Subtask 28-11-00-160-051
C. Cleaning after Test 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.
(1)
Use CLEANING AGENTS (Material No. 11-004) and a clean MISCELLANEOUS (Material No. 19-003) to remove dye from the tank.
(2)
Make sure that all the dye is removed and that the tank is clean.
5. Close-up
________
Subtask 28-11-00-080-053
A. Removal of Test Equipment
(1)
Remove the vacuum equipment from the DUMMY DOOR-NACA VENT (13).
(2)
Remove the manometer from the DUMMY DOOR-NACA VENT (13).
(3)
Remove the bolts (12) and the washers (11) from the DUMMY DOOR-NACA VENT (98D57204000000). Remove the DUMMY DOOR-NACA VENT.
1EFF : ALL 1 28-11-00Page 563 1 1 May 01/04 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 28-11-00-410-064
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install and TORQUE the bolts (10) in opposite sequence:
-
to between 25 and 30 lbf.in (0.28 and 0.33 m.daN) then
-
to between 90 and 100 lbf.in (1.01 and 1.13 m.daN).
(3)
Install the fuel tank access panels that you removed (Ref. TASK 28-10-00-910-002), (Ref. TASK 57-17-11-400-001), (Ref. TASK 57-27-11-400-001) and (Ref. TASK 57-27-11-400-002).
(4)
Install the applicable wing leading-edge access panels.
(5) Install the applicable wing trailing-edge access panels.
**ON A/C 301-399,
Subtask 28-11-00-410-064-A
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install and TORQUE the bolts (10) in opposite sequence:
-
to between 25 and 30 lbf.in (0.28 and 0.33 m.daN) then
-
to between 90 and 100 lbf.in (1.01 and 1.13 m.daN).
(3)
Install the fuel tank access panels that you removed (Ref. TASK 28-10-00-910-002), (Ref. TASK 57-17-11-400-001), (Ref. TASK 57-27-11-400-001) and (Ref. TASK 57-27-11-400-002).
(4)
Install the applicable wing leading-edge access panels.
(5)
Install the applicable wing trailing-edge access panels.
1EFF : ALL 1 28-11-00Page 564 1 1 Aug 01/05 1 1 1CES 1R **ON A/C ALL
Subtask 28-11-00-865-093
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
R 1QA, 2QA, 7QA, 8QA, 11QA, 12QA, 29QA, 30QA, 1QL, 2QL, 1QE, 2QE, 1QU, 2QU, 1QF, 2QF, 1QG, 2QG, 3QG, 4QG.
Subtask 28-11-00-860-069
D. Aircraft Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
Retract the spoilers (Ref. TASK 27-60-00-866-002).
(2)
On the spoiler servo-control, make sure that the pointer on the hex. head is opposite the letter 'O' on the housing.
(3)
Retract the flaps fully (Ref. TASK 27-50-00-866-009).
(4)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is on the slat/flap control lever.
(5)
Refuel, defuel or transfer fuel as necessary (Ref. TASK 28-25-00-869-001) (Ref. TASK 12-11-28-650-003) (Ref. TASK 28-25-00-650-001).
Subtask 28-11-00-942-083
E. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the access platform(s).
(3)
Close the MLG doors (Ref. TASK 32-12-00-410-001).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 28-11-00Page 565 1 1 May 01/04 1 1 1CES 1 TASK 28-11-00-790-009
Leak Test of the Fuel Tanks - Without Fuel - Helium Procedure
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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 FUEL 燃油1(123)
