69-53208-501 NAS 537B9P-34
NYLON WEAR X1 (CLEVIS TO ROD
WASHER(S) CLEVIS BEARING HOUSING) FWD
B A-A
Standby Rudder Actuator Wear Limits
Figure 601 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-24
ALL ú ú 01 Page 602 ú Mar 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
INDEX NO. 1 BOLT ROD END PART NAME DIM. ID OD (6.338) 0.2495 0.2495 0.2500 (6.338) (6.350) (6.312) 0.2485 (mm) DESIGN LIMITS DIAMETER INCHES MINIMUM (mm) MAXIMUM INCHES (6.287) 0.2475 (6.375) 0.2510 (mm) PERMITTED DIMENSION INCHES WEAR WEAR LIMITS (0.0635) 0.0025 (mm) MAXIMUM DIAMETER CLEARANCE INCHES PART WORN REPLACE X X PART WORN REPAIR REPAIR INSTR
2 BOLT CLEVIS OD ID (6.363) 0.2505 0.2495 (6.338) (6.350) 0.2500 (6.312) 0.2485 (6.287) 0.2475 (6.388) 0.2515 (0.0762) 0.0030 X X 1
3 BOLT ROD END ID OD (15.850) 0.6240 0.6250 (15.875) (15.824) 0.6230 (15.862) 0.6245 (15.723) 0.6190 (15.951) 0.6280 (0.1016) 0.0040 X X
4 BOLT CLEVIS ID OD (15.850) 0.6240 (15.913) 0.6265 (15.875) 0.6250 (15.824) 0.6230 (15.723) 0.6190 (16.015) 0.6305 (0.1651) 0.0065 X X 2
5 BOLT ROD BEARING ID OD (14.262) 0.5615 (14.288) 0.5625 (14.237) 0.5605 (14.275) 0.5620 (14.199) 0.5590 (14.313) 0.5635 (0.0889) 0.0035 X X
6 BOLT CLEVIS ID OD (14.262) 0.5615 (14.288) 0.5625 (14.275) 0.5620 (14.237) 0.5605 0.5590 (14.199) (14.313) 0.5635 0.0035 (0.0889) X X 3
GET A BUSHING. DRILL THE HOLE IN THE CLEVIS TO MAKE A 0.0000 TO 0.0010 INCH (0.000 TO 0.025 mm) INTERFERENCE FIT WITH THE BUSHING. THE MAXIMUM SIZE HOLE IN THE CLEVIS IS 0.3754 INCH (9.535 mm). REAM THE BUSHING TO A 0.2500-0.2505 INCH (6.350-6.363 mm) DIAMETER.
REPLACE THE WORN BUSHING.
REPLACE THE WORN BUSHING (SEE A-A), IT IS A SHRINK FIT INSTALLATION (REF. OHM, 20-50-03). REPLACE THE STEEL WEAR PLATE THAT IS BELOW THE UPPER BUSHING FLANGE WITH A NEW WEAR PLATE ATTACHED WITH BMS 5-95 SEALANT.
Standby Rudder Actuator Wear Limits
Figure 601 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-24
ALL ú ú 01 Page 603 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE A
FWD
STANDBY RUDDER ACTUATOR
SEE B
FWD
A
Standby Rudder Actuator Visual Inspection
Figure 602 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-24
ALL ú ú 02 Page 604 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
M13995
A 737-300/400/500MAINTENANCE MANUAL
VERTICAL FIN
STANDBY RUDDER ACTUATOR
RUDDER
FWD
VERNIER
CONTROL ROD
STANDBY RUDDER ACTUATOR
B
Standby Rudder Actuator Visual Inspection
Figure 602 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-24
ALL ú ú 01 Page 605 ú Jul 12/01
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 2(45)