TM 55-1510-220-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
AFTER TAKEOFF (CONT)
e.
Landing gear switch - UP.
DURING CLIMB
*1.
Engine and flight instruments - Monitor. All instruments must give
B1-10,
proper indication with minimum fluctuation.
C39
*2.
Engine control levers - Check for alignment.
*3.
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 for one minute.
c.
Read altimeter at end of one minute. Second reading must be 1000 +200 feet more than first reading.
*4.
Surface deice system - Check as follows:
C43
a.
Surface deice switch - AUTO. Surface boots should inflate and automatically deflate for one cycle.
Wing boots should stay inflated for 6 seconds, and then tail boots should stay inflated for 4 seconds.
b.
Surface deice switch - Hold to MANUAL position. Boots should stay inflated until switch is released.
2-38
