(2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft) 98D27504031000 1 PIN-SETTING 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (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)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
2 cotter pin 27-51-05 01 -010 R 2 cotter pin 27-51-05 01A-010A 7 cotter pin 27-51-05 01 -010
R 7 cotter pin 27-51-05 01A-010A 12 cotter-pin 27-51-05 01 -100 17 cotter-pin 27-51-05 01A-090
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-00-00-480-002 Installation of the Flap/Slat Control-Lever Locking
Tool (98D27803000000) 27-50-00-866-008 Extension of the Flaps on the Ground 27-51-00-710-002 Operational Test of the Flap Interconnecting Strut
and the Flap-Attachment Failure-Detection Sensors 27-51-00-820-003 To Do a Check of the Flap Rigged Position (With the Sharks Fin) 27-54-00-710-001 Operational Test of the Flap System
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-54-61-000-002 Removal of the Flap Kink-Seals 27-54-61-400-006 Installation of the Flap Kink-Seals 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST
F/CTL Page
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-51-44-991-001 Fig. 401
**ON A/C 301-399,
27-51-44-991-001-A Fig. 401A R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
27-51-44-991-004 Fig. 402
**ON A/C 301-399,
27-51-44-991-004-A Fig. 402A
**ON A/C ALL
3. Job Set-up
__________
Subtask 27-51-44-941-061
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the warning notice is in position to tell persons not to operate the flap/slat controls.
Subtask 27-51-44-860-051-A
B. Aircraft Maintenance Configuration
(1)
Make sure that the lower kink seal, the cushion seals and the upper kink seals are removed from the flaps (Ref. TASK 27-54-61-000-002).
(2)
Make sure that the flaps are extended to position 1 (Ref. TASK 27-50-00-866-008).
(3)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is on the flap/slat control lever (Ref. TASK 27-00-00-480-002).
(4)
Make sure that the access platform is in position:
-for the left wing, below zone 580
-for the right wing, below zone 680.
Subtask 27-51-44-865-051
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 401/TASK 27-51-44-991-001)
**ON A/C 301-399,
(Ref. Fig. 401A/TASK 27-51-44-991-001-A) **ON A/C ALL
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
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 FLIGHT CONTROLS 飛行操縱4(107)
