TM 1-1520-238-PM
2–23
PHASE NO.
Date
Aircraft Serial No.
Area Name and No.
LEFT FORWARD AVIONICS BAY AND MLG – 3
Inspect
Phase
Nos.
Initial
Action Taken
Faults and/or Remarks
Status
Inspection Requirements
2,4
8.
MLG trailing arm for cracks, distortion,
or corrosion. Cross tube end pivot boss
C
for security, damaged or worn bearing,
loose or missing hardware. Hydraulic
brake line for leakage, dents, corrosion,
and clamping security.
Access L115
ALL
9.
MLG end cap for cracks, distortion,
fractured weld, and elongated bolt holes.
C
ALL
10.
MLG SHOCK STRUT UPPER AND
LOWER ROD ENDS FOR BEARING
C
DAMAGE.
2,4
11.
MLG wheel for cracks, distortion, or
corrosion. Hub for grease leakage. Tire
C
for tread damage or uneven wear.
“FOD REMINDER”
Check work area for tools and parts after completion of maintenance and inspection.
