____
aircraft structure.
NOTE : If adjustment of the fastener (5) is necessary, loosen the
____ screws (6) or (8) and move the adjustment plate (7) to its correct position and tighten the screws (6) or (8).
R EFF : 001-049, 051-099, 101-149, 151-199, 25-23-47Page 405 201-299, 401-499, Config-1 Aug 01/05
CES
Cover Flap
Figure 402/TASK 25-23-47-991-017
CES Subtask 25-23-47-720-050
D. Test
(Ref. Fig. 402/TASK 25-23-47-991-017)
(1) Test of the opening force of the cover flap (1) NOTE : The procedure of the test is the same for all emergency exit
____
hatches.
(a)
Attach a spring scale (2) to the grip of the cover flap (1)
(b)
Pull the spring scale (2) inboard and at a right angle to the cover flap (1).
NOTE : Make sure that the force which is necessary to open the
____ cover flap (1) is 4.0 +0.5 -0.5 daN (8.9923 +1.1240 -1.1240 lbf).
NOTE : If adjustment is necessary move the arms of the fastener
____
(5) together. NOTE : Make sure that the proximity sensor of the door warning
____ system has the correct target value (Ref. TASK 52-71-13-400-001)
5. Close-up
________ Subtask 25-23-47-410-065
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Close the passenger/crew door (Ref. TASK 52-10-00-410-001)
(3) Remove the access platform(s). Subtask 25-23-47-862-061
B. De-energize the ground service network (Ref. TASK 24-42-00-862-001)
R EFF : 001-049, 051-099, 101-149, 151-199, 25-23-47Page 407 201-299, 401-499, Config-1 Aug 01/05
CES TASK 25-23-47-000-002
Removal of the Upper Sidewall Panel Assy 241LW, (242LW), 241CW, (242CW) and 241FW, (242FW)
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific warning notices
B. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
Power
25-21-41-000-001 Removal of the Passenger Seats
33-51-13-000-001 Removal of the Cabin Wall-Mounted
Emergency-Exit-Markers
33-51-16-000-001 Removal of the Emergency Exit Sign
52-21-11-000-001 Removal of the Emergency Exit Hatch
**ON A/C 001-049, 051-099, 101-149, 201-299,
25-23-47-991-002 Fig. 403 R **ON A/C 151-199, 401-499,
25-23-47-991-002-A Fig. 403A
R EFF : 001-049, 051-099, 101-149, 151-199, 25-23-47Page 408 201-299, 401-499, Config-1 Aug 01/05
CES
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
3. Job Set-up
__________
Subtask 25-23-47-861-069
A. Energize the ground service network (Ref. TASK 24-42-00-861-001).
Subtask 25-23-47-865-051
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU LIGHTING/EMER LT/CABIN 2WL H06 49VU LIGHTING/EMER LT/CABIN 1WL H05 122VU LIGHTING/CABIN/EMER/LT 3WL V07
4. Procedure
_________
Subtask 25-23-47-010-050
A. Get Access
(1)
Remove the related emergency exit hatch (Ref. TASK 52-21-11-000-001).
(2)
Make sure that the switch 4WL on the panel 25VU is in the OFF position.
(3)
Make sure that the switch LIGHT EMER on the panel 120RH is in the OFF position.
(4)
Put the warning notices on the panels 25VU and 120RH to tell persons not to operate the switches 4WL and LIGHT EMER.
(5)
Remove the related passenger seat, if necessary (Ref. TASK 25-21-41-000-001)
(6)
Remove the wall-mounted emergency exit-markers (Ref. TASK 33-51-13-000-001).
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 EQUIPMENT/FURNISHINGS 設(shè)備2(37)
