(4)
Remove the intermediate fairing (17) as follows:
(a)
Move the intermediate fairing (17) rearwards in the slotted holes, then lower it a small amount from the wing skin bolts.
(b)
Carefully release the harness (25) from the retention channel (inside the intermediate fairing (17)) and remove the intermediate fairing (17).
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 28-21-49Page 415 1201-227, 1May 01/05 1 1 1CES 1 **ON A/C ALL
TASK 28-21-49-400-001
Installation of the Fuel Pump Fairings
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 : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notice
No specific wax crayon
No specific access platform 2.8 m (9 ft. 2 in.)
R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) R
R 1EFF : ALL 1 28-21-49Page 416 1 1 May 01/05 1 1 1CES 1 B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 05-064 GB ABP1-4053 RELEASE AGENT (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
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears
32-12-00-010-001 Open the Main Gear Doors for Access
32-12-00-410-001 Close the Main Gear Doors after Access
**ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
28-21-49-991-001 Fig. 401
R **ON A/C 106-149, 228-299, 301-399, 401-499,
28-21-49-991-001-B Fig. 401A
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-227,
Post SB 28-1093 For A/C 001-049,051-099,101-105,151-154,201-207,
28-21-49-991-001-A Fig. 401B
1EFF : ALL 1 28-21-49Page 417 1 1 Aug 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
**ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
28-21-49-991-002 Fig. 402 R **ON A/C 106-149, 228-299, 301-399, 401-499,
28-21-49-991-002-C Fig. 402A
**ON A/C 155-158, 208-210,
28-21-49-991-002-A Fig. 402B
**ON A/C 001-049, 051-099, 101-105, 151-199, 201-227,
Post SB 28-1093 For A/C 001-049,051-099,101-105,151-158,201-210,
28-21-49-991-002-B Fig. 402C
**ON A/C ALL
3. Job Set-up
__________
Subtask 28-21-49-941-051
A. Safety Precautions
(1)
Make sure the safety barriers are in position.
(2)
Make sure that the ground safety locks are installed on the landing gear (Ref. TASK 32-00-00-481-001).
(3)
On the panel 400VU:
-
make sure that the landing-gear control-lever 6GA is in the DOWN position
-
make sure that the warning notice is in position to tell persons not to operate the landing gear.
1EFF : ALL 1 28-21-49Page 418 1 1 Aug 01/05 1 1 1CES 1 Subtask 28-21-49-010-051
B. Get Access
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 FUEL 燃油3(47)
