(15) (if installed) and the handgrip (14).
(b) Remove the screws (1) and the washers (2) and remove the lining 221RW.
EFF : ALL
25-23-45Page 407
Feb 01/03
R
CES TASK 25-23-45-400-006
Installation of the Door Frame Linings at the Left FWD 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
-------------------------------------------------------------------------------
No specific 1 WARNING NOTICE
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 33-51-00-710-008 Operational Test of the Emergency Lighting in the
Cabin by 'EMER EXIT LT' Switch
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) 25-23-45-991-006-A Fig. 401
EFF : ALL
25-23-45Page 408
3. Job Set-up
__________ Subtask 25-23-45-860-053
A. Aircraft Maintenance Configuration
(1)
Make sure that the ground service network is energized
(Ref. TASK 24-42-00-861-001)
(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)
Make sure that the WARNING NOTICE are in position on the panels 25VU and 120 RH to tell persons not to operate the switches 4WL and LIGHT EMER.
(5)
Clean the component interface and/or the adjacent area.
(6)
Do an inspection of the component interface and/or the adjacent area.
(7)
Make sure that the parts retained from the removed component are clean and in the correct condition.
Subtask 25-23-45-865-059
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------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
EFF : ALL
25-23-45Page 409
May 01/05
R
CES EFF : ALL
4. Procedure_________
Subtask 25-23-45-420-056-A
R A. Installation of the door frame linings 221AW, 221BW, 221CW, 221EW, 221FW, 221RW,221SW, 221VW, (Ref. Fig. 401/TASK 25-23-45-991-006-A)
R (1) Unless specified, TORQUE al nuts, bolts and screws (Ref. TASK 20-21-11-911-001).
R (2) Install the lining 221RW:
(a) Put the lining 221RW in position and install the screws (1) and the washers (2), but do not tighten the screws (1).
(b) 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).
(c) Tighten the screws (1).
(d) 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.
R (3) Install the lining 221CW:
(a) Put the lining 221CW in position and install the screws (29) and the washers (28).
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM EQUIPMENT/FURNISHINGS 設備2(21)
