Quantcast RIGHT FUSELAGE AREA (Cont)

 

Click here to make tpub.com your Home Page

Page Title: RIGHT FUSELAGE AREA (Cont)
Back | Up | Next

Click here for thousands of PDF manuals

Google


Web
www.tpub.com

Home


   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Logistics
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
   
   

 

Share on Google+Share on FacebookShare on LinkedInShare on TwitterShare on DiggShare on Stumble Upon
Back
RIGHT FUSELAGE AREA
Up
TM-55-1520-240-PMD CH-47D Helicopter Manual
Next
NOSE AREA
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
11

Privacy Statement - Press Release - Copyright Information. - Contact Us

Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business