TM 55-1520-240-PM
PHASE NO. _____
Area Name and No.
Aircraft Serial No.
Date
RAMP AREA #8
Inspect
Phase
Nos
Inspection Requirements
Status
Faults and/or Remarks
Action Taken
Initial
ALL
8.20 No. 2 Flight boost hydraulic pump
and hoses for leaks.
ALL
8.21 Utility hydraulic pump and hoses
for leaks.
ALL
8.22 APU start accumulator housing,
manifold, and mount fitting for leaks,
damage, cracks, and security. Adjacent
structure for buckling and cracks.
ALL
8.23 Transmission mounted generators
(left and right) for security of mounting,
loose or missing hardware, and
evidence of oil leaks. Wiring for security
of attachment and evidence of chafing.
Terminal covers for cracking and proper
installation.
ALL
8.24 Utility hydraulic pressure control
module housing for leakage. Mount
structure for cracks, buckling, and
damage.
4
8.25 Replace utility system filter
elements at 800 hours.
ALL
8.26 APU electronic control unit and
mount for condition and security.
Electrical wiring and connectors for
damage, chafing and security.
"FOD REMINDER"
Check work area for tools and parts after completion of maintenance and inspection.
2-60