TM 55-1510-221-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
AFTER TAKEOFF (CONT)
d.
Brake device switch Off.
e.
Landing gear switch UP.
DURING CLIMB
*1.
Engine and flight instruments
B1-9,C38
Monitor All instruments must give proper
indication with minimum fluctuation
*2.
Engine control levers Check for alignment
*3.
Vertical speed Indicators Check
B2
normal operation against altimeter as follows
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 device system Check as follows
C42
a.
Surface device switch SINGLE CYCLE
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
2-40
