A320飞机维护手册 AMM DOORS 舱门8(35)_航空信息_民用航空_通用航空

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121VU EIS/SLIDES/ARM AND WARN/FLT 121VU EIS/SLIDES/ARM AND WARN/GND 121VU EIS/SDAC1 AND 2/DOOR/DET/PAX 15WN 13WN 48WV P11P10P05
R Subtask 52-71-11-020-053-A
R D. Removal of the Lining Panel
R R R R R R R R R R R R R R R R R (1) Remove the lining panel: FOR 11WV1 221JW (Ref. TASK 25-23-45-000-005). FOR 11WV2 222JW (Ref. TASK 25-23-45-000-002). FOR 13WV1 831EZ, 831CZ (Ref. TASK 25-23-46-000-001). FOR 13WV2 841EZ, 841CZ (Ref. TASK 25-23-46-000-001). FOR 15WV1 261UW (Ref. TASK 25-23-45-000-003). FOR 15WV2 262UW (Ref. TASK 25-23-45-000-004). FOR 17WV1 832EZ 832CZ (Ref. TASK 25-23-46-000-002). FOR 17WV2 842EZ 842CZ (Ref. TASK 25-23-46-000-002).
R (2) Remove the insulation blanket.

4. Procedure
_________ Subtask 52-71-11-020-051
A. Removal of the Proximity Switches
(1)
FOR 11WV1, 11WV2, 15WV1, 15WV2
(Ref. Fig. 401/TASK 52-71-11-991-001)

(a)
Disconnect the electrical connector (1) from the proximity switch (2),

(b)
Put a blanking cap on the electrical connector.

(d)
Remove the nut (4) and the washer (5).

(e)
Remove the proximity switch (2) from the support (6).

(2)
FOR 13WV1, 13WV2
(Ref. Fig. 402/TASK 52-71-11-991-002)

(a)
Disconnect the electrical connector (11) from the proximity switch (12),

(b)
Put a blanking cap on the electrical connector.

(d)
Remove the nut (14) and the washer (15).

(e)
Remove the proximity switch (12) from the support (16).

(3)
FOR 17WV1, 17WV2
(Ref. Fig. 403/TASK 52-71-11-991-003)

(a)
Disconnect the electrical connector (21) from the proximity switch (22),

(b)
Put a blanking cap on the electrical connector.

(d)
Remove the nut (24) and the washer (25).

(e)
Remove the proximity switch (22) from the support (26).

1EFF : ALL 1 52-71-11Page 404 1 1 Feb 01/98 1 1 1CES 1

Proximity Switches (11WV1,11WV2,15WV1,15WV2)
Figure 401/TASK 52-71-11-991-001
1EFF : ALL 1 52-71-11 Page 405
1 1 Feb 01/98
1 1
1CES 1

Proximity Switches (13WV1,13WV2)
Figure 402/TASK 52-71-11-991-002
1EFF : ALL 1 52-71-11 Page 406
1 1 Feb 01/98
1 1
1CES 1

Proximity Switches (17WV1,17WV2)
Figure 403/TASK 52-71-11-991-003
1EFF : ALL 1 52-71-11 Page 407
1 1 Feb 01/98
1 1
1CES 1

TASK 52-71-11-400-001
Installation of the Proximity Switches of the Passenger/Crew Door (11WV1,11WV2,13WV1,13WV2,15WV1,15WV2,17WV1,17WV2)
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
FOR FIN 11WV1, 11WV2, 15WV1, 15WV2
Material No. 19-009 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.5MM DIA (Ref. 20-31-00)
FOR FIN 13WV1, 13WV2
Material No. 19-009 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.5MM DIA (Ref. 20-31-00)
FOR FIN 17WV1, 17WV2
Material No. 19-009 USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.5MM DIA (Ref. 20-31-00)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 52-10-00-410-001 Closing of the Passenger/Crew Door 52-10-00-860-001 Special Precautions before Work on the Passenger/Crew
Door 52-10-00-860-002 Special Precautions after Work on the Passenger/Crew
Door 52-71-00-710-001 Operational Test of the Door Warning System FOR FIN 11WV1, 11WV2, 15WV1, 15WV2
　
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