深夜福利✅_秘密教学第57话,你可以帮我吗_.手.动.输.入.网.址.联.系.客.服.人.员.lanan_shell
737-300/400/500MAINTENANCE MANUAL FEEL AND CENTERING UNIT - INSPECTION/CHECK __________________________________________ 1. General_______ A. This subject has one task. The task is an inspection of the feel and centering unit (which is referred to as the "centering unit"). The procedure has these parts: (1) The removal of the centering unit
(2) An inspection of the centering unit
(3) The installation of the centering unit
TASK 27-31-64-206-001 2. Feel and Centering Unit Wear Limits Inspection (Fig. 601)______________________________________________ A. Standard Tools and Equipment (1) Micrometer - 0-1, 1-2 inches
(2) Vernier Caliper
(1) 27-31-64/401, Feel and Centering Unit
SEE A FWD A A A Elevator Feel and Centering Unit Wear Limits Figure 601 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-64 ALL ú ú 01 Page 601 ú Jul 15/91 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 737-300/400/500MAINTENANCE MANUAL D E D E SEEB B 1. BEARING/BOLT
FWD A-A 4. CLEVIS BUSHING/BOLT 5. HOUSING/BEARING 5. HOUSING/ BEARING 6. BEARING/ CRANK SHAFT 3. BEARING/BOLT 6. BEARING/CRANK SHAFT FWD FWD D-D E-E Elevator Feel and Centering Unit Wear Limits Figure 601 (Sheet 2) EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-64 ALL ú ú 01 Page 602 ú Jul 15/91 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 737-300/400/500MAINTENANCE MANUAL NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR. REPAIR DIAMETER DIM. WEAR MITTED PER- DIA MAX ANCE CLEAR- MIN MAX 1 BEARING ID 0.3120 0.3125 0.3155 0.0035 X BOLT OD 0.3110 0.3120 0.3106 X 2 ROD CLEVIS ID 0.3120 0.3130 0.3160 0.0040 X 1 BOLT OD 0.3110 0.3120 0.3106 X 3 BEARING ID 0.3745 0.3750 0.3780 0.0035 X BOLT OD 0.3735 0.3745 0.3731 X 4 CLEVIS BUSHING ID 0.3750 0.3765 0.3795 0.0050 X 2 BOLT OD 0.3735 0.3745 0.3731 X 5 HOUSING ID 1.9375 1.9385 1.9415 0.0040 X BEARING OD 1.9365 1.9375 1.9360 X 6 BEARING ID 0.9990 1.0000 1.0025 0.0035 X CRANK SHAFT OD 0.9985 0.9990 0.9965 X
GET THE BUSHING. BORE THE HOLE TO GET 0.0002 TO 0.0013 INCH INTERFERENCE FIT (0.4379 INCH MAXIMUM). REAM THE BUSHING T0 0.3120/0.3130 INCH DIAMETER REPLACE THE WORN BUSHING Elevator Feel and Centering Unit Wear Limits Figure 601 (Sheet 3)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-31-64 ALL ú ú 01 Page 603 ú Jul 15/91 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 737-300/400/500MAINTENANCE MANUAL C. Access (1) Location Zone 702 Tail Compartment Access Door 704 Tail Cone
(2) Access Panels 3701 Stabilizer Trim Access Door 3801 Tail Cone Access Door, LH 3802 Tail Cone Access Door, RH
S 026-002 (1) 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 3
