RIGHT FUSELAGE AREA (Cont)

Seq .

Seq.

No.

Item and Procedure

No.

Item and Procedur e

4.4

Examine aft landing gear lower drag link for cracks, corrosion,

4.11

Aft exter nal cargo hook for freedom of motion, cleanliness,

blistering or flaking paint. Examine the area within a 3 inch

damage, bumpers and corrosion. Attachment fitting on structure

radius of the forward end, upper and lower bolt holes for evidence

for cleanliness. Hook latch mechanism for locked position and

of cracking. If necessary, clean immediate area to provide more

manual release cable for sufficient clearance between ball fitting

accurate results.

and lever (through inspection window). Electrical harness and

release cable for proper installation, cuts, kinking, or fraying.

4.5

Ground contact proximity switch, bracket, target, and link for

Latch roller for freedom of operation.

security, damage, and excessive play.

4.12

Main and auxiliary fuel tanks for evidence of leaks. Filler caps

4.6

Swivel lock, swivel housing, and power steering actuator

for security. Visible portion of tank vents for damage and

assembly for leaks.

obstruction. Vent fairings for security. Sump drains for leaks.

4.7

Aft brake and hose for leakage, chafing, and damage.

4.13

Static por t for obstruction and damage.

4.8

Aft landing gear wheel for cracks and corrosion. Paint for

4.14

Navigation and NVG lights for condition.

chipping or peeling. Bolts for sealants.

4.15

Refueling station and panel for security of lights, switches, and

4.9

Aft landing gear tire for proper inflation (with gage) and for cuts,

refueling nozzle cap. Check for evidence of fuel leaks.

blisters, slippage, and wear. Refer to TM 55-2620-200-24.

4.16

Forward landing gear support structure for buckling, cracks,

4.10

On helicopters (With 7 4 ), engine water wash system quick

corrosion, loose or missing hardware.

disconnect hoses and tubes for security, damage, chafing

and proper support. Engine work platform support struts for

4.17

Forward landing gear str ut for leaks, cleanliness of exposed

condition, security, and proper operation of pins.

piston, and normal extension (visual).

4.18

Forward landing gear brakes and brake hoses for leaks, chafing,

and damage.

4.19

Forward landing gear wheels for cracks and corrosion. Paint for

chipping or peeling. Bolts for sealant.

"FOD REMINDER"

Check wo rk area for tools and par ts after completion o f maintenance and insp ection.

TM 55-1520-240-PMD