Material No. 09-008 USA MIL-S-8802 CLASS A EARLY QUICK REPAIR FUEL TANK SEALANT (Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
Material No. 16-021 F ASNB70720
FLEXIBLE POLYURETHANE (Ref. 20-31-00)
1EFF : ALL 1 34-53-11Page 408 1 1 May 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
Material No. 19-002 USA MIL-T-713
SYNTHETIC FIBRE CORD (NYLON) 2.5MM DIA.
(Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
R 20-21-15-912-001 Tightening Torques for Electrical Component Fasteners 20-28-00-912-005 Electrical Bonding of Antennas With Conductive Bolts. 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 34-53-00-710-002 Operational Test of the ADF 51-76-11-300-001 Repair of the Sealing
**ON A/C 001-049, 051-099, 101-149, 201-299,
34-53-11-991-001 Fig. 401
R **ON A/C 151-199, 401-499,
34-53-11-991-001-A Fig. 401A
**ON A/C 301-399,
34-53-11-991-001-B Fig. 401B
1EFF : ALL 1 34-53-11Page 409 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL
3. Job Set-up
__________
Subtask 34-53-11-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the ground service network is energized (Ref. TASK 24-42-00-861-001).
(2)
Make sure that the access platform is in position.
(3)
Make sure that the aircraft is in the same configuration as for the removal task.
(4)
Make sure that the parts retained from the removed component are clean and in the correct condition.
**ON A/C 301-399,
Subtask 34-53-11-865-051
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU NAV/ADF/1 1RP1 H14 121VU COM NAV/ADF/2 1RP2 K02
**ON A/C ALL
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 401/TASK 34-53-11-991-001)
1EFF : ALL 1 34-53-11Page 410 1 1 May 01/05 1 1 1CES 1
R **ON A/C 151-199, 401-499,
(Ref. Fig. 401A/TASK 34-53-11-991-001-A) **ON A/C 301-399,
(Ref. Fig. 401B/TASK 34-53-11-991-001-B) **ON A/C ALL
Subtask 34-53-11-420-051
A. Installation of the ADF Loop and Sense Antenna
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 : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE SPECIAL
_______
MATERIAL.
THIS MATERIAL IS DANGEROUS.
(1)
Clean the component interface and/or the adjacent area with CLEANING AGENTS (Material No. 11-004) and lint free cloth.
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Remove the blanking caps from the electrical connectors.
(4)
Make sure that the electrical connectors are clean and in the correct condition.
(5)
Put the new o-ring (3) in the correct position on the antenna.
(6)
Put the new gasket (4) on the fuselage and align the bolts hole.
(7)
Remove the masking tape from the coaxial cable (6) and connect the cable connector (5) to the antenna connector.
1EFF : ALL 1 34-53-11Page 411 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 34-53-11Page 412 1 1 Aug 01/05 1 1 1CES 1
R R (8) Install the antenna (2) ) to the fuselage structure with the bolts (1).
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 NAVIGATION 導航4(157)
