Adjustment of the Ground Service Panel Door of the Blue Hydraulic System
Figure 402/TASK 52-42-25-991-002
R 1EFF : 001-049, 051-061, 101-103, 201-203, 1 52-42-25Page 411 1 1 May 01/05 1 1 1CES 1
Adjustment of the Ground Service Panel Door of the Blue Hydraulic System
Figure 402A/TASK 52-42-25-991-002-A
R 1EFF : 062-099, 104-149, 151-199, 204-299, 1 52-42-25Page 412 1401-499, 1Aug 01/05 1 1 1CES 1
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(3)
If it is necessary to adjust the access door (2):
(a)
Remove the access panel 197BB as necessary (Ref. TASK 53-35-13-000-002).
(b)
Loosen the screws (31).
(c)
Adjust the latch hooks (30) until you get the correct values.
(d)
Tighten the screws (31).
(4)
Make sure that it is possible to open and close the access door (2) correctly.
(5)
Make sure that the latch assemblies are correctly locked and that the access door (2) makes a continues surface with the skin of the aircraft.
**ON A/C 301-399,
Subtask 52-42-25-820-050-A
B. Adjustment of the Ground Service Panel Door of the Blue Hydraulic System
(1)
Carefully close and lock the access door (2).
(2)
Make sure that the values of the permitted contour offset and the gap between the access door (2) and the panel 197KB are in the limits. (Ref. Fig. 402B/TASK 52-42-25-991-002-B)
(3)
If it is necessary to adjust the access door (2):
(a)
Remove the access panel 197KB as necessary (Ref. TASK 53-35-13-000-002).
(b)
Loosen the screws (31).
(c)
Adjust the latch hooks (30) until you get the correct values.
(d)
Tighten the screws (31).
(4)
Make sure that it is possible to open and close the access door (2) correctly.
1EFF : ALL 1 52-42-25Page 413 1 1 Aug 01/05 1 1 1CES 1R Adjustment of the Ground Service Panel Door of the Blue Hydraulic System R Figure 402B/TASK 52-42-25-991-002-B
1EFF : 301-399, 1 52-42-25Page 414 1 1 May 01/04 1 1 1CES 1
(5) Make sure that the latch assemblies are correctly locked and that the access door (2) makes a continues surface with the skin of the aircraft.
**ON A/C ALL
5. Close-up
________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 52-42-25-410-050
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
If removed, install the access panel 197BB (Ref. TASK 53-35-13-400-002).
(3) Remove the access platform(s).
**ON A/C 301-399,
Subtask 52-42-25-410-050-A
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
If removed, install the access panel 197KB (Ref. TASK 53-35-13-400-002).
(3)
Remove the access platform(s).
1EFF : ALL 1 52-42-25Page 415 1 1 Aug 01/05 1 1 1CES 1
FIXED INTERIOR - DESCRIPTION AND OPERATION
__________________________________________
1. General
_______
Data to the fixed interior doors is given in the Chapter 52-51-00, P. Block
001.
1EFF : ALL 1 52-50-00Page 1 1 1 Feb 01/98 1 1 1CES 1 PASSENGER COMPARTMENT FIXED INTERIOR DOORS - DESCRIPTION AND OPERATION
______________________________________________________________________
1.
General
_______ The cockpit door is installed between FR13 and FR14 in zone 220 and divides the cockpit from the passenger cabin. The cockpit door also has a Cockpit Door Lock System (CDLS) to open it electrically.
2.
Component Location
__________________ R (Ref. Fig. 001)
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-299, 301-302,
R (Ref. Fig. 002)
R **ON A/C 106-149, 303-399, 401-499,
R (Ref. Fig. 002A)
R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-231, 301-302,
R Post SB 25-1444 For A/C 001-049,051-099,101-105,151-199,201-231,301-302,
R (Ref. Fig. 002B)
R **ON A/C ALL
R (Ref. Fig. 003)
-------------------------------------------------------------------------------FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I ATA I I I I DOOR I REF. -------------------------------------------------------------------------------
R 22MQ INDICATION LIGHT 119VU 210 831/841 52-51-00 23MQ BUZZER 211HC 210 831/841 52-51-14 24MQ CONTROL UNIT 20VU 210 831/841 52-51-13 25MQ KEYPAD 221 831/841 52-51-15 26MQ TOGGLE SWITCH UNLOCK/NORM/LOCK 119VU 210 831/841 52-51-00 30MQ TOP ELECTRICAL RELEASE STRIKE 221 831/841 52-51-12 31MQ MID ELECTRICAL RELEASE STRIKE 221 831/841 52-51-12 32MQ BOT ELECTRICAL RELEASE STRIKE 221 831/841 52-51-12
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM DOORS 艙門7(21)
