AFMS – GFC 500 Mooney M20M/M20R/M20S Series
190-02291-18 Rev. 5
Page 4–4
GO AROUND
1. GO AROUND button ............................................. PRESS – Verify GA / GA on G5, GI 275, or G3X
(autopilot will not disengage)
2. Autopilot (if engaged) ............... VERIFY airplane pitches up following flight director command bars
3. Throttle ...................................................................................................... APPLY Go Around power
4. GMC 507 Mode Panel .................................... PRESS NAV to couple to selected navigation source
OR
PRESS HDG to Fly ATC Assigned Missed Approach Heading
5. Altitude Preselect .................................................................................................................. VERIFY
Set to appropriate altitude.
NOTE
The pilot is responsible for initial missed approach guidance in accordance with published
procedure. When the GA button is pressed the Flight Director command bars will command
go-around pitch attitude and wings level. The pilot must set Go Around power, then select
the CDI to the appropriate navigation source and select the desired lateral and vertical
flight director modes.
MANUAL PITCH TRIM WITH AUTOPILOT ENGAGED
(Amber TRIM UP or TRIM DOWN displayed on G5, GI 275, or G3X)
NOTE
If the aircraft is not equipped with a pitch trim servo, the pilot must manually adjust the
pitch trim when airspeed and aircraft configuration changes are made.
A message will be displayed on the G5, GI 275, or G3X display to indicate the pitch servo is holding
sustained force, and the pilot must manually trim the aircraft.
1.
If TRIM UP message is displayed ...........................................................
MANUALLY TRIM nose up
2.
If TRIM DOWN message is displayed ...............................................
MANUALLY TRIM nose down
Summary of Contents for M20M
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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...
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Page 94: ...MOONEY MODEL M20M 5 1 8 ISSUED 3 90...
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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...
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Page 114: ...SECTION VI WEIGHT AND BALANCE MOONEY MODEL M20M 6 8 ISSUED 3 90...
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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...
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