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时间:2011-04-06 23:21来源:蓝天飞行翻译 作者:航空
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 (b)  
Compare the dimensions you measured with the permitted dimensions shown in Fig. 601.

 (c)  
Repair or replace the parts that are out of the tolerance.

 

 (3)  
Install the parts.


 S 426-004
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A

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MAINTENANCE MANUAL

SEE A
OVERRIDE MECHANISM CAM FOLLOWER LINK ASSEMBLY
ROLLOUT POWER CONTROL PACKAGE (3 LOCATIONS) FEEL AND CENTERING UNIT BELLCRANK
TUBE ASSEMBLY
CLEVIS
ASSEMBLY
OVERRIDE MECHANISM OUTPUT CRANK
OVERRIDE MECHANISM CAM
CONTROL ROD
ASSEMBLY

FWD
A
D20216
RPCP Mechanical Linkage and Override Mechanism Wear Limits
Figure 601 (Sheet 1)

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A
747-400
MAINTENANCE MANUAL

SEE  B  19.  BEARING/BOLT ASSEMBLY 
20.  BOLT ASSEMBLY TUBE ASSEMBLY/ 
B  21.  BRACKET/BOLT ASSEMBLY 
A  B 
FWD  A  RPCP OUTPUT ARM 

B

RPCP Mechanical Linkage and Override Mechanism Wear Limits
Figure 601 (Sheet 2)

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A
747-400
MAINTENANCE MANUAL

4.  ROD ASSEMBLY/ BOLT
OVERRIDE

ASSEMBLY ASSEMBLY  5. BEARING/BOLT
7.  BUSHING/BOLT ASSEMBLY
A-A
RPCP Mechanical Linkage and Override Mechanism Wear Limits
Figure 601 (Sheet 3)

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A
747-400
MAINTENANCE MANUAL

CRANK OUTPUT  17. ASSEMBLY BEARING/BOLT  18.  CLEVIS ASSEMBLY/ BOLT ASSEMBLY 
C  ASSEMBLY LINK  12. OUTPUT CRANK/ BOLT ASSEMBLY 
OVERRIDE MECHANISM CAM  C  16. 10. SHAFT BEARING/OUTER ASSEMBLY BEARING/BOLT  13. BEARING/BOLT ASSEMBLY LINK ASSEMBLY SHAFT OUTER 
SHAFT INNER 
11. INNER SHAFT/ BEARING 
B-B 
15. LINK ASSEMBLY/ BOLT ASSEMBLY 

14. BEARING/BOLT ASSEMBLY
C-C

RPCP Mechanical Linkage and Override Mechanism Wear Limits
Figure 601 (Sheet 4)

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A
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MAINTENANCE MANUAL

INDEX NO.  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  REPLACE WORN PART  REPAIR WORN PART  REPAIR INSTR 
DIAMETER  DIM. WEAR MITTED PER- DIA MAX CLEAR-ANCE
MIN  MAX 
1  OUTPUT ARM  ID  0.3745  0.3750  0.3755  0.0030  1 
BOLT ASSY  OD  0.3735  0.3745  0.3725  X  3 
2  BEARING  ID  0.3747  0.3750  0.3753  0.0028  2 
BOLT ASSY  OD  0.3735  0.3745  0.3725  X  3 
 
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