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时间:2011-04-20 07:49来源:蓝天飞行翻译 作者:航空
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 21-31-04
 ALL  ú ú 01 Page 401 ú Jan 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

4. DC MOTOR 
ELECTRICAL 
CONNECTOR 
3. ACTUATOR 
5. POTENTIOMETER 
2. AC MOTORS  ELECTRICAL 
CONNECTOR 
1. AC MOTORS 
ELECTRICAL  6. DC MOTOR AND 
CABIN PRESSURE  CONNECTORS  POTENTIOMETER 
OUTFLOW VALVE 
ACTUATOR  A  7. ACTUATOR 
SEE  A  SUPPORT 
FRAME 
8. ACTUATOR BOLT 
A  (2 LOCATIONS) 9. WASHER 
10. BOLT 
(SEE A-A) 

INBD FWD
CABIN PRESSURE OUTFLOW VALVE ACTUATOR
2. AC MOTORS
A
15. ACTUATOR ARM
2` (REF)
8.
 ACTUATOR BOLT

9.
 WASHER (2 LOCATIONS)


17. CONNECTING ROD
7. ACTUATOR SUPPORT
FRAME16. ACTUATOR 10. BOLT
DRIVE SHAFT
12.
 WASHER

13.
 NUT

14.
 PIN


THE ANGLE IS MEASURED BETWEEN THE PLANE
THROUGH THE ACTUATOR BOLT CENTERLINES

A-A
AND THE DOWN SLOPE OF THE CENTERLINE
OF THE ACTUATOR ARM (VALVE FULLY CLOSED)

Cabin Pressure Outflow Valve Actuator Installation
Figure 401

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 21-31-04
 ALL  ú ú 01 Page 402 ú Sep 20/94
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A

757 MAINTENANCE MANUAL
 S 864-005
 WARNING: IF YOU USE THE ACCESS THROUGH THE CABIN PRESSURE OUTFLOW VALVE,
_______ MAKE SURE THE ELECTRICAL POWER IS OFF, THE CIRCUIT BREAKERS ARE OPEN, AND THE DO-NOT-CLOSE TAGS ARE ATTACHED. IF ELECTRICAL POWER IS SUPPLIED TO THE VALVE WHEN IT IS IN THE FULLY OPEN POSITION, THE VALVE WILL MOVE TO THE NOT FULLY OPEN POSITION. THE MOVEMENT OF THE VALVE CAN CAUSE INJURY TO PERSONS.
 (3)  
Remove the electrical power (AMM 24-22-00/201).

 S 864-004

 (4)  
Open these circuit breakers on the overhead circuit breaker panel, P11, and attach DO-NOT-CLOSE tags:

 (a)  
11B14, CABIN ALTITUDE CONTROL MANUAL

 (b)  
11B15, CABIN ALTITUDE CONTROL SELECT

 (c)  
11N15, CABIN ALTITUDE CONTROL AUTO 1

 (d)  
11N24, CABIN ALTITUDE CONTROL AUTO 2


 S 034-005
 (5)  
Disconnect the electrical connectors (1, 4) on the manual DC and auto AC motors (6, 2).

 (a)  
Put a tag on the AC motor electrical connectors (1) to identify them for installation.


 S 034-006
 (6)  
Disconnect the electrical connector (5) from the potentiometer (6).

 S 034-007

 (7)
Remove the bolt (10), washer (12), nut (13), and pin (14) that connect the actuator arm (15) to the connecting rod (17).

 (8)  
Remove the actuator bolts (8) and the actuator (3).


 S 024-008
 TASK 21-31-04-404-009
 3. Install the Cabin Pressure Outflow Valve Actuator (Fig. 401)
_________________________________________________
 A. Parts
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 21-31-04
 ALL  ú ú 02 Page 403 ú Jan 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL

 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT |FIG | ITEM | ................................................................................ | 401 | 3 | Actuator | 21-31-03 | 01 | 40 | | | 8 | Actuator Bolt | | | 45 | | | 9 | Washer | | | 55 | | | 10 | Bolt | | | 35 | | | 12 | Washer | | | 37 | | | 13 | Nut | | | 38 | | | 14 | Pin | | | 33 | 2......…........…...................................…...........….....…........1
 B. References
 (1)  
AMM 06-46-00/201, Entry, Service and Cargo Doors Access Doors and Panels


 
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