TM 55-1500-345-23
CODE
NO.
DIRECTIONS
WORDING
38
Both sides fuselage at sta 241, WL-34, aircraft
FUSLG JACK
black.
POINT AND
MOORING
POINT UNDER
38
Both sides of fuselage, 1/2inch aircraft black
MOORING
POINT UNDER
letters and arrow, sta 496, WL -28.
39
Aircraft black.
115/208 V 400 CYCLE A.C.
NOTE
Below access door at sta 163, WL-23.
Above external power access panel, sta 169, on
EXT PWR
40
left side, aircraft black.
DC-AC
41
Fwd of external power access panel on left side,
28 V.D.C.
sta 166, 1/2-in. aircraft black letters.
42
Below door jettison handle on left side, sta 93, WL
24, aircraft black.
43
Left side of fuselage aft of cabin window, sta 93,
U.S. ARMY MODEL CH-47A (B, C or D)
WL -11.50. First two lines 1-in, remaining lines 1/2
U.S.A. SERIAL NO. (insert serial no.)
inch aircraft black.
Service this aircraft with MIL-T-83133 grade No.
JP-8 aviation fuel. If not available refer to TB
55-9150-200-24 for alternate fuel.
44
Below lower flight compartment side window in line
with door jettison handle on left side aircraft black.
FOR TACTICAL HELICOPTERS ONLY.
DELETED
45
Figure 9-10. Exterior Markings, CH-47 (Sheet 18 of 29)
9-72
Change 11
