500  Elevator Hinge Wear Limits 
Oct 20/84  Figure 601 (Sheet 3)  27-31-11 
Page 603 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

INDEX NO.  PART NAME  DIM  DESIGN LIMITS  WEAR LIMITS  REPLACE WORN PART  REPAIR WORN PART  REPAIR INSTR. 
DIAMETER  MAX WEAR DIM.  MAX DIAM CLEAR-ANCE 
MIN  MAX 
1  BEARING  ID  0.3120  0.3125  0.3170  0.0050  X 
BOLT  OD  0.3110  0.3120  0.3070  X 
2  BEARING  ID  0.3745  0.3750  0.3825  0.0080  X 
BOLT  OD  0.3735  0.3745  0.3665  X 
3  BEARING  ID  0.3120  0.3130  0.3170  0.0050  X 
BOLT  OD  0.3110  0.3120  0.3070  X 
4  BEARING  ID  0.3745  0.3755  0.3825  0.0080  X 
BOLT  OD  0.3735  0.3745  0.3675  X 

Elevator Hinge Wear Limits  500 
27-31-11  Figure 601 (Sheet 4)  Feb 20/89 
Page 604 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

3. Elevator Control Linkage Wear Limits
G09254
500  Elevator Control Linkage Wear Limits 
May 15/68  Figure 602 (Sheet 1)  27-31-11 
Page 605 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

INDEX NO.  PART NAME  DIM  DESIGN LIMITS  WEAR LIMITS  REPLACE WORN PART  REPAIR WORN PART  REPAIR INSTR. 
DIAMETER  MAX WEAR DIM.  MAX DIAM CLEAR-ANCE 
MIN  MAX 
1  BEARING  ID  0.6245  0.6250  0.6280  0.0040  X 
BOLT  OD  0.6230  0.6240  0.6226  X 
2  BEARING  ID  0.6250  0.6265  0.6295  0.0055  X 
BOLT  OD  0.6230  0.6240  0.6226  X 
3  BEARING  ID  0.8147  0.8157  0.8187  0.0045  X 
BOLT  OD  0.8132  0.8142  0.8128  X  1 
4  BEARING  ID  0.6250  0.6265  0.6295  0.0055  X 
BOLT  OD  0.6230  0.6240  0.6226  X 
5  BEARING  ID  0.6245  0.6250  0.6280  0.0040  X 
BOLT  OD  0.6230  0.6240  0.6226  X 

REPLACE WORN BUSHING ON BOLT ASSEMBLY
G44611
Elevator Control Linkage Wear Limits  500 
27-31-11  Figure 602 (Sheet 2)  May 15/68 
Page 606 
B
O
E
I
NG P
R
OP
RI
E
T
A
R
Y
 - Copyri
ght
 . - Unpubl
i
s
hed W
o
rk
 - S
ee t
i
t
l
e page f
o
r det
ai
l
s
.
 

ELEVATORS - REMOVAL/INSTALLATION
EFFECTIVITY
Airplanes with Graphite Elevators
1.  General
A.  For interchangeability of aluminum/fiberglass elevator with graphite/epoxy elevator, refer to 27-09-800.
B.  Balancing requirements are a function of elevator part number and elevator tab part number. Ensure that balancing requirements for elevator-elevator tab combination to be installed have been met per Chapter 51 of Structural Repair Manual. Elevator rebalancing is required after structural repairs or after repainting.
C.  If an elevator control tab is being installed on the elevator during elevator installation, it is necessary to check that the number of elevator control tab adjust weights installed on the elevator nose corresponds with the required number of adjust weights marked on the elevator tab data plate (Ref 27-31-31, MP).
2. Equipment and Materials
A.  Elevator Sling - C55001
B.  Hoist capable of lifting 200 pounds at a height of 20 feet
C.  Rigging Pins Kit - F70207-3, -52, -61, or -84:
REF NO.  F70207-( )  DIAMETER (INCHES)  LENGTH (INCHES)  FUNCTION 
E-5  -11  0.309-0.3116.7  +0.25  AFT CONTROL QUADRANT 

D.  Trammel Bar - F80055-1
E.  Corrosion Preventive Compound - MIL-C-11796, Class 3 (Ref 20-30-21)
F.  Loading block - 17 inches long, 2 x 4 wood block
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 2(80)