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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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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
317 Tail Cone Compartment - Left
318 Tail Cone Compartment - Right
E. Procedure
SUBTASK 27-31-91-020-002
(1) Remove the elevator neutral shift mechanism. To remove it, do this task: Elevator Neutral Shift
Mechanism Removal, TASK 27-31-91-000-801.
SUBTASK 27-31-91-020-003
(2) Use these tools to check for wear on the parts of the elevator neutral shift mechanism
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 27-31-91-020-004
(3) Examine the parts of the elevator neutral shift mechanism 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
GUN ALL 27-31-91
Page 601
Oct 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(d) If the parts are not in the tolerance, replace or repair the part as required.
Table 601/27-31-91-993-801
NAME OF THE
PARTS THAT ARE
IN CONTACT
DIM.
DIAMETER DESIGN LIMITS WEAR LIMITS
MINIMUM
inches/mm
MAXIMUM
inches/mm
PERMITTED
MAXIMUM I.D./
MINIMUM O.D. OF
WORN PART
MAXIMUM
SERVICE
DIAMETRIC
CLEARANCE
#1 OUTER
BEARING
HOUSING
I.D.
1.9375 in
49.212 mm
1.9385 in
49.238 mm
1.9415 in
49.314 mm
0.004 in
#1 BEARING O.D.
1.9365 in
49.187 mm
1.9375 in
49.212 mm
1.9360 in
49.174 mm
0.102 mm
#2 BEARING I.D.
0.9995 in
25.387 mm
1.0000 in
25.400 mm
1.0025 in
25.463 mm 0.0035 in
#2 ELEVATOR
NEUTRAL SHIFT
MECHANISM
O.D.
0.9985 in
25.362 mm
0.9990 in
25.375 mm
0.9965 in
25.311 mm
0.089 mm
SUBTASK 27-31-91-020-005
(4) Install the elevator neutral shift mechanism. To install it, do this task: Elevator Neutral Shift
Mechanism Installation, TASK 27-31-91-400-801.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
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D633A101-GUN
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Elevator Neutral Shift Mechanism Wear Limits
Figure 601 (Sheet 1 of 3)/27-31-91-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-91
Page 603
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Neutral Shift Mechanism Wear Limits
Figure 601 (Sheet 2 of 3)/27-31-91-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-91
Page 604
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Neutral Shift Mechanism Wear Limits
Figure 601 (Sheet 3 of 3)/27-31-91-990-803
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-91
Page 605
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
FEEL SYSTEM PITOT PROBE - REMOVAL/INSTALLATION
1. General
A. This procedure has these tasks:
(1) A removal of a feel system pitot probe
(2) An installation of a feel system pitot probe.
B. The feel system pitot probe is referred to as the "pitot probe" in this procedure.
C. A pitot probe is installed on each side of the vertical fin. This procedure is applicable for the left and
right pitot probes.
TASK 27-31-94-000-801
2. Feel System Pitot Probe Removal
(Figure 401)
A. Tools/Equipment
NOTE: When more than one tool part number is listed under the same "Reference" number, the
tools shown are alternates to each other within the same airplane series. Tool part numbers
that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.
Reference Description
COM-2481 Tool - Sealant Removal, BAC5000, PSD 6-184 Approved
(Part #: 1-6390-A, Supplier: 63318, A/P Effectivity: 737-ALL)
 
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