TM 55-1500-345-23
CODE
NO.
DIRECTIONS
WORDING
64
DELETED
65
Both sides of fuselage centered on access plate,
ACCESS FUEL
aircraft black. Sta 381, 449.
SYSTEM INSP
66
Left and right aft work platform, centered on
WORK PLATFORM
platform at WL -2.50, black letters.
67
WORK
Both sides of fuselage, fore and aft of work platform
PLATFORM
above support point at sta 474.0 and 521.0, WL
SUPPORT
-6.0 black letters.
POINT
68
Both sides of fuselage, sta 485, WL -34. 1/2-in.
COMPT DRAINS
black letters as required per model helicopter.
UNDER
69
Left side of fuselage, sta 546.50, WL 15, black
ACCESS
letters.
APU EMERG
FLUID SHUT OFF
70
Left side of fuselage, sta 543, WL 50. First line
ENGINE
1-in. black letters, remaining letters 1/4-in., located
DRAINS
in front of each overboard drain tube.
*STARTER RELIEF
VALVE DRAIN
HYDRAULIC DRAIN
NOTE
AFT XMSN DRIP PAN
ENGINE COMB CHAMB
Applicable on CH-47, serial No. 67-18494
ENGINE BREATHER
and subsequent.
ENGINE MANF
71
Both sides of engine cowling below screened air
ACCESS ENGINE
intake, sta 486, WL 46.0, black letters.
QUICK
DISCONNECT
72
Both sides of rear pylon, sta 471, WL 79, black
AIRCRAFT
LIFT PTS
letters.
INSIDE
Figure 9-10. Exterior Markings, CH-47 (Sheet 21 of 29)
Change 11
9-75
