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时间:2011-03-30 10:22来源:蓝天飞行翻译 作者:航空
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(a)  
Pull plunger of Nylatch fasteners out to unlocked position (Section B-B).

(b)  
Pull cover from hinge mounting bracket.

 

(2)  
Remove hinge linkage pin from hinge linkage (Detail A).

(a)  
Press on both ends of pin at same time to release internal lock. Withdraw pin part way.

(b)  
Grasp pin behind exposed shoulder and press release plug on end. Support door and withdraw pin.

(c)  
Repeat steps for pin on opposite end of door and lower door to access position.

 


May 15/80 25-24-511 Page 201
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

Carry-All Compartment Installation  503 
25-24-511  Figure 201 (Sheet 1)  Oct 20/85 
Page 202 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 

EFFECTIVITY
DOORS WITH REMOVABLE PIN


504  Carry-All Compartment Installation 
Feb 15/80  Figure 201 (Sheet 2)  25-24-511 
Page 203 

BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

EFFECTIVITY
DOOR WITH QUICK RELEASE CAM

Carry-All Compartment Installation  504 
25-24-511  Figure 201 (Sheet 3)  Feb 15/80 
Page 204 

BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

504  Carry-All Compartment Installation 
Feb 15/80  Figure 201 (Sheet 4)  25-24-511 
Page 205 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 


Carry-All Compartment Installation  504 
25-24-511  Figure 201 (Sheet 5)  Feb 20/84 
Page 206 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 


504  Carry-All Compartment Installation 
Feb 15/80  Figure 201 (Sheet 6)  25-24-511 
Page 207 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 


EFFECTIVITY
DOOR WITH
REMOVABLE PIN


Carry-All Compartment Installation  504 
25-24-511  Figure 201 (Sheet 7)  Feb 15/80 
Page 208 

BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
EFFECTIVITY
DOORS WITH
REMOVABLE PIN

 

504  Carry-All Compartment Installation 
Feb 15/80  Figure 201 (Sheet 8)  25-24-511 
Page 209 

BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

EFFECTIVITY
DOORS WITH QUICK-RELEASE CAM

Carry-All Compartment Installation  504 
25-24-511  Figure 201 (Sheet 9)  Feb 15/80 
Page 210 

BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
EFFECTIVITY
DOORS WITH QUICK-RELEASE CAM


504  Carry-All Compartment Installation 
Feb 15/80  Figure 201 (Sheet 10)  25-24-511 
Page 211 

BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

D.  Lower Carry-All Compartment door for access (Doors With Quick-Release Cam)
(1)  
Support door in partly open position and insert small rod in hole in bottom surface of articulated hinge frame.

(2)  
Press upward until quick-release cam clicks into unlatched position. Accomplish for both ends of door (Fig. 201, Detail K).

(3)  
Pull door downward to lowered position.


E.  Remove temperature sensor wire bundle (compartments with temperature sensors) (Detail D).
(1)  
Check that RIGHT A/C PACK switch is off.

(2)  
Open RIGHT AUTO TEMP CONT circuit breaker on circuit breaker panel P6.

(3)  
Remove wire bundle ties and clamps, all accessible locations.

NOTE:  Identify location of ties and clamps on wire bundle to assist in re-assembly.

(4)  
Disconnect electric wire bundle at connectors (3 places).

(5)  
If all clamps have been removed, remove wire bundle from compartment and stow for protection.


F.  Remove curved ceiling panels above compartments if required for additional access (Ref 25-21-341).
G.  Remove end closure (end compartments only) (Ref 25-24-512).
3.  Remove Compartment Door and Articulated Hinge (Doors With Removable Pin)
NOTE:  The door and articulated hinge assemblies may be removed with the compartment installed or removed.
A.  Remove door (Section C-C)
 
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