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DURING CLIMB
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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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DURING CLIMB (CONT) - TM-55-1510-218-MTF0061
TM 55-1510-218-MTF
TROUBLESHOOTING
PROCEDURE
REFERENCE
DURING CLIMB (CONT)
a. Aircraft rate of climb - Fly an
indicated 1000 feet per minute.
b. Read altimeter at beginning of
timing and time for one min-
ute.
c. Read altimeter at end of one
minute. Second reading must
be 1000 200 feet more than
first reading.
*4. Surface deicing system - Check as
follows:
a. Surface deicer switch - SIN-
GLE CYCLE AUTO. Surface
boots should inflate and auto
matically deflate for one cycle.
Wing boots should stay inflated
for 6 seconds. and tail boots
should stay inflated for 4 sec-
onds.
b. Surface deicer switch - Hold to
DEICE MANUAL position.
Roots should stay inflated until
switch is released.
c. Surface deicer switch - Release.
Check boots visually to see that
they are sucked down flat after
use.
C60
*5. Propeller deice system - Check as
follows:
a. Propeller deice switch - Set to
AUTO position.
b. Propeller deicer ammeter -
Monitor for 14 to 18 amperes
2-50

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