H) Throttle

    FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.

  • Page 42: Bat (Battery) Switch

    FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 19. Avionics master switch .................OFF 20. Essential Bus switch ..................OFF 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.
  • Page 43 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F STARTING ENGINE (DA 40 only) (a) Cold engine 1. Strobe light (ACL) ..................ON 2. Electrical fuel pump............ON, note pump noise (=functional check of pump) 3.
  • Page 44 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F (b) Warm engine 1. Strobe light (ACL) ..................ON 2. Electrical fuel pump............ON, note pump noise (=functional check of pump) 3.
  • Page 45 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F (c) Engine will not start after injection (”flooded engine”) Warm engine 1. Strobe light (ACL) ..................ON 2. Electrical fuel pump............ON, note pump noise (=Functional check of pump) 3.
  • Page 46 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F STARTING ENGINE (DA 40 F only) (a) Cold engine 1. Strobe light (ACL) ..................ON 2. Mixture ..................... fully RICH 3.
  • Page 47 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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..................OFF...

  • Page 48: When Engine Starts

    FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F (c) Engine will not start after priming (”flooded engine”) 1. Strobe light (ACL) ..................ON 2. Electrical fuel pump..................OFF 3. Mixture ..................LEAN, fully aft 4.

  • Page 49: Master Switch (Alt)

    FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F BEFORE TAXIING 1. Avionics master switch .................. ON 2. Electrical equipment ..............On as required 3. Flaps................UP – T/O – LDG – T/O (indicator and visual check) 4.
  • Page 50 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F BEFORE TAKE-OFF 1. Position airplane into wind if possible 2. Parking brake ....................set 3. Safety harnesses................on and fastened 4. Rear door ..............check closed and locked 5.
  • Page 51 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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;...
  • Page 52 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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...
  • Page 53 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.
  • Page 54 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.
  • Page 55 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F APPROACH: 1. Navigation Source......SELECT VOR using CDI button on PFD 2. Course Bearing Pointer ..........SET using course knob 3.
  • Page 56 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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.
  • Page 57 Descent Alerts (PDA) functions may be inhibited to stop alerting for acceptable flight conditions (such as below glideslope maneuvers). For detailed operating instructions regarding the G1000 TAWS Option, refer to the Garmin DA 40/DA 40F Pilot’s Guide. 190-00492-10 Rev 5...

  • Page 58: Section Ivb

    FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F SECTION IVB ABNORMAL PROCEDURES (Not FAA Approved) 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.

  • Page 59: System Descriptions

    Emergency or Abnormal Procedures Sections of the AFM or this Supplement for the appropriate procedure to follow for each message. 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...

  • Page 60: Diamond Model Da 40 F

    Engine instruments are displayed on the MFD. Discrete engine sensor information is processed by the Garmin Engine Airframe (GEA) sub-system. When an engine sensor indicates a value outside the normal operating range, the legend will turn yellow for caution range, and turn red and flash for warning range.
  • Page 61 FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM 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: •...

  • Page 62: Diamond Model Da 40 F

    The red AP DISC switch on the either control stick will interrupt power to the manual electric trim for as long as the switch is depressed. Loss of instruments or components of the G1000 system will affect the GFC 700 AFCS as follows:...

  • Page 63: Diamond Model Da 40 F

    FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT GARMIN G1000 INTEGRATED AVIONICS SYSTEM DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F • Loss of the AHRS will cause the autopilot to disconnect. The autopilot and flight director will be inoperative. Manual electric trim will be available.

  • Page 64: Diamond Model Da 40 F

    DIAMOND MODEL DA 40 DIAMOND MODEL DA 40 F 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. Refer to the Garmin G1000 Cockpit Reference Guide for descriptions of the G1000 and GFC 700 system and operating procedures.
  • Page 65 Fuel quantity: Fuel quantity indicating for the Standard Tank configuration functions as described in the DA 40 AFM. Also, refer to the ‘G1000 Pilot's Guide for the Diamond DA 40’ for additional information about the functionality of the G1000’s fuel quantity gauge.

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