(7)
Press and hold the ends of the replacement section and the seal
together and let them dry for some minutes.
(8)
Cut a piece of SPECIAL MATERIALS (Material No. 05-024) to a size of the repair areas.
(9)
Apply a layer of BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) BONDING AND ADHESIVE COMPOUNDS (Material No. 08-026) to the contact surface of the replacement tissue and the repair areas.
(10)
Wind the replacement tissue around the repair areas.
(11)
Cover the repair area with a layer of foil SPECIAL MATERIALS (Material No. 05-023) and put the seal in the wooden bonding block.
(12)
Compress the seal over a period of 24 hours in the wooden bonding block with a clamp.
(13)
Remove the wooden bonding block and the foil from the repair area of the seal.
(14)
Prepare the repair area with very fine emery cloth to get a smooth surface on the seal.
1EFF : ALL 1 52-32-18Page 807 1 1 Feb 01/98 1 1 1CES 1 Subtask 52-32-18-350-050
C. Repair of the Chafe Marks
(1)
Prepare the chafe mark with very fine emery cloth.
(2)
Carefully degrease the chafe mark with CLEANING AGENTS (Material No. 11-016) and a lint-free cloth.
(3)
Apply a thin layer of BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) BONDING AND ADHESIVE COMPOUNDS (Material No. 08-026) to the chafe mark with a spatula.
(4)
Prevent a dust layer on the treated chafe marks during the BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004) drying period of 10 to 12 hours.
5. Close-up
________ Subtask 52-32-18-410-051
A. Close Access
(1)
Install the repaired door seal (Ref. TASK 52-32-18-400-001).
(2)
Close the applicable cargo compartment door (Ref. TASK 52-30-00-860-002).
1EFF : ALL 1 52-32-18Page 808 1 1 Feb 01/98 1 1 1CES 1 1EFF : ALL 1 52-32-18Page 809 1 1 Aug 01/01 1 1 1CES 1
R TASK 52-32-18-300-002
R Reinforcement of Door Seal
R 1. Reason for the Job__________________
R Self Explanatory
R 2. Job Set-up Information______________________
R A. Fixtures, Tools, Test and Support Equipment
R -------------------------------------------------------------------------------
R REFERENCE QTY DESIGNATION
R -------------------------------------------------------------------------------
R No specific additional silicon tube (Spec: NSA 3629-8-12)
R No specific very fine emery cloth
R No specific wooden bonding block
R B. Consumable Materials
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R Material No. 05-023 USA MIL-I-631
R POLYTEREPTHALATE (Ref. 20-31-00)
R Material No. 08-004 USA MIL-A-25457
R ADHESIVE SEALANT (Ref. 20-31-00)
R Material No. 08-026
R ADHESIVE/SEALANT ONE PART,RTV SILICONE RUBBER
R (Ref. 20-31-00)
R C. Referenced Information
R -------------------------------------------------------------------------------
R REFERENCE DESIGNATION
R -------------------------------------------------------------------------------
R 52-30-00-860-001 Open the FWD or AFT Cargo-Compartment Door with the
R Yellow Electric Pump
R 52-30-00-860-002 Close the FWD or AFT Cargo-Compartment Door with the
R Yellow Electric Pump
R 52-31-18-000-001 Removal of the Door Seal
R 52-31-18-400-001 Installation of the Door Seal
R 52-32-18-991-007 Fig. 804
3. Job Set-up
__________
Subtask 52-32-18-010-052
A. Get Access
(1)
Open the AFT cargo compartment door and safty it with the support struts (Ref. TASK 52-30-00-860-001).
(2)
Remove the door seal (Ref. TASK 52-31-18-000-001).
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
Subtask 52-32-18-350-051
A. Reinforcement of Door Seal
(Ref. Fig. 804/TASK 52-32-18-991-007)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM DOORS 舱门5(73)
