TM 55-1520-240-PM
PHASE NO. _____
Area Name and No.
Aircraft Serial No.
Date
NOSE AREA #1
Inspect
Phase
No’s
Inspection Requirements
Status
Faults and/or Remarks
Action Taken
Initial
ALL
1.10 Electrical wiring and connectors
for security, visible through right and left
chin bubble windshield panels or nose
access door. Wires for evidence of
chafing, proper support, and condition
of insulation. Terminal boards for
condition and proper installation
of covers. Visible pitot-static and
AFCS sideslip port tubing for proper
connection and support and not kinked.
Access 29
ALL/C
1.11 Dynamic absorber for security.
Support structure for cracks and loose
or missing hardware. Access 29
ALL/C
1.12 Entire area for structural damage,
skin cracks, loose or missing rivets,
dents and evidence of corrosion. Paint
for chipping or peeling. Stencil and
decals for condition.
ALL/C
1.13 Inspect and lubricate the pedal
box bearings only if they are removed
from the aircraft for other maintenance.
2, 4
1.14 Inspect ducting for security of
clamps, cuts, chaffing, and FOD.
Access door and seal for cuts,
damage, security, distortion, and
wear. Access 77
"FOD REMINDER"
Check work area for tools and parts after completion of maintenance and inspection.
2-5
