D. Cleaning
(Ref. Fig. 401/TASK 53-19-42-991-001)
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)
Remove the old sealant from the mating surface of the fuselage with a nonmetallic scraper.
(2)
Clean the mating surface of the fuselage with CLEANING AGENTS (Material No. 11-003) and MISCELLANEOUS (Material No. 19-003).
(3)
Remove the old sealant from the screws (1) and (2) with a nonmetallic scraper.
(4)
Clean the screws (1) and (2) with CLEANING AGENTS (Material No. 11-003) and MISCELLANEOUS (Material No. 19-003).
(5)
Remove the old sealant from the component interface with a nonmetallic scraper.
(6)
Clean the component interface with CLEANING AGENTS (Material No. 11-003) and MISCELLANEOUS (Material No. 19-003).
(7)
Do an inspection of the component interface and/or the adjacent area.
Subtask 53-19-42-220-051
E. Check of the Clearances
(Ref. Fig. 402/TASK 53-19-42-991-003)
(1) Put the static port blanking-plate (3) in position on the fuselage structure.
R EFF : 106-149, 154-199, 207-299, 301-399, 53-19-42Page 406 401-499, Aug 01/05
CES
(2)
In zone D, make sure that the out-of-flush dimension A1 is 0.55 -0.25 +0.25 mm (0.0216 -0.0098 +0.0098 in.) between the fuselage structure and the static port blanking-plate (3).
(3)
In zone E, make sure that the out-of-flush dimension A1 is 0.55 -0.35 +0.35 mm (0.0216 -0.0137 +0.0137 in.) between the fuselage structure and the static port blanking-plate (3).
(4)
If necessary, remove the unwanted layers of the laminated shim (4) to adjust the thickness of the static port blanking-plate (3).
NOTE : Initially, the laminated shim (4) of the static port
____ blanking-plate (3) has 16 layers. The thickness of each layer of the laminated shim (4) is 0.05 mm (0.0019 in.). Thus, the total thickness of the laminated shim (4) is 0.8 mm (0.0314 in.).
(5) Remove the static port blanking-plate (3) from the fuselage structure.
Subtask 53-19-42-390-051
F. Application of Sealants
(Ref. Fig. 402/TASK 53-19-42-991-003)
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.
CAUTION : MAKE SURE THAT NO SEALANT GOES INTO THE MIDDLE HOLES OF THE
_______ BLANKING PLATE. SEALANT IN THE HOLES CAN CAUSE DAMAGE TO THE STATIC PROBE AND CAN CAUSE THE PROBE TO GIVE INCORRECT DATA.
(1) On the component interface, put masking tape on the middle holes.
R EFF : 106-149, 154-199, 207-299, 301-399, 53-19-42Page 407 401-499, Aug 01/05
CES
Installation of the Static Port Blanking-Plate Figure 402/TASK 53-19-42-991-003- 12 (SHEET 1)
R EFF : 106-149, 154-199, 207-299, 301-399, 401-499, 53-19-42 Page 408 Aug 01/05
CES
Installation of the Static Port Blanking-Plate Figure 402/TASK 53-19-42-991-003- 22 (SHEET 2)
R EFF : 106-149, 154-199, 207-299, 301-399, 401-499, 53-19-42 Page 409 Aug 01/05
CES
(2) Apply SEALANTS (Material No. 09-019B) to the mating surface of the static port blanking-plate (3).
NOTE : The mating surface of the static port blanking-plate (3) is
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM FUSELAGE 機(jī)身1(128)
