R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) 98D55307531001 1 SLING - DORSAL FIN, LEADING EDGES, END CAP
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-052 SELF-ADHES.PVC DISKS FOR HOISTING POINT BLANKING (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. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
Material No. 11-003 USA ASTM D 740
METHYL-ETHYL-KETONE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
EFF : ALL
53-45-11Page 405
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
51-76-11-300-001 Repair of the Sealing 53-45-11-991-001 Fig. 401
3. Job Set-up
__________
Subtask 53-45-11-865-051
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 53-45-11-869-050
B. Aircraft Maintenance Configuration
(1)
Make sure that the aircraft is in the same configuration as for the removal task.
(2)
Make sure that the warning notice is in position to tell persons not to operate the flight controls.
EFF : ALL
53-45-11Page 406
Feb 01/00
R
CES EFF : ALL
4. Procedure_________
(Ref. Fig. 401/TASK 53-45-11-991-001)
Subtask 53-45-11-914-050
A. Preparation for Installation:
R R (1) Remove the old sealant from the dorsal fin and the aircraft mating surfaces with a SCRAPER - NON METALLIC.
R R R (2) Clean the dorsal fin and aircraft mating surfaces with CLEANING AGENTS (Material No. 11-003) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003).
WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THE_______ SPECIAL MATERIAL. THIS MATERIAL IS DANGEROUS.
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.
R R (3) Apply SEALANTS (Material No. 09-018) to the dorsal fin and aircraft mating surfaces (Ref. TASK 51-76-11-300-001).
Subtask 53-45-11-420-050
B. Installation:
(1) Make sure that the work area is clean and clear of tool(s) and other items.
R R (2) Attach the SLING - DORSAL FIN, LEADING EDGES, END CAP (98D55307531001) to the crane and the hoisting lug (2).
R R (3) Lift the dorsal fin (4) with the CRANE HEIGHT 10 M (33 FT) and put it in the installation position on the aircraft.
R (4) Install the screws (3) and TORQUE to 0.3 m.daN (26.54 lbf.in).
53-45-11Page 407
Aug 01/03
(5)
Make sure that the clearances at points 'a', 'b' and 'c' are as follows:
-
point 'a' is 10.0 +3.5 -3.5 mm (0.3937 +0.1377 -0.1377 in.),
-
point 'b' is 1.0 +1.0 -1.0 mm (0.0393 +0.0393 -0.0393 in.),
-
point 'c' is 3.5 +0.5 -0.5 mm (0.1377 +0.0196 -0.0196 in.).
(6)
Disconnect the sling from the hoisting lug (2).
(7)
Remove the hoisting lug (2) from the hoisting point (1).
(8)
Install the plastic plug in the hoisting point (1).
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FUSELAGE 機身3(89)
