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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 ú CONFIG 1 ú 01 Page 605 ú Mar 15/92 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ú CONFIG 1 ú 01 Page 606 ú Mar 15/92 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
(1) 27-51-04/401, Inboard Trailing Edge Flap
(1) Location Zone 309, 409 Wing Trailing Edge Inboard Flap and Spoilers
S 026-002-002 (1) Do this task: "Inboard Trailing Edge Flap Removal" (Ref 27-51-04/401).
(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. ____ 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
