NO. 1 ENGINE AREA (LOWER SECTION)

Seq .

Seq.

No.

Item and Procedure

No.

Item and Procedur e

6.20

Swivel lock and swivel housing for leaks.

NO. 1 ENGINE AREA (LOWER SECTION)

6.21

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

NOTE

With engine air par ticle separators (EAPS) installed, it is not

6.22

Aft landing gear wheel for cracks and corrosion. Paint for

necessary to inspect the engine air inlet nor is it necessary

chipping or peeling. Bolts for sealant.

to open the engine cowling during the daily inspection. Use

6.23

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

a flashlight and inspect through the openings in the engine

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

cowling. All filter buttons are visible using a flashlight. It is

only necessar y to slide EA PS forward ever y 25 flight hours

6.24

Static ground wire for security and ground contact.

or whenever there is a suspected compressor stall, surge,

6.25

Fluid drain lines for damage and obstructions.

signs of oil coming from inlet, or if other non-scheduled or

scheduled maintenance is required.

6.26

Access doors, work platfor ms, and panels for damage. Latching

mechanisms for secur ity and proper operation. Seals for cuts,

7.1

Engine inlet screen for cleanliness, cracks, damage, loose

tears, cracks and security. Engine wor k platform support str uts

hardware, and proper installation.

for secur ity, twisting, and proper operation of pins.

7.2

Engine inlet housing and ducts for cleanliness, foreign object

6.27

Entire area for str uctural damage, skin cracks, dents or buckling,

damage, and debris. Visible area of compressor blades and

loose or missing r ivets, and evidence of corrosion. Paint for

stators for damage and foreign materials. On helicopters

chipping or peeling. Stencils and decals for condition.

(Without 74 ), refer to TM 55-2840-254-23. On helicopters (With

74 ), refer to TM 1-2840-265-23.

7.3

Main fuel filter bypass indicator for extension. If bypass has

occurred, inspect for contaminated fuel system. On helicopters

(Without 74 ), refer to TM 55-2840-254-23. On helicopters (With

74 ), refer to TM 1-2840-265-23.

"FOD REMINDER"

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

TM 55-1520-240-PMD