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Garmin G1000 Airplane Flight Manual Supplement

Integrated avionics system installed in mooney m20r
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Download this manual See also: Reference Manual, Maintenance Manual
MOONEY
M20R
MOONEY AIRPLANE COMPANY, INC.
LOUIS SCHREINER FIELD KERRVILLE, TEXAS 78028
AIRPLANE FLIGHT MANUAL SUPPLEMENT
INTEGRATED AVIONICS SYSTEM
INSTALLED IN MOONEY M20R
REG. NO. _____________________________________________
SERIAL NO. ____________________________________________
This Supplement must be attached to the FAA Approved Airplane Flight
Manual when the GARMIN G1000 Integrated Avionics System is
installed in accordance with Mooney Drawing Number 950300. The in-
formation contained herein supplements and / or replaces the informa-
tion of the basic Airplane Flight Manual. For Limitations, Procedures
and Performance information not contained in this Supplement, consult
the basic Airplane Flight Manual.
FAA APPROVED
Michele M. Owsley
Manager, Aircraft Certification Office
FEDERAL AVIATION ADMINISTRATION
2601 Meacham Boulevard
Fort Worth, Texas 76137-0150
CopyrightE 2006 All Rights Reserved Mooney Airplane Company -- Louis Schreiner Field Kerrville, Texas 78028
ISSUED 11 - 2004
REVISION A 06--2005
REVISION B 03--2006
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
FAA APPROVED
FOR
GARMIN G1000
SUPP0001B
AFM SUPPLEMENT
1 of 33
FAA APPROVED

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  • Page 1 SERIAL NO. ____________________________________________ This Supplement must be attached to the FAA Approved Airplane Flight Manual when the GARMIN G1000 Integrated Avionics System is installed in accordance with Mooney Drawing Number 950300. The in- formation contained herein supplements and / or replaces the informa- tion of the basic Airplane Flight Manual.
  • Page 2 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R LOG OF REVISIONS REV. PAGE DESCRIPTION APR’VD NUMBER NUMBER(S) APPROVED DATE 7, 17, 29, Add following components from Garmin G1000 Cockpit Reference Guide: GDL 69A 17, 30 Add SKYWATCHt Capability THE REVISED PORTIONS OF AFFECTED PAGES ARE INDICATED BY VERTICAL LINES IN THE MARGIN.

  • Page 3: Table Of Contents

    MOONEY AFM SUPPLEMENT M20R GARMIN G1000 INTEGRATED AVIONICS SYSTEM TABLE OF CONTENTS SECTION PAGE GENERAL ......... . .
  • Page 4 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R INTENTIONALLY LEFT BLANK 4 of 33 ISSUED 11 - 2004 REVISION A 06--2005 FAA APPROVED REVISION B 03--2006...
  • Page 5 M20R GARMIN G1000 INTEGRATED AVIONICS SYSTEM SECTION I - - GENERAL 1. The GARMIN G1000 Integrated Avionics System is a fully integrated flight, engine, communication, navigation and surveillance instru- mentation system. The system consists of a Primary Flight Display (PFD), Multi--Function Display (MFD), audio panel (GMA), Air Data...
  • Page 6 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R airspace operations, provided it is receiving usable navigation infor- mation from the GPS receiver. (A separate software application for prediction of GPS navigation availability may be required for oceanic and remote operations. Refer to appropriate limitations for the air- space you are operating in to determine if this GPS prediction soft- ware is required.)

  • Page 7: Igeneral

    1. The GARMIN G1000 Cockpit Reference Guide for the M20R Series aircraft, P/N 190--00450--01, Revision A or later approved revision must be immediately available to the flight crew. 2. The GARMIN G1000 must utilize the following or later FAA approved software versions: SUB- -SYSTEM SOFTWARE VERSION 4.06...
  • Page 8 GPS overlay with the G1000 GPS receiver is not authorized. (c) Use of the G1000 VOR/ILS receiver to fly approaches not ap- proved for GPS require VOR/ILS navigation data to be valid on the PFD display.
  • Page 9 NOTE: In some areas outside the United States, datums other than WGS- -84 or NAD- -83 may be used. If the G1000 is authorized for use by the appropriate Airworthiness authority, the re- quired geodetic datum must be set in the G1000 prior to its use for navigation.
  • Page 10 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R 2.2 POWER PLANT INSTRUMENT MARKINGS Power plant instrument markings and their color code significance are shown in the table below. NOTE: When an indication lies in the caution range, the legend for that display will change to the color of the caution range.
  • Page 11 These messages appear on the PFD for flight crew aware- ness. The following warnings and cautions may appear in various locations on the PFD or MFD. Consult the G1000 Cockpit Reference Guide and the G1000 Pilot’s Guide for detailed descriptions of each annunciation as necessary.
  • Page 12 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R Annunciation Cause AHRS Aligning – Keep Attitude and Heading Reference System is Wings Level aligning. Keep wings level using standby attitude indicator. ATTITUDE FAIL Display system is not receiving attitude reference information from the AHRS; ac-...
  • Page 13 MOONEY AFM SUPPLEMENT M20R GARMIN G1000 INTEGRATED AVIONICS SYSTEM DECALS AND PLACARDS M20R FLIGHT PANEL - PLACARD LOCATIONS RSPL- -01 PART DECAL/PLACARD LOCATION NUMBER NOMENCLATURE 150056-1001 SPEEDBRAKE EQUIPPED FOR OPERATING... 150056-1004 N NUMBER 150056-1012 14V RECEPTACLE 800399-007 PANEL LIGHTS/GLARESHIELD 150056-1010...
  • Page 14 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R INTENTIONALLY LEFT BLANK 14 of 33 ISSUED 11 - 2004 REVISION A 06--2005 FAA APPROVED REVISION B 03--2006...

  • Page 15: Emergency Procedures

    2. These checklists assume that the aircraft is equipped with a standby alternator system installed by Mooney Airplane Company, Inc. 3. If GARMIN G1000 GPS navigation information is not available or in- valid, utilize remaining operational navigation equipment as re- quired.
  • Page 16 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R 7. In an in--flight emergency, depressing and holding the Comm trans- fer button for 2 seconds will select the emergency frequency of 121.500 MHz, and will show it in the ”Active” frequency window.
  • Page 17 MOONEY AFM SUPPLEMENT M20R GARMIN G1000 INTEGRATED AVIONICS SYSTEM -CAUTION- If the autopilot is engaged, when the BAT circuit breaker is pulled, the autopilot will disconnect without annunciation. ALT SENSE EMER ALT BUS ALT FIELD EMER ALT FIELD ALT OUT...
  • Page 18 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R 5. Terminate flight as soon as practical. 6. On approach, the pilot may engage the “BAT” circuit breaker to rees- tablish power to all systems if necessary. 7. If using battery power only and the primary battery has been de- pleted (minimum of 18 VDC), the pilot may select the alternate bat- tery using the main battery selection switch.
  • Page 19 MOONEY AFM SUPPLEMENT M20R GARMIN G1000 INTEGRATED AVIONICS SYSTEM d) ERRONEOUS OR LOSS OF ENGINE AND FUEL DISPLAYS NOTE: Loss of an engine parameter is indicated by a red X through the data field. Erroneous information may be identified by in- dications which do not agree with other system information.
  • Page 20 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R INTENTIONALLY LEFT BLANK 20 of 33 ISSUED 11 - 2004 REVISION A 06--2005 FAA APPROVED REVISION B 03--2006...

  • Page 21: Normal Procedures

    The following normal procedures have been modified as the result of the G1000 installation. Procedures which have not been modified as a result of the G1000 installation should be used as written in the POH/ AFM. DETAILED OPERATING PROCEDURES Normal operating procedures for the G1000 are described in the GAR- MIN G1000 Cockpit Reference Guide and the GARMIN G1000 Pilot’s...
  • Page 22 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R Cabin Heat .........
  • Page 23 AFM SUPPLEMENT M20R GARMIN G1000 INTEGRATED AVIONICS SYSTEM Parking Brake ........
  • Page 24 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R Stdby Alt/Emerg Bus switch ....... .
  • Page 25 MOONEY AFM SUPPLEMENT M20R GARMIN G1000 INTEGRATED AVIONICS SYSTEM Emergency Gear Extension (RED) Handle DOWN and LATCHED Oil Temperature ......
  • Page 26 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R CLIMB (CRUISE) Power ..........

  • Page 27: Vperformance

    See current weight and balance data. SECTION VII - - SYSTEM DESCRIPTIONS 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 Com- puter (ADC), and the sensors and computers to process flight and en- gine information for display to the pilot.
  • Page 28 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R Altimeter setting knob (baro/QNH set) Course knob Map range knob and cursor control FMS control buttons and knob PFD softkey buttons, including master warning/caution acknowl- edgement Altitude reference set knob Heading bug control...
  • Page 29 The G1000 also interfaces to the STEC 55x autopilot and repeats the autopilot mode annunciators on the G1000 PFD. This provides easy viewing of the autopilot operating mode and status, but remains a sup- plemental display of autopilot operating modes.
  • Page 30 In the event of an alternator failure, the standby alternator and selected main battery will power the following: A reduced subset of the G1000 system, which is comprised of the PFD/MFD, AHRS, ADC, Com1, Nav1, GPS1, transponder, audio panel, and Engine Instruments;...
  • Page 31 EQUIPMENT LOCATION The G1000 ADC and GEA LRU’s are located behind the PFD and MFD, which may be removed using a hexagonal tool. The magnetometer is located in the right wing outboard of the landing light. The AHRS, and remaining LRU’s are located behind the cabin near the main batteries.
  • Page 32 AFM SUPPLEMENT MOONEY GARMIN G1000 INTEGRATED AVIONICS SYSTEM M20R RSPL- -02 M20R POWER SUMMARY 7.3 - - VACUUM SYSTEM GX aircraft are all electric, there is no Vacuum System in the standard aircraft. 32 of 33 ISSUED 11 - 2004...

  • Page 33: Handling And Servicing

    M20R GARMIN G1000 INTEGRATED AVIONICS SYSTEM 7.4 - - INSTRUMENT PANEL The instrument panel has been designed to incorporate the G1000 Inte- grated Cockpit. All Communications, Navigation, Engine Instruments, and System annunciations have been integrated into a custom design package specifically for the M20R series aircraft.

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