曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
12.662 mm 12.687 mm 12.652 mm
#3 BUSHING I.D.
0.6245 in 0.6250 in 0.6275 in
15.862 mm 15.875 mm 15.938 mm 0.0033 in
#3 BOLT
ASSEMBLY
O.D.
0.6237 in 0.6242 in 0.6212 in 0.084 mm
15.842 mm 15.855 mm 15.778 mm
#4 BUSHING I.D.
0.6245 in 0.6250 in 0.6265 in
15.862 mm 15.875 mm 15.913 mm 0.0033 in
#4 BOLT
ASSEMBLY
O.D.
0.6237 in 0.6242 in 0.6212 in 0.084 mm
15.842 mm 15.855 mm 15.778 mm
#5 BEARING I.D.
0.6245 in 0.6250 in 0.6275 in
15.862 mm 15.875 mm 15.938 mm 0.0033 in
#5 BOLT
ASSEMBLY
O.D.
0.6237 in 0.6242 in 0.6212 in 0.084 mm
15.842 mm 15.855 mm 15.778 mm
#6 SUPPORT LINK I.D.
0.7500 in 0.7507 in 0.7522 in
19.050 mm 19.068 mm 19.106 mm 0.0022 in
#6 BUSHING O.D.
0.7495 in 0.7500 in 0.7491 in 0.056 mm
19.037 mm 19.050 mm 19.027 mm
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-14
Page 603
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
(Continued)
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
#7 BUSHING I.D.
0.6245 in 0.6250 in 0.6265 in
15.862 mm 15.875 mm 15.913 mm 0.0023 in
#7 BOLT O.D.
0.6237 in 0.6242 in 0.6212 in 0.058 mm
15.842 mm 15.855 mm 15.778 mm
#8 BEARING I.D.
0.3122 in 0.3125 in 0.3155 in
7.930 mm 7.937 mm 8.014 mm 0.0035 in
#8 BOLT O.D.
0.3110 in 0.3120 in 0.3106 in 0.089 mm
7.899 mm 7.925 mm 7.889 mm
#9 INPUT ROD I.D.
0.3120 in 0.3130 in 0.3160 in
7.925 mm 7.950 mm 8.026 mm 0.0040 in
#9 BOLT O.D.
0.3110 in 0.3120 in 0.3106 in 0.102 mm
7.899 mm 7.925 mm 7.889 mm
SUBTASK 27-31-14-020-008
(4) Install the elevator PCU. To install it, do this task: Elevator Power Control Unit Installation,
TASK 27-31-14-400-801.
------------------------- END OF TASK ---------------------------
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-14
Page 604
Jun 10/2005
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Power Control Unit Wear Limits
Figure 601 (Sheet 1 of 3)/27-31-14-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-14
Page 605
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Power Control Unit Wear Limits
Figure 601 (Sheet 2 of 3)/27-31-14-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-14
Page 606
Oct 10/2003
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
Elevator Power Control Unit Wear Limits
Figure 601 (Sheet 3 of 3)/27-31-14-990-804
737-600/700/800/900
AIRCRAFT MAINTENANCE MANUAL
EFFECTIVITY
GUN ALL 27-31-14
Page 607
Jun 10/2006
D633A101-GUN
BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details
ELEVATOR PITOT-STATIC SYSTEM - MAINTENANCE PRACTICES
1. General
A. This procedure has these tasks:
(1) Elevator Pitot-Static System Flushing
(2) Elevator Pitot-Static System Drainage Inspection
(3) Elevator Pitot Probe Inspection
(4) Elevator Pitot System Leak Test.
(5) Elevator Pitot System Pressurization
TASK 27-31-17-170-801
2. Elevator Pitot-Static System Flushing
(Figure 201)
A. Tools/Equipment
Reference Description
STD-1280 Source - Air, Regulated, Dry Filtered, 0-30 PSIG
B. Location Zones
Zone Area
311 Area Aft of Pressure Bulkhead - Left
312 Area Aft of Pressure Bulkhead - Right
323 Vertical Fin - Front Spar To Rear Spar
C. Access Panels
Number Name/Location
311BL Stabilizer Trim Access Door
323FL Vertical Fin, Access
D. Prepare for the Flushing
SUBTASK 27-31-17-010-001
(1) Remove this access panel:
Number Name/Location
323FL Vertical Fin, Access
SUBTASK 27-31-17-010-002
(2) Open this access panel:
Number Name/Location
311BL Stabilizer Trim Access Door
E. Elevator Pitot-Static System Flushing
SUBTASK 27-31-17-170-001
(1) Flush the pitot system:
(a) Disconnect the pitot lines from the pitot probes.
(b) Disconnect the pitot lines from the elevator feel computer.
(c) Remove the restrictor valves from the pitot lines.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:
737-600-700-800-900 AIRCRAFT MAINTENANCE MANUAL飞机维护手册3(33)