TM 1-1510-224-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
2.
Propeller synchronization - As required.
3.
Yaw damper - ENGAGE (required above
17,000 feet).
4.
Brake deice - As required.
5.
ICE VANE CONTROL switches - As
required.
6.
STANDBY PUMP switches - As required.
7.
Cabin pressurization - Check. Adjust
rate control knob so that cabin rate-of-
climb equals one third of aircraft rate-of-
climb.
* 8.
Wings and center section - Check for
security and no fuel fuel/oil leaks.
E29
9.
Flare/chaff dispenser safety point -
Remove as required.
10.
ASE - As required.
*11.
Engine and flight instruments - Monitor.
All
instruments
must
give
proper
indication with minimum fluctuation.
E6
*12.
Engine
control
levers
-
Check
for
alignment.
E29
*13.
Vertical speed indicators - Check normal
operation against altimeter as follows:
B2
(a)
Aircraft rate of climb - Fly an
indicated 1000 feet per minute.
(b)
Read altimeter at beginning of
timing, and time of one minute.
(c)
Read altimeter at end of one
minute. Second reading must be
1000 +200 feet more than first
reading.
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