1EFF : ALL 1 27-54-49Page 417 1 1 May 01/05R 1 1 1CES 1
TASK 27-54-49-000-001
Removal of the Flap Track 1 Actuator 6205CM(6255CM)
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.
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job__________________
Self Explanatory
2. Job Set-up Information______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific clamp No specific safety barriers No specific warning notice No specific warning notice(s) No specific access platform 2.8 m (9 ft. 2 in.) 98D27504030001 1 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT
1EFF : ALL 1 27-54-49Page 418 1 1 May 01/05R 1 1 1CES 1
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power
27-50-00-400-003 27-50-00-866-008 27-54-45-000-002 27-54-45-000-003 31-32-00-860-006 32-12-00-010-001 27-54-49-400-001 Installation of the Lock-Torque Shaft - Flaps and Slats (98D27504030001)Extension of the Flaps on the GroundRemoval of the Torque Shaft 6204CM(6254CM)Removal of the Torque Shaft 6206CM(6256CM)Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL PageOpen the Main Gear Doors for AccessInstallation of the Flap Track 1 Actuator 6205CM(6255CM) (for corrective action)
**ON A/C 001-049, 051-061, 101-103, 201-203,
27-54-49-991-001 Fig. 402
R **ON A/C 062-099, 106-149, 151-199, 204-299, 401-499,
27-54-49-991-001-B Fig. 402A
**ON A/C 104-105,
27-54-49-991-001-A Fig. 402B
**ON A/C 301-399,
27-54-49-991-001-C Fig. 402C **ON A/C 001-049, 051-061, 101-103, 201-203, 301-399, 27-54-49-991-005 Fig. 403
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
27-54-49-991-005-A Fig. 403A
FOR FIN 6205CM
57-51-37-000-002 Removal of the Access Panels 573AB(673AB),
573BB(673BB), 573CB(673CB)
FOR FIN 6255CM
57-51-37-000-002 Removal of the Access Panels 573AB(673AB),
573BB(673BB), 573CB(673CB)
**ON A/C ALL
3. Job Set-up
__________
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 402/TASK 27-54-49-991-001) R **ON A/C 062-099, 106-149, 151-199, 204-299, 401-499,
(Ref. Fig. 402A/TASK 27-54-49-991-001-B)
**ON A/C 104-105,
(Ref. Fig. 402B/TASK 27-54-49-991-001-A)
**ON A/C 301-399,
(Ref. Fig. 402C/TASK 27-54-49-991-001-C)
**ON A/C 001-049, 051-061, 101-103, 201-203, 301-399,
(Ref. Fig. 403/TASK 27-54-49-991-005)
Flap Track 1 Actuator
Figure 402/TASK 27-54-49-991-001
R 1EFF : 001-049, 051-061, 101-103, 201-203, 1 27-54-49Page 421 1 1 May 01/05 1 1 1CES 1
Flap Track 1 Actuator Figure 402A/TASK 27-54-49-991-001-B
R 1EFF : 062-099, 106-149, 151-199, 204-299, 1 27-54-49Page 422 1401-499, 1Aug 01/05 1 1 1CES 1
Flap Track 1 Actuator
R Figure 402B/TASK 27-54-49-991-001-A
R 1EFF : 104-105, 1 27-54-49 Page 423
1 1 May 01/05
1 1
1CES 1
R Flap Track 1 Actuator
R Figure 402C/TASK 27-54-49-991-001-C
R 1EFF : 301-399, 1 27-54-49 Page 424
1 1 May 01/04
1 1
中國航空網 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5(101)
