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BEFORE LANDING - TM-55-1510-218-MTF0081
Up
TM-55-1510-218-MTF Maintenance Test Flight Manual Army Model C-12C C-12D and C-12F Aircraft
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AFTER LANDING - TM-55-1510-218-MTF0083
TM 55-1510-218-MTF
TROUBLESHOOTING
PROCEDURE
REFERENCE
LANDING (CONT)
*4. Brake operation - Check during
landing roll for any tendency to
bleed down, drag after release or
indicate  assymmetrical braking
power.
*5. Propeller reversing - Check as fol-
E3.5
lows:
a. During landing utilize maxi-
mum reverse power.
b. Check for smoothness of opera-
tion and equal thrust from en-
gines.
*c. Turbine tachometers - Maxi-
mum reverse N1 should be 82
to 88%. Maximum difference
between engines should be 2%
N1.
*6. Oil temperature - Monitor. Ground
idle limits are 10 to 99C.
*7. Oil pressure - Monitor. Ground
idle limits arc 60 PSI minimum.
GO-AROUND
1. Power - As required.
2. Landing gear control switch - UP.
3. Flap switch - UP.
4. Landing lights - OFF.
5. Climb power - Set.
6. Yaw damp - As required.
7. Brake deice - OFF.
2-72

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