AFMS – GFC 500 Mooney M20M/M20R/M20S Series
190-02291-18 Rev. 5
Page 3–6
LOSS OF AIRSPEED DATA
(Red X through airspeed tape on the G5, GI 275, or G3X display, amber AP with a red X in autopilot
status box)
NOTE
If airspeed data is lost while the autopilot is tracking airspeed, the flight director will
default to pitch mode (PIT).
1. AP DISC / TRIM INT Button .........................................................................PRESS AND RELEASE
(to cancel disconnect tone)
2. Aircraft Attitude ........................................................... MAINTAIN / REGAIN AIRCRAFT CONTROL
3. Manual Elevator Trim ............................................................................................. TRIM as required
NOTE
The autopilot cannot be re-engaged. The flight director will be available however IAS
mode cannot be selected. Loss of airspeed will be accompanied by a red PTRIM
indication on the G5, GI 275, or G3X (if a pitch trim servo is installed).
LOSS OF ALTITUDE DATA
(Red X through altitude tape on the G5, GI 275, or G3X display)
NOTE
If altitude data is lost while the autopilot is tracking altitude, the autopilot will default to
pitch mode (PIT).
1. Autopilot .......................................................................................... SELECT different vertical mode
LOSS OF GPS INFORMATION
This procedure applies only if the optional GPS navigator is installed:
(GPS position information is lost to the autopilot.)
NOTE
If GPS position data is lost while the autopilot is tracking a GPS, VOR, LOC or Back
Course the autopilot will default to roll mode (ROL). The autopilot will default to pitch
mode (PIT) if GPS information is lost while tracking an ILS. The autopilot uses GPS aiding
in VOR, LOC and BC modes.
1. Autopilot ........................................... SELECT different lateral and/or vertical mode (as necessary)
If on an instrument approach:
1. AP DISC / TRIM INT button ............................................. PRESS, Continue the approach manually
Or
2. Missed Approach Procedure .................................................................... EXECUTE (as necessary)
Summary of Contents for M20M
Page 2: ......
Page 4: ......
Page 10: ...INTRODUCTION MOONEY MODEL M20M BLANK ISSUED 3 90...
Page 12: ...SECTION I GENERAL MOONEY MODEL M20M FIGURE 1 1 THREE VIEW ISSUED 3 90...
Page 60: ...SECTION IV NORMAL PROCEDURES MOONEY MODEL M20M ISSUED 3 90...
Page 78: ...SECTION V PERFORMANCE MOONEY MODEL M20M ISSUED 3 90...
Page 82: ...SECTION V PERFORMANCE MOONEY MODEL M20M 5 6 ISSUED 3 90...
Page 89: ...SECTION V PERFORMANCE ISSUED 3 90 5 13...
Page 90: ...SECTION V PERFORMANCE MOONEY MODEL M20M 5 14 ISSUED 3 90...
Page 91: ...MOONEY MODEL M20M SECTION V PERFORMANCE ISSUED 3 90 5 1 5...
Page 93: ......
Page 94: ...MOONEY MODEL M20M 5 1 8 ISSUED 3 90...
Page 95: ......
Page 97: ...RPM PEAK T I T...
Page 99: ...MOONEY SECTION V MODEL M20M PERFORMANCE ISSUED 3 90 5 23...
Page 102: ...SECTION V PERFORMANCE MOONEY MODEL M20M 5 26 ISSUED 3 90...
Page 104: ...SECTION V PERFORMANCE MOONEY MODEL M20M 5 28 ISSUED 3 90...
Page 111: ...MOONEY MODEL M20M SECTION VI WEIGHT AND BALANCE M2OM WT BAL RECORD ISSUED 3 90 6 5...
Page 113: ......
Page 114: ...SECTION VI WEIGHT AND BALANCE MOONEY MODEL M20M 6 8 ISSUED 3 90...
Page 120: ......
Page 153: ......
Page 157: ...MOONEY M20M SECTION VII AIRPLANE AND SYSTEM DESCRIPTION ISSUED3 90 REV A 1 96 7 23...
Page 176: ...SECTION Vlll HANDLING SERVICE AND MAINTENANCE MOONEY MODEL M20M BLANK ISSUED 3 90...
Page 178: ...SECTION IX SUPPLEMENTAL DATA SUPPLEMENT INSERTED MOONEY MODEL M20M DATE ISSUED 3 90...
Page 180: ...SECTION IX SUPPLEMENTAL DATA MOONEY MODEL M20M BLANK ISSUED 3 90...
Page 360: ......
