25-22-41Page 402
**ON A/C ALL
4. Procedure
_________
Subtask 25-22-41-020-051
A. Remove the Single-Seat Assembly
(Ref. Fig. 401/TASK 25-22-41-991-001)
(1)
Remove the seat upholstery (6).
(2)
Open the door (3).
(3)
Remove all the equipment from the stowage compartment of the seat.
(4)
If applicable, disconnect the electrical connector (7).
(5)
If necessary, put blanking caps on the disconnected electrical connectors (7) and (8).
(6)
Remove the bolts (5) and the washers (4).
(7) Remove the seat assembly (2) and the washers (1). R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
Subtask 25-22-41-020-052
B. Remove the Double-Seat Assembly
(Ref. Fig. 402/TASK 25-22-41-991-002)
(1)
Remove the seat upholstery (6).
(2)
Open the door (5).
(3)
Remove all the equipment from the stowage compartment of the seat.
(4)
Remove the screws (7) and (8).
(5)
Remove the bolts (3) and the washers (2).
(6)
Remove the seat assembly (4) and the washers (1).
EFF : ALL
25-22-41Page 403
Wall-Mounted Cabin Attendant-Seat - Single Folding Figure 401/TASK 25-22-41-991-001
R EFF : CES ALL 25-22-41 Page 404 May 01/05
Wall-Mounted Cabin Attendant-Seat - Double Bench Figure 402/TASK 25-22-41-991-002
R EFF : 001-049, 051-099, 101-105, 151-199, 201-210, 25-22-41 Page 405 May 01/05
CES
R **ON A/C ALL
TASK 25-22-41-000-002
Removal of the Restraint System
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001 Energize the Ground Service Network from the External
Power
25-22-41-991-003 Fig. 403
25-22-41-991-004 Fig. 404
3. Job Set-up
__________
Subtask 25-22-41-861-051
A. Aircraft Maintenance Configuration
(1) Energize the ground service network
(Ref. TASK 24-42-00-861-001).
4. Procedure
_________
Subtask 25-22-41-020-053
A. Removal of the Restraint System
(Ref. Fig. 403/TASK 25-22-41-991-003)
(1)
Pull the headrest (4) up and remove it.
(2)
Open the seat pan (2) and put some type of weight on it to hold it in the open position.
(3)
Remove the backrest cushions (3). NOTE : The burrstrips attach the cushions to the seat structure.
____
EFF : ALL
25-22-41Page 406
R R Restraint System with the Inertia Reel(s) Figure 403/TASK 25-22-41-991-003
EFF : ALL 25-22-41 Page 407 Nov 01/98
CES
R (4) Remove the bolts (10), the nuts 12, the washers (11) and release the
R restraint system assy (1).
R (5) Remove the screws (8), the washers (9) and the inertia reel(s) (7).
R (6) Remove the screws (6), the strap guides (5) and restraint system assy
R (1).
R Subtask 25-22-41-020-054
R B. Removal of the Restraint System
R (Ref. Fig. 404/TASK 25-22-41-991-004)
R (1) Open the seat pan (2) and put some type of weight on it to hold it in
R the open position.
R (2) Remove the backrest cushion (3).
R NOTE : The burrstrips attach the cushion to the seat structure.____
R (3) Remove the bolts (8), the nuts (9) and the washers (7).
中國航空網(wǎng) m.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1(151)
