TM 55-1500-345-23
CODE
NO.
DIRECTIONS
WORDING
149
Both sides of aft pylon inside reservoir cooler
REMOVE BONDING JUMPER
access covers, 1/2-in. aircraft black letters.
WHEN DOOR IS TO BE REMOVED
INSTALL BONDING JUMPER
WHEN INSTALLING DOOR
150
Both sides aft pylon, 1/2-in. aircraft black letters,
ACCESS HYDRAULIC
sta 525.80, WL 84.50.
COMPARTMENT
151
Both sides of aft pylon, 1/2-in. aircraft black letters,
FRAGILE ANTENNA
sta 613.70, WL 102.0.
DO NOT PUSH
152
Right side aft fuselage, 1/2-in. aircraft black letters,
GROUND TEST CONNECTION
sta 565.25, WL 15.50.
FLIGHT CONTROL SYSTEM 2
3000 PSI
USE HYDRAULIC FLUID
MIL-H-83282
153
Both engine cowlings, fwd of screened air intake,
ACCESS
1/2-in. aircraft black letters, sta 486, WL 46.
ENGINE QUICK
DISCONNECTS
154
Right side aft pylon, 1/2-in. aircraft black letters,
RS ENGINE XMSN
sta 472, WL 73.
FILTER AND DRAIN ACCESS
155
Right side aft pylon, 1/2-in. aircraft black letters,
ACCESS HYDR
sta 505, WL 27.
COOLING FANS
156
Front of aircraft, 1/2-in. aircraft black letters, center,
NO HAND HOLD
WL 41.
157
Bottom of fusleage, both sides, 1/2-in. aircraft
FUEL DRAIN - VENT
black letters, sta 434, 368, 233, BL 53.
158
Both sides of fuselage, 1/2-in. aircraft black letters,
FUEL DRAIN
sta 395, 267, 194, BL 53.
Figure 9-10. Exterior Markings, CH-47 (Sheet 29 of 29)
Change 11
9-83
