(9)
Install access panels 9512, 9514, and 9515.
(10)
Install the hinge coverplates and fairings.
S 224-047
S 414-048
S 434-049
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
AIRPLANES WITH GRAPHITE/COMPOSITE RUDDER ú 27-21-11
ú ú 02 Page 413 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
RUDDER - INSPECTION/CHECK
_________________________
1. General_______
A. This procedure gives you the instructions to make sure the hinges for the rudder are not worn too much.
TASK 27-21-11-226-006
2. Rudder Wear Limits (Fig. 601)__________________
A. Standard Tools and Equipment
(1)
Micrometer
(2)
Vernier Caliper
B.
References
(1)
27-21-21/401, Rudder Hinges
C.
Access
(1)
Location Zones
708 Rudder
(2)
Access Panels
9555R Cover - Rudder Nose
9556L Cover - Rudder Nose
9557R Cover - Rudder Nose
9559R Cover - Rudder Nose
9560L Cover - Rudder Nose
9561R Cover - Rudder Nose
9562L Cover - Rudder Nose
9563R Cover - Rudder Nose
9564L Cover - Rudder Nose
9565R Cover - Rudder Nose
9566L Cover - Rudder Nose
9567R Cover - Rudder Nose
9568L Cover - Rudder Nose
D.
Procedure
(1)
Remove the rudder hinge that you will examine (Ref 27-21-21/401).
(2)
Measure the parts of the rudder hinge for worn areas.
S 226-003
(3)
Compare the dimensions that you measured with the permitted dimensions shown in Figure 601.
(4)
Replace or repair the parts that are not in the tolerance.
(5)
Install the rudder hinge (Ref 27-21-21/401).
S 026-001
S 226-002
S 436-005
S 426-004
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-11
ALL ú ú 02 Page 601 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
HINGE 7, SEE C
VERTICAL FIN HINGE 6, SEE C
HINGE 5, SEE C
RUDDER
HINGE 4, SEE C
HINGE 3, SEE C
HINGE 2, SEE B
HINGE 1, SEE A
2. BEARING/ BOLT
1. BUSHING/BOLT
(2 LOCATIONS)
12. BUSHING/ BOLT
9. BUSHING/ BUSHING
BEARING BAR
10. BUSHING/ BOLT
1
11. BUSHING/
BOLT FWD
HINGE 1
A
1THE DIMENSIONS ARE THE SAME FOR EACH END OF THE BEARING BAR
Rudder Wear Limits Figure 601 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-21-11
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
BOLT4. BEARING/
(2 LOCATIONS) 3. BUSHING/BOLT
BOLT 16. BUSHING/
13. BUSHING/ BUSHING
BAR BEARING 1 BOLT15. BUSHING/ BOLT14. BUSHING/
FWD
HINGE 2
B
20,24,28,32,36. BUSHING/BOLT
19,23,27,31,35. BUSHING/BUSHING BOLT 6,8. BEARING/ 18,22,26,30,34. BUSHING/BOLT 17,21,25,29,33. BUSHING/BUSHING
5,7. BUSHING/ BOLT
FWD 20,24,28,32,36. BUSHING/BOLT
EXAMPLE HINGES 3,4,5,6,7
C
1 THE DIMENSIONS ARE THE SAME FOR EACH END OF THE BEARING BAR Rudder Wear Limits Figure 601 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú 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(32)