(3)
Make sure that the cargo door is opened (Ref. TASK 52-30-00-860-001) and safetied with the SUPPORT STRUT - CARGO DOORS (98D52307524000).
(4)
Make sure that the access platform in position below the opened cargo door.
1EFF : ALL 1 52-31-18Page 411 1 1 May 01/05 1 1 1CES 1
4. Procedure
_________ R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 401/TASK 52-31-18-991-001-A)
**ON A/C 051-052,
(Ref. Fig. 401A/TASK 52-31-18-991-001-B) R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
(Ref. Fig. 402/TASK 52-31-18-991-002-A)
**ON A/C 051-052,
(Ref. Fig. 402A/TASK 52-31-18-991-002)
Subtask 52-31-18-560-050
A. Preparation of Replacement Component WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
WARNING : DO NOT GET THE FLUID ON YOUR SKIN OR IN YOUR EYES. IF YOU DO:
_______
-FLUSH IT AWAY WITH CLEAN WATER
-GET MEDICAL AID.
(1)
Examine the new door seal to find the ink mark "LOWER DOOR". NOTE : The door seal with the ink mark "LOWER DOOR" does not have
____ inflation holes in the marked area. (Ref. Fig. 401A/TASK 52-31-18-991-001-B)
(2)
If you find this ink mark no further action is required.
1EFF : ALL 1 52-31-18Page 412 1 1 Aug 01/05 1 1 1CES 1 (3) If you do not find this ink mark, continue as follows:
(a)
Clean the lower area of the new door seal on the inner and outer side with CLEANING AGENTS (Material No. 11-003A) and allow to dry.
(b)
Fill the inflation holes located in the lower area of the new door seal with BONDING AND ADHESIVE COMPOUNDS (Material No. 08-026) or BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004).
NOTE : Apply sufficent material so that a small bead forms on the
____ inner side of the door seal.
(c) Use a plastic spatula and make the outer surface of the door seal smooth
NOTE : Allow it to dry for 4 hours at room temperature.
____ R **ON A/C 001-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 52-31-18-420-050-A
B. Installlation of the Door Seal and the associated Components (Ref. Fig. 401/TASK 52-31-18-991-001-A, 402/TASK 52-31-18-991-002-A)
(1) Install the door seal (1) as follows:
(a)
Clean the component interface and/or the adjacent area.
(b)
Do an inspection of the component interface and/or the adjacent area.
(c)
Make sure that the ink mark "LOWER DOOR" is in the correct position.
(d)
Push the door seal (1) correctly into the retainer (2).
(e)
Make sure that the inflation holes of the door seal are in their correct position on the inner side of the cargo door.
NOTE : If the door seal is not installed in the correct position,
____ it cannot inflate correctly during the flight. This causes the cabin pressure to decrease and can result in a disruption of the flight.
1EFF : ALL 1 52-31-18Page 413 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 52-31-18Page 414 1 1 May 01/05 1 1 1CES 1 1EFF : 051-052, 1 52-31-18Page 415 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 52-31-18Page 416 1 1 May 01/05 1 1 1CES 1 SEAL - DOOR - REPAIRS
(2) Install the door actuators (18) in the cargo door as follows:
(a) Put the piston eye-end of the door actuator (18) in the actuator attachment fitting (13) and install the bolt (14) with the washer (15).
(b) If you can not install the bolt (14), adjust the length of the door actuator (Ref. TASK 52-31-11-820-004).
(c) Install the washer (15) and the nut (16) on the bolt (14).
(d) TORQUE the nut (16) to between 1.0 and 1.35 m.daN (88.49 and 119.46 lbf.in) and safety it with the new cotter pin (17).
(e) Install the bonding jumper (10) with the bolt (12), the washer (11) and the nut (9) at the actuator attachment fitting (13) (Ref. TASK 20-28-00-912-004).
(3) Install the wire harness 4611VB (21) in the door actuator area and connect the electrical connector (20) to the receptacle (19) (Ref. TASK 52-31-24-400-001).
R **ON A/C 051-052,
R Subtask 52-31-18-420-050
R R B. Installlation of the Door Seal and the associated Components (Ref. Fig. 401A/TASK 52-31-18-991-001-B, 402A/TASK 52-31-18-991-002)
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 DOORS 艙門4(81)
