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时间:2010-08-23 15:50来源:蓝天飞行翻译 作者:admin
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SUBTASK 27-31-41-860-003
(5) Do this task: Put the Elevator Systems A and B Back to the Condition Before the Pressure
Removal, TASK 27-31-00-840-802.
SUBTASK 27-31-41-710-001
(6) Do this task: Elevator Balance Panels - Test, TASK 27-31-00-700-803.
SUBTASK 27-31-41-010-004
(7) Install this access panel:
Number Name/Location
318BR Tailcone Access Door
SUBTASK 27-31-41-410-001
(8) For the left elevator, install these access panels:
Number Name/Location
333BB Horizontal Stabilizer, Access Panel, Trailing Edge
333CB Horizontal Stabilizer, Access Panel, Trailing Edge
333DB Horizontal Stabilizer, Access Panel, Trailing Edge
333EB Horizontal Stabilizer, Access Panel, Trailing Edge
SUBTASK 27-31-41-410-002
(9) For the right elevator, install these access panels:
Number Name/Location
343BB Horizontal Stabilizer, Access Panel - T.E. Area
343CB Horizontal Stabilizer, Access Panel - T.E. Area
343DB Horizontal Stabilizer, Access Panel - T.E. Area
343EB Horizontal Stabilizer, Access Panel - T.E. Area
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-41
Page 410
Oct 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
ELEVATOR BALANCE PANEL - INSPECTION/CHECK
1. General
A. This task supplies the data for a dimensional inspection of the elevator balance panel.
B. This task does not remove or install the rudder. Refer to the Elevator Balance Panel - Removal/
Installation for procedures to remove and install the elevator balance panel.
TASK 27-31-41-200-801
2. Elevator Balance Panel - Inspection
(Figure 601)
A. General
(1) This procedure gives wear limits and repair data for the elevator balance panel.
B. References
Reference Title
27-31-41-000-801 Elevator Balance Panel - Removal (P/B 401)
27-31-41-400-801 Elevator Balance Panel - Installation (P/B 401)
C. Tools/Equipment
Reference Description
STD-1096 Micrometer - Depth, 0-1 Inch, Readable to 1/1000 Inch
STD-1097 Caliper - Vernier, 0-6 Inch, Readable to 1/1000 Inch
D. Location Zones
Zone Area
334 Left Horizontal Stabilizer - Elevator
344 Right Horizontal Stabilizer - Elevator
E. Procedure
SUBTASK 27-31-41-020-005
(1) Remove the elevator balance panel. To remove it, do this task: Elevator Balance Panel -
Removal, TASK 27-31-41-000-801.
SUBTASK 27-31-41-020-006
(2) Use these tools to check for wear on the parts of the elevator balance panel connections:
(a) micrometer (0-1 Inch, readable to 1/1000 Inch), STD-1096
(b) readable to 1/1000 inch vernier 0 - 6 inch caliper, STD-1097.
SUBTASK 27-31-41-020-007
(3) Examine the parts of the elevator balance panel connections for worn areas:
(a) Remove the parts to be checked.
(b) Measure the parts, as necessary, with a micrometer (0-1 Inch, readable to 1/1000 Inch),
STD-1096 or a readable to 1/1000 inch vernier 0 - 6 inch caliper, STD-1097.
(c) Compare the dimensions you measured with the permitted wear dimensions that follow:
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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Page 601
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D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Table 601/27-31-41-993-801
NAME OF THE
PARTS THAT
ARE IN
CONTACT
DIM.
DIAMETER DESIGN LIMITS
inches
(mm)
WEAR LIMITS
inches
(mm)
MINIMUM MAXIMUM
PERMITTED
MAXIMUM I.D./
MINIMUM O.D. OF
WORN PART
MAXIMUM
SERVICE DIAMETRIC
CLEARANCE
#1 FORWARD
HINGE HALF
I.D.
0.0930
(2.362)
0.0980
(2.489)
0.1040
(2.642) 0.0175
(0.445)
#1 FORWARD *[1]
HINGE PIN
O.D.
0.0880
(2.235)
0.0900
(2.286)
0.0865
(2.197)
#2 AFT HINGE
HALF
I.D.
0.1830
(4.648)
0.1880
(4.775)
0.1940
(4.928) 0.0175
(0.445)
#2 AFT HINGE *[1]
PIN
O.D.
0.1780
(4.521)
0.1800
(4.572)
0.1765
(4.483)
*[1] TOTAL PLAY IN THE JOINT = 0.0350 INCH (0.889 MILLIMETER)
(d) If the parts are not in the tolerance, replace or repair the parts, as required.
SUBTASK 27-31-41-020-008
(4) Install the elevator balance panel. To install it, do this task: Elevator Balance Panel -
Installation, TASK 27-31-41-400-801.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
 
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