TM 1-1520-238-PM
2–64
PHASE NO.
Date
Aircraft Serial No.
Area Name and No.
MAIN TRANSMISSION – 9
Inspect
Phase
Nos.
Initial
Action Taken
Faults and/or Remarks
Status
Inspection Requirements
ALL
12.
Input shafts, couplings, and drive
flanges for cracks, dents, distortion, and
C
corrosion.
Access L200, R200, LN6, RN6
2,4
13.
Input shaft and coupling bolts for proper
installation.
C
Access L200, R200, LN6, RN6
ALL
14.
Primary hydraulic manifold for leakage,
corrosion, loose connections, and
C
security. Sight gage for proper fluid
level. Check manifold air inlet check
valve filter for cleanliness.
Access L200
ALL
15.
Generators for cleanliness and fod,
smooth and easy rotation. Spline gear
C
and adapter for damage and wear. Gen
seal for leakage.
Access L200, R200
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
