TM 1-1520-238-23
2-362.2
Change 5
2.99A.
STRUCTURAL ASSEMBLY (DOPPLER MOUNT) REMOVAL/INSTALLATION continued
M04-5187-2
7
6
5
4
10
11
12
1
9
14
13
3
2
4
5
7
6
8
3
(2 PLCS)
(8 PLCS)
(2 PLCS)
2.99A.3. Removal
a. Remove mount (1) from fuselage (2).
(1) Remove wire harness W203 (3) from mount (1).
(a) Remove four screws (4), washers (5), clamps (6), and spacers (7) from mount (1).
(b) Remove harness (3) from mount (1).
(2) Remove wire harness W213 (8) from mount bracket (9).
(a) Remove screw (10), washer (11), and clamp (12) from bracket (9).
(b) Remove harness (8) from bracket (9).
(3) Remove eight screws (13) and washers (14) from mount (1).
CAUTION
Reposition W203 wire harness and W213 wire harness so mount can be removed without interfer-
ence, or damage to wire harness may occur.
(4) Remove mount (1).
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