TM 1-1520-238-23
11-685
11.154. PILOT DIRECTIONAL SHEAR PIN ACTIVATED DECOUPLER (SPAD) ASSEMBLY
DISASSEMBLY/ASSEMBLY (AVIM) – continued
b. Install lever (30) on bellcrank (2).
(1) Aline lever (30) with bellcrank (2).
(2) Install bushing (37) in lever (30).
(3) Install bolt (35) through washer (36), bushing
(37), lever (30), and bellcrank (2).
(4) Check fit of self-retaining bolt (35) (para
11.1).
(5) Install washer (34) and nut (33).
(6) Install new cotter pin (32).
(7) Install
rivet
(31)
in
lever
(30)
(TM 1-1500-204-23).
c. Install arm (22) on bellcrank (2).
(1) Aline arm (22) with bellcrank (2).
(2) Install bushing (29) in arm (22).
(3) Install bolt (27) through washer (28), bushing
(29), arm (22), and bellcrank (2).
(4) Check fit of self-retaining bolt (27) (para
11.1).
(5) Install washer (26) and nut (25).
(6) Install new cotter pin (24).
(7) Install
rivet
(23)
in
arm
(22)
(TM 1-1500-204-23).
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M04-4312-15
32
33
2
37
36
35
30
34
31
M04-4312-16
27
28
29
2
22
24
25
26
23
