C. Procedure
S 012-032-B00
(1)
Do this task: Get Access to the Hinges for the Thrust Reverser.
S 492-003-B00
(2)
Put the bearing replacement tool (punch and anvil assemblies) on the applicable hinge fitting.
(3)
Remove the vibration isolator with the hand pump.
(4)
Remove the tool from the hinge fitting.
S 022-004-B00
S 092-005-B00
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
54-42-13
ALL ú ú B07 Page 213 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
TASK 54-42-13-422-001-B00
6. Roller Swage Vibration Isolator Installation, Forward and Center Fitting________________________________________________________________________ (Fig. 202, 203)
A. Equipment
(1)
MIT311A1550 - Bearing Replacement Tool Kit
(2)
Hand Pump
B. Access
(1) Location Zones
500 Left Nacelle
600 Right Nacelle
C. Procedure
S 492-007-B00
(1) Put the bearing replacement tool and the new vibration isolator on the applicable hinge fitting.
(a) Use the pressure plate and spacer bushing from the tool kit.
S 422-008-B00
CAUTION:_______USE THE CORRECT VIBRATION ISOLATOR. THE VIBRATION ISOLATORS FOR THE FORWARD AND THE CENTER HINGE FITTINGS ARE DIFFERENT. IF YOU DO NOT USE THE CORRECT VIBRATION ISOLATOR, DAMAGE TO THE THRUST REVERSER OR THE STRUT CAN OCCUR.
(2)
Install the vibration isolator with the hand pump.
S 092-009-B00
(3)
Remove the tool from the hinge fitting.
S 022-073-B00
(4)
With the roller staking assembly, stake the vibration isolator into the hinge fitting.
S 212-011-B00
(5)
Examine the vibration isolator to make sure it is installed correctly.
(6)
Remove the staking tool from the hinge fitting.
S 092-012-B00
TASK 54-42-13-202-077-B00
7. Hinge Fitting Examination, Aft Fitting (Fig. 204)______________________________________
A. References
(1) AIPC 54-42-50
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
54-42-13
ALL ú ú B07 Page 214 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
B. Access
(1) Location Zones
500 Left Nacelle
600 Right Nacelle
C. Procedure
S 012-078-B00
(1)
Do this task: Get Access to the Hinges for the Thrust Reverser.
S 212-079-B00
(2)
Examine the hinge fitting for damage (SRM 54-50-90).
S 212-080-B00
(3)
Examine the bushings for wear or damage.
(a) If the bushings are damaged, replace the bushings (CMM 54-50-01).
(4)
Do this task: Put the Airplane Back to Its Usual Condition.
S 412-089-B00
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
54-42-13
ALL ú ú B06 Page 215 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
~.............................................................................. | Bolt Gap/Dimensions AIPC 54-42-50-01A | ................................................................................ | AMM | | | | IPC | |Fig. 203 Item # | Part | Name | Min Max | Item # | ................................................................................ | 41 |311A1563 |Bushing | 2.357 | 2.383 |140 | ................................................................................ | 39 |311A1563 |Washer | 0.092 | 0.108 |125 | ................................................................................ | 43 |BACW10BP6ACU |Washer | 0.057 | 0.069 |130 | ................................................................................ | 42 |BACJ40AD47 |Jumper | 0.050 | 0.080 | | ................................................................................ | |STACKUP | | 2.556 | 2.639 | | ................................................................................ | | | | | | | ................................................................................ | 32 |BACB30LE6U42 |Bolt Shank | 2.615 | 2.635 |120 | ................................................................................ | 31 |Gap (None) |See Note | 0.00 | 0.00 | | ................................................................................ | 34 |311A1553 |Fitting | 2.055 | 2.085 |150 | ................................................................................ | 33 |BACW10B8APU |Washer | 0.064 | 0.078 |100 | ................................................................................ | 32 |311A1563 |Bolt Shank | 2.165 | 2.185 |95 | ................................................................................ | 36 |311A1563 |Washer | 0.064 | 0.078 |110 | ................................................................................ | |Required GAP | | 0.002 | 0.066 | | 2................….............…............…............…............…........1
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 NACELLES/PYLONS(52)