Exhaust Gate Actuation Mechanism Wear Limits Figure 601 (Sheet 4)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THREE EXHAUST GATE ú
27-51-04
PUSHRODS. ú CONFIG 1 ú 01 Page 605 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A12094
A 737-300/400/500MAINTENANCE MANUAL
INDEX NO. PART NAME DIM. DESIGN LIMITS WEAR LIMITS REPLACE WORN PART REPAIR WORN PART REPAIR INSTR
DIAMETER DIM. WEAR MITTED PER- DIA MAX CLEAR-ANCE
MIN MAX
15 BEARING ID 0.3743 0.3750 0.3775 0.0030 X
BOLT OD 0.3735 0.3745 0.3713 X
16 BUSHING ID 0.3750 0.3756 0.3787 0.0042 X
BOLT OD 0.3735 0.3745 0.3708 X
17 BUSHING ID 0.2500 0.2505 0.2535 0.0040 X
BOLT OD 0.2485 0.2495 0.2460 X
18 BEARING ID 0.2495 0.2500 0.2525 0.0030 X
BOLT OD 0.2485 0.2495 0.2465 X
19 BUSHING ID 0.3750 0.3756 0.3777 0.0032 X
BUSHING OD 0.3740 0.3745 0.3718 X
20 BUSHING ID 0.2500 0.2505 0.2535 0.0040 X
BOLT OD 0.2485 0.2495 0.2460 X
21 BEARING ID 0.2495 0.2500 0.2525 0.0030 X
BOLT OD 0.2485 0.2495 0.2465 X
22 BUSHING ID 0.3750 0.3756 0.3777 0.0032 X
BUSHING OD 0.3740 0.3745 0.3718 X
23 BUSHING ID 0.2500 0.2505 0.2535 0.0040 X
BOLT OD 0.2485 0.2495 0.2460 X
24 BEARING ID 0.2495 0.2500 0.2525 0.0030 X
BOLT OD 0.2485 0.2495 0.2465 X
25 BUSHING ID 0.3750 0.3756 0.3770 0.0032 X
BUSHING OD 0.3740 0.3745 0.3718 X
26 BUSHING ID 0.2500 0.2505 0.2535 0.0040 X
BOLT OD 0.2485 0.2495 0.2460 X
27 BEARING ID 0.2495 0.2500 0.2525 0.0030 X
BOLT OD 0.2485 0.2495 0.2465 X
Exhaust Gate Actuation Mechanism Wear Limits Figure 601 (Sheet 5)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THREE EXHAUST GATE ú
27-51-04
PUSHRODS. ú CONFIG 1 ú 01 Page 606 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A12095
A
737-300/400/500MAINTENANCE MANUAL
INBOARD TRAILING EDGE FLAP - INSPECTION/CHECK
_____________________________________________
1. General_______
A. This procedure contains one task: an inspection of the inboard trailing edge flap. To do this check you measure the diameters of parts of the exhaust gate actuator mechanism.
TASK 27-51-04-206-001-002
2. Inboard Trailing Edge Flap Inspection_____________________________________
A. Standard Tools and Equipment
(1)
Micrometer - 0 to 1 inch
(2)
Micrometer - 1 to 2 inch
B.
References
(1)
27-51-04/401, Inboard Trailing Edge Flap
C.
Access
(1)
Location Zone 309, 409 Wing Trailing Edge Inboard Flap and Spoilers
D.
Procedure
S 026-002-002
(1)
Do this task: "Inboard Trailing Edge Flap Removal" (Ref 27-51-04/401).
S 226-003-002
(2)
Examine the exhaust gate actuator mechanism for worn parts:
(a)
Remove the parts to be examined.
(b)
Measure the parts.
NOTE: Use a micrometer to measure the parts.
____
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 4
