R 57-10-00-991-022 Fig. 615
3. Job Set-up
__________
Subtask 57-10-00-941-070
A. Safety Precautions
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
(1)
Obey the fuel safety precautions (Ref. TASK 28-00-00-910-001) and (Ref. TASK 28-10-00-910-001).
(2)
Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
(3)
Put warning notices in the cockpit to tell persons not to operate the flaps or slats.
Subtask 57-10-00-010-069
B. Get Access
(1)
Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE below the access panels 540AB and 640AB.
(2)
Remove the access panels: (Ref. TASK 57-27-11-000-001) (Ref. TASK 28-10-00-910-002)
-
for the left wing: 540AB
-
for the right wing: 640AB.
(3)
Open the RIB2 surge doors:
-
for the left wing: 540AZ, 540BZ
-
for the right wing: 640AZ, 640BZ.
(4)
Install the HOOK-COVER (RIB 2 SURGE DOORS) (98D57004013000) on the forward surge doors.
(5)
Install the HOOK-COVER (RIB2-SURGE DOORS) (98D57004014000) on the aft surge doors.
(6)
Use a FLASHLIGHT, if necessary.
Subtask 57-10-00-110-062
C. Cleaning of the Structure
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 THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
(1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if necessary.
4. Procedure
_________
Subtask 57-10-00-220-062
A. Inspection R (Ref. Fig. 615/TASK 57-10-00-991-022)
(1)
Do a detailed inspection of:
-
the external surface of RIB1
-
the top surface of the triform fitting of the outer wing box. This inspection is applicable between the front spar and the rear spar.
(2)
Make sure that there is no:
(a)
Corrosion damage:
-If you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 512200,P.Block001) for types of corrosion, inspection, removal and corrosion protection.
(b)
Other damage (cracks, scratches, stress, marks dents, bumps...):
R RIB1 - Left and Right Sides - External Structure Figure 615/TASK 57-10-00-991-022
1EFF : 1 1 1CES ALL 1 111 57-10-00 Page 671 May 01/05
-If you find this type of damage, refer to the Structural Repair Manual (Ref. SRM 511100,P.Block001) for damage classification and corrective action.
5. Close-up
________
Subtask 57-10-00-410-068
A. Close Access
(1)
Remove the HOOK-COVER (RIB 2 SURGE DOORS) (98D57004013000) on the forward surge doors.
(2)
Remove the HOOK-COVER (RIB2-SURGE DOORS) (98D57004014000) on the aft surge doors.
(3)
Close the RIB2 surge doors:
-
for the left wing: 540AZ, 540BZ
-
for the right wing: 640AZ, 640BZ.
(4)
Install the access panels:
(Ref. TASK 57-27-11-400-001)
-
for the left wing: 540AB
-
for the right wing: 640AB.
Subtask 57-10-00-942-079
B. Put the Aircraft back to its Initial Configuration.
(1)
Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the flap/slat control lever.
(2)
Make sure that the work area is clean and clear of tool(s) and other items.
(3)
Remove the warning notice(s).
(4)
Remove the access platform(s).
1EFF : ALL 1 57-10-00Page 672 1 1 May 01/05R 1 1 1CES 1
TASK 57-10-00-200-023
Special Detailed Inspection of CWB, Upper Surface of Triform Fitting (On First Row of Fasteners from RIB1), between Stringer No 8 and FR42, LH/RH
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 WINGS 機翼1(57)
