-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004  Electrical Bonding of Components With Conductive
 Bolts and Screws and Bonding Straps in the Fuselage
 and in the Wings (this does not include the tanks)-
27-50-00-000-002  Removal of the Inboard and Outboard Flap
 Hoisting-Sling
 27-50-00-400-002  Installation of the Inboard and Outboard Flap
 Hoisting-Sling
 27-50-00-866-008  Extension of the Flaps on the Ground
 27-50-00-866-009  Retraction of the Flaps on the Ground
 27-50-00-866-011  Manual Extension of the Flaps
 27-50-00-866-012  Manual Retraction of the Flaps
 27-51-00-820-003  To Do a Check of the Flap Rigged Position (With the
 Sharks Fin)
 27-51-00-820-008  Adjustment of the Flap Rigged Position With the
 Sharks Fin Tool (A318/319/320)
 27-51-44-400-001  Installation of the Interconnecting Strut
 27-54-00-710-001  Operational Test of the Flap System
 27-54-61-000-002  Removal of the Flap Kink-Seals
 27-54-61-400-006  Installation of the Flap Kink-Seals
 27-60-00-866-002  Extension-Retraction of the Spoilers for Maintenance
 27-64-00-710-001  Operational Test of the Spoiler Hydraulic Actuation
 32-12-00-410-001  Close the Main Gear Doors after Access
 53-35-11-000-001  Removal of the Wing-to-Fuselage Fairings
 54-55-00-000-001  Removal of the Aft Movable Fairing
 54-55-00-400-001  Installation of the Aft Movable Fairing
 57-55-11-010-001  To Lower the Flap Track No. 2 Movable Fairing for
 Access
 57-55-11-410-001  To Lift the Flap Track No. 2 Movable Fairing after
 Access
 ISB 27-1066
 ISB 27-1108

 **ON A/C 001-001, 051-052, 27-54-61-991-001 Fig. 401
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 429 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, Post SB 27-1117 For A/C 001-001,051-052, 27-54-61-991-001-A Fig. 401A **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 27-54-61-991-012 Fig. 402 **ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
R  27-54-61-991-005 Fig. 403 **ON A/C 106-149, 159-199, 211-299, 401-499,
R  27-54-61-991-005-B Fig. 403A **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 27-54-61-991-006 Fig. 404 27-54-61-991-013 Fig. 405 **ON A/C 001-049, 051-061, 101-103, 201-203,
R  27-54-61-991-007 Fig. 406 **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
R  27-54-61-991-007-A Fig. 406A **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 27-54-61-991-008  Fig. 408 

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 430 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1

 3. Job Set-up
__________ Subtask 27-54-61-941-060
 A. Safety Precautions
 (1)
 Make sure that the safety barriers are in position.

 (2)
 Make sure that the warning notice(s) is on the panel 400VU to tell persons not to operate the landing gear.

 (3)
 Make sure that the warning notice is in position to tell persons not to operate the flight controls.

 Subtask 27-54-61-865-051
 B. 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
 Subtask 27-54-61-860-058
 C. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
 (1)
 Make sure that the flaps are in the position 3 (Ref. TASK 27-50-00-866-011).

 (2)
 Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is on the applicable torque shaft.

 (3)
 Make sure that the access platform is in position below the applicable inboard flap.

 (4)
 Make sure that the number 1 spoiler is fully extended (Ref. TASK 27-60-00-866-002).
　
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6(23)