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时间:2011-04-21 08:06来源:蓝天飞行翻译 作者:航空
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 27-31-01
 ALL  ú ú 01 Page 602 ú Mar 20/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL

NO. INDEX 1  PART NAME DIM. BUSHING BUSHING OD ID  INCHES MAXIMUM (mm) MINIMUM INCHES DIAMETER DESIGN LIMITS (mm) (14.249) 0.5610 (14.262) 0.5615 (14.293) 0.5627 (14.275) 0.5620  WEAR LIMITS WEAR INCHES DIMENSION PERMITTED (mm) (14.229) 0.5602 (14.326) 0.5640  INCHES CLEARANCE DIAMETER MAXIMUM (mm) (0.064) 0.0025  REPLACE WORN PART X X  INSTR REPAIRREPAIR WORN PART 
2  BUSHING BOLT ID OD  0.3755 (9.525) 0.3750 (9.538) 0.3745 (9.487) 0.3735 (9.512)  0.3755 (9.538) (9.462) 0.3725  (0.076) 0.0030  X X 
3  BUSHING BOLT OD ID  (9.525) 0.3750 (9.540) 0.3756 0.3745 (9.487) 0.3735 (9.512)  (9.591) 0.3776 0.3725 (9.462)  (0.079) 0.0031  X X 
4  BUSHING BUSHING OD ID  0.6877 (17.450) 0.6870 (17.468) 0.6865 (17.424) 0.6860 (17.437)  (17.501) 0.6890 (17.404) 0.6852  (0.064) 0.0025  X X 
5  BUSHING BOLT OD ID  (12.700) 0.5000 (12.713) 0.5005 (12.662) 0.4985 (12.687) 0.4995  (12.764) 0.5025 (12.637) 0.4975  (0.076) 0.0030  X X 
6  BUSHING BUSHING OD ID  (17.450) 0.6870 (17.468) 0.6877 0.6865 (17.424) 0.6860 (17.437)  (17.501) 0.6890 0.6852 (17.404)  (0.064) 0.0025  X X 
7  BUSHING BOLT OD ID  0.5007 (12.700) 0.5000 (12.718) 0.4995 (12.662) 0.4985 (12.687)  0.5027 (12.769) (12.637) 0.4975  (0.081) 0.0032  X X 
8  BUSHING BUSHING OD ID  (17.450) 0.6870 (17.468) 0.6877 0.6865 (17.424) 0.6860 (17.437)  (17.501) 0.6890 (17.404) 0.6852  (0.064) 0.0025  X X 
9  BUSHING BOLT ID OD  (12.700) 0.5000 (12.713) 0.5005 (12.662) 0.4985 (12.687) 0.4995  (12.764) 0.5025 (12.637) 0.4975  (0.076) 0.0030  X X 
10  BUSHING BOLT ID OD  0.5007 (12.700) 0.5000 (12.718) (12.662) 0.4985 (12.687) 0.4995  (12.769) 0.5027 (12.637) 0.4975  (0.081) 0.0032  X X 

Elevator Hinge Wear Limits
Figure 601 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-31-01
 ALL  ú ú 01 Page 603 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 ELEVATOR INDEX PLATE - REMOVAL/INSTALLATION
___________________________________________
 1.  General_______
 A.  This procedure contains steps to remove and install the elevator index plates.
 B.  The steps to remove and install the left index plate are the same as the steps for the right index plate.
 C.  It is important to mark the exact location of the initial index plate before removal. If you can not find the location of the initial index plate, it will be necessary to use special tooling to make sure the index plate is installed in the correct location.
 TASK 27-31-02-024-001
 2.  Remove the Index Plate______________________
 A.  Equipment
 (1)  
Gage Assembly - B27039-3, Part of the
 Elevator/Stabilizer Trim Control Systems
 Rigging Equipment, B27039-1


 B.  
References

 (1)  
06-42-00/201, Empennage Access Doors and Panels

 (2)  
24-22-00/201, Electrical Power - Control

 (3)  
29-11-00/201, Main (Left, Right, and Center) Hydraulic Systems

 C.  
Access

 (1)  
Location Zones 211/212 Control Cabin 311/312 Area Aft of Pressure Bulkhead to BS 1787.45 315/316 Auxiliary Power Unit Compartment

 (2)  
Access Panels
 311AL Forward Stabilizer Compartment
 315AL Auxiliary Power Unit
 316AR Auxiliary Power Unit


 D.  
Prepare for the Removal

 (1)  
Supply electrical power (Ref 24-22-00).


 S 864-002
 S 864-003
 WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES WHEN
_______ HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS, AND STABILIZER ARE FULLY POWERED SURFACES. INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS SUPPLIED.
 (2) Pressurize the right and center hydraulic systems (Ref 29-11-00).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
 
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