Nov 01/04
R
CES C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ASRM 53-41-11-101 (for corrective action)
ASRM 53-41-11-201 (for corrective action)
**ON A/C 001-049, 051-099, 101-149, 201-299,
53-41-00-991-063 Fig. 645 R **ON A/C 151-199, 401-499,
53-41-00-991-063-A Fig. 645A
**ON A/C 301-399,
53-41-00-991-063-B Fig. 645B
**ON A/C ALL
3. Job Set-up
__________
Subtask 53-41-00-941-072
A. Install the ground support equipment.
(1)
Put a warning notice in position to tell persons not to operate the flight controls.
(2)
Put the ACCESS PLATFORM 3M (10 FT)- ADJUSTABLE in the required position.
Subtask 53-41-00-110-095
B. Cleaning Procedure WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE
_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK.
WARNING : MAKE SURE THAT THERE IS A GOOD FLOW OF AIR THROUGH THE WORK
_______ AREA WHEN YOU USE SPECIAL MATERIALS. IF YOU GET ONE OF THESE MATERIALS ON YOUR SKIN, IN YOUR MOUTH OR IN YOUR EYES : -FLUSH IT AWAY WITH A FLOW OF CLEAN WATER FOR BETWEEN 10 AND 15 MINUTES. -GET IMMEDIATE MEDICAL AID IF IRRITATION OCCURS. DO NOT BREATHE THE FUMES FROM THE MATERIAL. DO NOT SMOKE WHEN YOU USE THE MATERIAL. DO NOT USE THE MATERIAL NEAR A FLAME, SPARKS OR SOURCES OF HEAT. THESE MATERIALS ARE DANGEROUS : THEY ARE POISONOUS, FLAMMABLE AND SKIN IRRITANTS.
(1) Clean the area with a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003) and the CLEANING AGENTS (Material No. 11-004), and let the area dry.
4. Procedure
_________
**ON A/C 001-049, 051-099, 101-149, 201-299,
(Ref. Fig. 645/TASK 53-41-00-991-063)
R **ON A/C 151-199, 401-499,
(Ref. Fig. 645A/TASK 53-41-00-991-063-A)
**ON A/C 301-399,
(Ref. Fig. 645B/TASK 53-41-00-991-063-B)
**ON A/C 001-049, 051-099, 101-149, 201-299,
Subtask 53-41-00-210-114
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
-the lower skin of the longitudinal lap joints in the crack stopper areas at stringer 18, LH/RH between FR 47 and FR 64, external surface.
Lower Skin of longitudinal Lap Joints in Crack Stopper Areas at Stringer 18, LH/RH, External Surface Figure 645/TASK 53-41-00-991-063
CES
Lower Skin of longitudinal Lap Joints in Crack Stopper Areas at Stringer 18, LH/RH, External Surface Figure 645A/TASK 53-41-00-991-063-A
CES
Lower Skin of longitudinal Lap Joints in Crack Stopper Areas at Stringer 18, LH/RH, External Surface Figure 645B/TASK 53-41-00-991-063-B
CES NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for
____
the allowable damage limits.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for
____
the correct repair procedure.
R **ON A/C 151-199, 401-499,
Subtask 53-41-00-210-114-A
A. Inspection
(1) Examine the following area for scratches, dents and cracks:
-the lower skin of the longitudinal lap joints in the crack stopper areas at stringer 18, LH/RH between FR 47/51 and FR 64, external surface.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-101) for
____
the allowable damage limits.
NOTE : If necessary, refer to the ASRM (Ref. ASRM 53-41-11-201) for
____
the correct repair procedure.
**ON A/C 301-399,
Subtask 53-41-00-210-114-B
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FUSELAGE 機身3(36)
