Piper ARCHER III, Руководство по эксплуатации для пилотов

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PA-28-181, ARCHER 111
SECTION 3
EMERGENCY PROCEDURES
3.Se
Avionics System Failures ( continued)
Electric PitchTrim Failure
Indication: Red boxed PTRM on PFD
NOTE
Loss of the electric pitch trim servo will not cause
the autopilot to disconnect. Monitor pitch altitude
for unusual behavior. Be alert to possible autopilot
out-of-trim conditions (see AUTOPfLOT OUT
OF
TRIM
procedure this section) and expect
residual control forces upon disconnect. The
autopilot will not re-engage after disconnect with
failed pitch trim.
Autopilot ............................................................................ DISCONNECT
Electric Pitch Trim Runaway
Indication: An unexpected pitch deviation from the desired flight
path and red PTRNI annunciation
NOTE
After the autopilot is disengaged, it can not be
re-engaged until the electric pitch trim system
regains functionality.
Control Wheel ................................................................. GRASP FlRML Y
Altitude Indicators .............................................................. CROSSCHECK
NP
DISC Switch ..................................................... DEPRESS and HOLD
PITCH TRIM Circuit Breaker (Row 3, Col. l) ................................. PULL
Pitch Trim ............................................................. RETRlM MANUALLY
ISSUED: December 22, 2017 REPORT: VB-2749
3-33