(2)
Remove the screws (1) from the sealing panel (2).
(3)
Remove the sealing panel (2).
(4)
Remove the screws (4) from the upper side of the access panel (3), which you can see.
(5)
Remove the screws (5) from the upper clip assy (7).
(6)
Retract the flaps (Ref. TASK 27-50-00-866-009).
(7)
Remove the screws (4) from the lower side of the access panel (3).
(8)
Remove the screws (5) from the lower clip assy (6).
(9)
Hold the reinforcement hook plate (11) and remove the screws (10) and the bushes (9).
(10)
Remove the access panel (3) together with the slide panel (8) from the fuselage.
(11)
Remove the reinforcement hook plate (11).
(12)
Pull the slide panel (8) out of the access panel (3).
(13) Remove any loose and unwanted sealant in the related area.
Subtask 53-35-11-020-053
D. Removal of the Access Panel 193AB (194AB)
(Ref. Fig. 413/TASK 53-35-11-991-020)
(1)
Fully extend the flaps (Ref. TASK 27-50-00-866-008).
(2)
Remove the screws (2) from the sealing panel (1).
EFF : ALL
53-35-11Page 425
R Access Panel 193BB (194BB) Figure 412A/TASK 53-35-11-991-019-A
EFF : ALL 53-35-11 Page 426 May 01/04
CES
Panel 193AB (194AB) Figure 413/TASK 53-35-11-991-020
R EFF : CES ALL 53-35-11 Page 427 May 01/05
(3)
Remove the sealing panel (1).
(4)
Remove the screws (3) from the upper side of the access panel (7), which you can see.
(5)
Remove the screws (5) from the upper clip assy (6).
(6)
Retract the flaps (Ref. TASK 27-50-00-866-009).
(7)
Remove the screws (5) from the lower clip assy (4).
(8)
Remove the screws (3) from the lower side of the access panel (7).
(9)
Remove the access panel (7) from the fuselage.
(10) Remove any loose and unwanted sealant in the related area.
EFF : ALL
53-35-11Page 428
May 01/05
R
CES
**ON A/C ALL
TASK 53-35-11-400-001
Installation of the Wing-to-Fuselage Fairings
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific adhesive tape
No specific emery cloth, grade 120 to 240
No specific emery cloth, grade 180
No specific lint-free cloth
No specific nonmetallic pencil
No specific plastic spatula
No specific spatula
No specific Torque Wrench : range 35 to 40 lbf.in
(0.39 to 0.45 m.daN) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific BONDING COMPOUND PQ10054.040 (Caf.4)
No specific SILICONE SEALANTS RTV 3145, GREY
Material No. 05-013A C Z-24.223
RELEASE AGENT (Ref. 20-31-00) Material No. 07-006 AIB TN 10106 TYPE II ANTISTATIC PAINT (HIGH RESISTIVITY) (Ref. 20-31-00) Material No. 08-004 USA MIL-A-25457 ADHESIVE SEALANT (Ref. 20-31-00)
EFF : ALL
53-35-11Page 429
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 08-004A USA MIL-A-46106 TYPE I
ADHESIVE SEALANT (Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
Material No. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
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本文鏈接地址：A320飛機維護手冊 AMM FUSELAGE 機身2(111)
