Main Structure Cone/Rear Fuselage
Figure 001
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Feb 01/98
CES
E. Fittings
(1)
The attachment fittings for the vertical stabilizer are made of aluminum-alloy and are machined. The attachment fittings are riveted in pairs to the top part of FR70, FR72 and FR74.
(2)
The attachment fittings for the horizontal stabilizer are made of aluminum-alloy. Bolts are used to attach these fittings to the upper and the lower section of FR77.
(3)
The diagonal struts support the fittings and the hinge bearings of the horizontal stabilizer.
(4)
The attachment fittings for the tail-cone are at the aft side of FR77. They are machined and are part of FR77. The working platform in the cone/rear fuselage is between FR71 and FR73. It has an aluminum-alloy frame work and a honeycomb top panel.
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53-51-00Page 3
MAIN STRUCTURE - INSPECTION/CHECK
_________________________________
TASK 53-51-00-210-001
Detailed Visual Inspection of Rear Pressure Bulkhead AFT Face and Fuselage Internal Structure, FR70 and FR71, from STGR 26 LH/RH to Bottom Center Line
1. Reason for the Job
__________________
Refer to the MPD TASK: 535101-01
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific lint-free cloth
No specific nonmetallic scraper
No specific access platform 3.0 m (9 ft. 10 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-013 USA MIL-PRF-81733 TYPE I CLASS A
CORROSION INHIBITING BRUSH CONSISTENCY
(Ref. 20-31-00)
R Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00)
Material No. 15-005 AIB TN 10138 TYPE I GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 15-008 AIB TN 10138 TYPE II GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
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53-51-00Page 601
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
51-75-13-916-002 Repair to a layer of Corrosion Preventive Compound
ASRM 530011 (for corrective action)
ASRM 530012 (for corrective action)
ASRM 530013 (for corrective action)
53-51-00-991-001 Fig. 601
3. Job Set-up
__________
Subtask 53-51-00-010-051
A. Get Access
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION
_______
BEFORE YOU START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
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.
(1)
Put the access platform below the access door 312AR.
(2)
Open the access door 312AR.
(3)
Get access to the inspection area.
(4)
Remove the rear pressure-bulkhead cover (1).
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May 01/01
R
CES (5) Clean the inspection area with CLEANING AGENTS (Material No. 11-003)
and a lint-free cloth . R
4. Procedure
_________
(Ref. Fig. 601/TASK 53-51-00-991-001)
Subtask 53-51-00-210-050
A. Inspection. 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM FUSELAGE 機(jī)身3(99)
