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BEFORE TAXIING (CONT) - TM-55-1510-218-MTF0040
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TM-55-1510-218-MTF Maintenance Test Flight Manual Army Model C-12C C-12D and C-12F Aircraft
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BEFORE TAXIING (CONT) - TM-55-1510-218-MTF0042
TM 55-1510-218-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
troller will illuminate after
approximately 8 seconds.
The A/P TRIM FAIL and
MASTER WARNING an-
nunciators will illuminate
after approximately 15 sec-
onds.
(2) Master warning annuncia-
tor - Reset.
(3) Control wheel - Hold for-
ward of mid travel. Trim
wheel should run nose up
after approximately 3 sec-
onds. The TRIM UP an-
nunciator on the autopilot
controller will illuminate
after approximately 8 sec-
onds. The A/P TRIM FAIL
and MASTER WARNING
annunciators
will illumi-
nate after approximately 15
seconds.
(4) Master warning annuncia-
tor - Reset.
h. Overpower check: (Ieft power
Iever) - Press.
If unable to overpower autopilot in any axis,
or if autopilot or yaw damper disengages
during overpower test, do not use.
2-31

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