R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 56-12-11-914-052
A. Preparation for Installation
(Ref. Fig. 421/TASK 56-12-11-991-020)
(1)
Lightly rub the retainer area (41) which contains the seal (40) with a scotch brite.
(2)
Clean the surfaces and remove the grease with CLEANING AGENTS (Material No. 11-003) and a MISCELLANEOUS (Material No. 19-003).
(3)
Lightly rub the seal surfaces which touch the retainer (41).
1EFF : ALL 1 56-12-11Page A411 1 1 Aug 01/05 1 1 1CES 1
(4)
Apply BONDING AND ADHESIVE COMPOUNDS (Material No. 08-018) on the surfaces of the seal (40).
(5)
Let BONDING AND ADHESIVE COMPOUNDS (Material No. 08-018) become almost dry.
Subtask 56-12-11-420-055
B. Installation of the Seal
(Ref. Fig. 421/TASK 56-12-11-991-020)
(1)
Put the seal (40) in position.
(2)
Put a strong force on the seal (40) for 30 minutes.
(3)
Make sure that there is no remaining adhesive compound on the retainer.
(4)
Make sure that the external lip of the seal (40) moves freely around the retainer (41).
Subtask 56-12-11-210-062
C. Sealing Check
(1)
Close the sliding window
(2)
Apply water to the periphery of the sliding window from the outside of the aircraft
(3)
Wait ten minutes and make sure that there is no water leakage at level of the window frame.
(4)
If water goes into the cockpit, make sure that the adjustments are correct and that the seal is in the correct condition.
(5)
Dry if necessary.
R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 56-12-11Page A412 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1 1EFF : 051-099, 1 56-12-11Page A413 1 1 May 01/05 1 1 1CES 1
R **ON A/C 051-099,
R Subtask 56-12-11-914-052-A
R A. Preparation for Installation
R (Ref. Fig. 421A/TASK 56-12-11-991-020-A)
R (1) Lightly rub the retainer area (41) which contains the seal (40) with
R a scotch brite.
R (2) Clean the surfaces and remove the grease with CLEANING AGENTS
R (Material No. 11-003) and a MISCELLANEOUS (Material No. 19-003).
R (3) Lightly rub the seal surfaces which touch the retainer (41).
R (4) Apply on the surface of the seal (40):
R (a) BONDING AND ADHESIVE COMPOUNDS (Material No. 08-018) for the seal
R P/N D53111246200.
R (b) BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) for the seal
R P/N D53111248200.
R (5) Let the adhesive compound become almost dry.
R Subtask 56-12-11-420-055-A
R B. Installation of the Seal
R (Ref. Fig. 421A/TASK 56-12-11-991-020-A)
R (1) Put the seal (40) in position.
R (2) Put a strong force on the seal (40) for 30 minutes.
R (3) Make sure that there is no remaining adhesive compound on the
R retainer.
R (4) Make sure that the external lip of the seal (40) moves freely around
R the retainer (41).
Subtask 56-12-11-210-062-A
C. Sealing Check
(1)
Close the sliding window
(2)
Apply water to the periphery of the sliding window from the outside of the aircraft
(3)
Wait ten minutes and make sure that there is no water leakage at level of the window frame.
(4)
If water goes into the cockpit, make sure that the adjustments are correct and that the seal is in the correct condition.
(5) Dry if necessary.
**ON A/C ALL
5. Close-up
________
Subtask 56-12-11-865-078
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1DG1, 4DG1, 5DG1, 1DG2, 4DG2, 5DG2, 5SQ1, 5SQ2. 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 WINDOWS 風(fēng)擋 窗戶(75)
