Pilatus PC-12 NGX, Pilot'S Information Manual

Page: 200 / 625

Trim Runaway 3-14-03
Non-commanded trim operation, rapidly increasing out of trim forces.
1. TRIM INTERRUPT switch........... ON
2. Circuit breaker of failed trim:....... PULL
Circuit Breaker Location
PITCH TRIM Essential Bus
L
A1
PITCH TRIM ALTN Main Bus
R
A1
AIL TRIM Essential Bus
L
C1
RUD TRIM Essential Bus
L
B1
3. TRIM INTERRUPT switch........... OFF
Note
Reduce speed if control forces are high. If the rudder trim has failed the autopilot
is not operative.
The autopilot will disconnect when TRIM INTERRUPT is operated.
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No Main Stabilizer Trim 3-14-04
1. TRIM INTERRUPT...................... Check OFF
2. ALTERNATE STAB TRIM............ Operate as required
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No Stabilizer Trim, Main or Alternate 3-14-05
1. Aircraft......................................... Carry out Landing with Immobilized
Horizontal Stabilizer - 3-9-07
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Section 3 - Emergency Procedures (EASA Approved)
Electrical Trim
Pilot's Operating Handbook Report No: 02406
Issue date: Mar 06, 2020
Page 3-14-2
12-C-A15-40-0314-00A-141A-A
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