25-23-45Page 441
May 01/03 R CES
(3)
Remove the lining 262TW:
(a)
Remove the screws (16), the washers (17) and the latch hook (18).
(b)
Remove the handgrip: CAUTION : DO NOT USE TOO MUCH FORCE WHEN YOU REMOVE THE COVER AS
_______
(c)
Remove the cap (3), the screws (4) and (1) and the washers (2).
(d)
Carefully tilt the lining, remove the nuts (22) and disengage the socket (23) .
(e)
Remove the lining 262TW.
(4)
Remove the lining 262WW:
(a)
Remove the cap (3), the screws (4) and (1) and the washers (2).
(b)
Remove the handgrip: CAUTION : DO NOT USE TOO MUCH FORCE WHEN YOU REMOVE THE COVER AS
THIS CAN CAUSE DAMAGE TO THE RETAINER.
1_ Put a SCREWDRIVER - SMALL with a flat blade between the
handgrip cover (9) and the handgrip (14).
2_ Carefully push the the lugs (10) of the handgrip cover (9) in
the direction of the arrows and remove the handgrip cover (9).
3_ Remove the screws (11) and (12), the plates (13), the spacer
(15) (if installed) and the handgrip (14).
_______ THIS CAN CAUSE DAMAGE TO THE RETAINER.
1 Put a SCREWDRIVER - SMALL with a flat blade between the
_ handgrip cover (9) and the handgrip (14).
2 Carefully push the the lugs (10) of the handgrip cover (9) in
_ the direction of the arrows and remove the handgrip cover (9).
3 Remove the screws (11) and (12), the plates (13), the spacer
_ (15) (if installed) and the handgrip (14).
(c) Remove the lining 262WW.
EFF : ALL
25-23-45Page 442
May 01/03
R
CES TASK 25-23-45-400-005
Installation of the Door Frame Linings at the Right AFT Passenger/Crew Door
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
11-00-00-400-002 Installation of the Decals 20-21-11-911-001 Tightening Torques for Standard Threaded Fasteners 24-42-00-861-001 Energize the Ground Service Network from the External
Power 24-42-00-862-001 De-energize the Ground Service Network Supplied from
the External Power
33-51-11-400-001 Installation of the Cabin Emergency Light
33-51-13-400-001 Installation of the Cabin Wall-Mounted
Emergency-Exit-Markers
33-51-16-400-001 Installation of the Emergency Exit Sign
R 35-23-00-710-001 Operational Check of Manual Mask Release 52-10-00-410-001 Closing of the Passenger/Crew Door AMM 11-32-25 P.Block 001 INTERIOR PLACARDS (SEE ALSO 11-42-25) 25-23-45-991-005-A Fig. 404
EFF : ALL
25-23-45Page 443
3. Job Set-up
__________
Subtask 25-23-45-860-050
A. Aircraft Maintenance Configuration
(1) Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001) Clean the component interface and/or the adjacent area. Make sure that the parts retained from the removed component are clean and in the correct condition. Make sure that the parts retained from the removed component are clean and in the correct condition.
4. Procedure
_________
Subtask 25-23-45-420-061-A
A. Installation of the door frame linings 262WW, 262TW, 262UW, 262VW
(Ref. Fig. 404/TASK 25-23-45-991-005-A) R
R (1) Unless specified, TORQUE al nuts, bolts and screws (Ref. TASK 20-21-11-911-001).
R (2) Install the lining 262TW:
(a)
Put the the lining 261TW in position.
(b)
Install the screws (1), (4) and the washers (2), but do not tighten the screws (1) and (4).
(c)
Install the handgrip: 1 Put the spacer (15) (if installed), the handgrip (14), the
_ plates (13) and the screws (11) and (12) in position. TORQUE the screws (11) and (12) to 0.8 m.daN (70.79 lbf.in).
(d)
Tighten the screws (1) and (4) and install the cap(s) (3).
(e)
Install the handgrip cover (9). Make sure that the lugs (10) of the handgrip cover engage correctly. Press the handgrip cover into position until you hear a click.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM EQUIPMENT/FURNISHINGS 设备2(29)
