S 226-009
(3)
Measure the parts of the standby rudder actuator for worn areas.
S 226-010
(4)
Compare the dimensions that you measured with the permitted dimensions shown in Figure 601.
S 436-011
(5)
Replace or repair the parts that are not in the tolerance.
S 426-012
(6)
Install the standby rudder actuator (AMM 27-21-24/401).
TASK 27-21-24-216-015
3. Standby Rudder Actuator Visual Inspection (Fig. 602)
_________________________________________
A. Access
(1)
Location Zones
706 Vertical Fin
708 Rudder
(2)
Access Panels
9515L TE Access Panel - Rudder
9528R Access Door - Rudder
9529R Access Door - Rudder
B.
Procedure
S 016-016
(1)
Open these access panels to get access to the stanby rudder actuator: 9515L, 9528R, and 9529R.
(2)
Do a general visual inspection of the standby rudder actuator.
S 216-017
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-24
ALL ú ú 01 Page 606 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 416-018
(3) Close these access panels: 9515L, 9528R, and 9529R.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-24
ALL ú ú 01 Page 607 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
RUDDER PEDAL ASSEMBLIES - REMOVAL/INSTALLATION
______________________________________________
TASK 27-21-31-004-003
1. Remove the Rudder Pedal Assembly________________________________
A. Special Tools and Equipment
(1) F70207-93 Rig Pin Kit:
~........................................................................ | | F70207 | DIAMETER | LENGTH | | | REF NO. | -( ) | (INCHES) | (INCHES) | FUNCTION | .......................................................................... | R-1 | -14 | 0.309-0.311 | 12.7 |0.25 | RUDDER PEDAL ARMS | | | | | | | | R-2 | -14 | 0.309-0.311 | 12.7 |0.25 | RUDDER PEDAL ARMS | | | | | | | | R-3 | -11 | 0.309-0.311 | 6.7 |0.25 | RUDDER FORWARD QUADRANT | | | | | | | | R-4 | -11 | 0.309-0.311 | 6.7 |0.25 | RUDDER FORWARD QUADRANT | 2.........….........….............…............….........................1
B. Standard Tools and Equipment
(1)
Ruler - 2 feet long, graduated hundredths of an inch, Commercialy Available
C.
Consumable Materials
(1)
C00528 Compound - Corrosion Preventive, MIL-C-11796, Class 3
D.
References
(1)
27-21-00/201, Rudder and Rudder Trim Control Systems
E.
Access
(1)
Location Zones
101/102 Control Cabin
202 Lower Nose Compartment
203 Nose Wheel Well
F.
Prepare for Removal
S 014-007
(1)
Open the forward access door (1103) to get access to the nose compartment.
(2)
Remove the forward access panels from the nose wheel well.
S 014-008
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-31
ALL ú ú 01 Page 401 ú Nov 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
G. Remove the Rudder Pedal Assembly
S 484-012
(1)
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 2(46)
