54-10-00
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A
737-300/400/500MAINTENANCE MANUAL
NACELLE STRUT - INSPECTION/CHECK
________________________________
1. General_______
A. The nacelle strut inspection is a check for the wear limits on the nacelle strut components.
B. To do the inspection of the nacelle strut (Fig. 601), you must remove the strut.
TASK 54-10-00-216-001-B00
2. Inspect the Nacelle Strut_________________________
A. References
(1) 54-10-00/401, Nacelle Strut
B. Access
(1) Location Zone
500 Left Nacelle
600 Right Nacelle
C. Procedure
S 016-002-B00
(1) Remove the strut (Ref 54-10-00/401).
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A 737-300/400/500MAINTENANCE MANUAL
STRUT
FWD
STA 194.24 (REF) ASSEMBLY STRUT PIN SEE A UPPER LINK FUSE PIN BSEE SPAR (REF) WING FRONT FUSE BOLT SEE C
POINT SLING ATTACH POINT SLING ATTACH SEE SIDE LINK F SEE PIN E DIAGONAL BRACE FUSE PIN SEE D
FWD
Nacelle Strut Wear Limits
Figure 601 (Sheet 1)
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A 737-300/400/500MAINTENANCE MANUAL
REFER TO CMM 54-50-01 REFER TO SRM 54-50-90REFER TO SRM 57-20-90
Nacelle Strut Wear Limits Figure 601 (Sheet 2)
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A
737-300/400/500MAINTENANCE MANUAL
BUSHING/ BUSHING
Nacelle Strut Wear Limits
Figure 601 (Sheet 3)
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A 737-300/400/500MAINTENANCE MANUAL
INDEX NO. PART NAME DIM. DESIGN LIMITS WEAR LIMITS REPLACE PART WORN REPAIR WORN PART REPAIR INSTR.
DIAMETER WEAR DIM. ALLOWED DIAM CLEAR-ANCE MAX
MIN MAX
1 RACE ID 2.6765 2.6775 2.6805 0.006 X
BALL OD 2.6735 2.6745 X
2 BALL ID 1.8015 1.8030 1.8057 0.008 X
FUSE PIN OD 1.7995 1.8000 1.7968 X
3 BUSHING ID 1.8015 1.8030 1.8051 0.0056 X
FUSE PIN OD 1.7995 1.8000 1.7974 X 1
4 RACE ID 2.6765 2.6775 2.6805 0.006 X
BALL OD 2.6735 2.6745 X
5 BALL ID 1.8015 1.8030 1.8057 0.008
FUSE PIN OD 1.7995 1.8000 1.7968
6 BUSHING ID 1.3665 1.3680 1.3703 0.0053 X
FUSE PIN OD 1.3650 1.3660 1.3627 X 1
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