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时间:2011-03-21 14:21来源:蓝天飞行翻译 作者:admin
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R  ECAM Display Unit (Ref 31-64) via the FCDC. 
R  2. System Description__________________ 
R  A. Roll function 
R  (Law ref 27-90, Spoilers Slaving and Monitoring Ref 27-94) 
R  The spoilers 2 thru 5 assist the ailerons in roll control. 
R  The Roll axis is controlled and monitored by the three SEC's associated 
R  with ailerons. 
R  The SEC's elaborate the surface deflection orders: 
R  In manual control mode, minly from the side stick (Ref 27-92) 
R  In autopilot mode from FMGES (Ref 22-10).

 


R  B. Speedbrake function 
R  (Ref. Fig. 001) 
R  (Law Ref 27-90, Spoilers Slaving and Monitoring Ref 27-94) 
R  The speedbrake function is controled and monitored by the three SEC's 
R  with spoilers 2, 3 and 4. 
R  The speedbrake lever controls the position of these spoilers and so is 
R  used for the preselection of ground spoilers function. 

R  C. Ground Spoilers 
R  (Ref. Fig. 002) 
R  (Law Ref 27-90, Spoilers Slaving and Monitoring Ref 27-94) 
R  The ground spoilers function is ensured by all spoilers. 
R  The activation of this function is dependent upon: 
R  - The function preselection (give by speedbrake lever position) 
R  - The two engines at idle 
R  - Flight/Ground transition (With Ground and wheel speed information). 
R

 

 Speedbrake Function - Block Diagram
 Figure 001

 1EFF : ALL 1 27-60-00Page 3/4 1 1 Feb 01/98 1 1 1CES
1


 Ground Spoilers - Block Diagram
 Figure 002

 1EFF : ALL 1 27-60-00Page 5/6 1 1 Feb 01/98 1 1 1CES
1 SPOILER - MAINTENANCE PRACTICES


_______________________________
 TASK 27-60-00-866-002
 Extension-Retraction of the Spoilers for Maintenance
 NOTE : The procedure is the same for all spoilers
____
 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 access platform 1.6 m (5 ft. 3 in.)
 No specific access platform 3.5 m (11 ft. 6 in.)
 No specific metal rod (tommy bar) dia. 4 mm (0.1574 in.)
 98D27603002001 1 SPOILER MAINTENANCE KEY
 98D27604000000 1 COLLAR-SAFETY, SPOILER
 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-00-00-080-002 Removal of the Flap/Slat Control-Lever Locking Tool
 (98D27803000000) 27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 27-64-00-710-001 Operational Test of the Spoiler Hydraulic Actuation 27-80-00-866-004 Extending the Slats on the Ground
R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 27-60-00-991-003 Fig. 201 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

 

R **ON A/C 051-051,
R 27-60-00-991-003-A Fig. 201A R **ON A/C ALL
 3. Job Set-up
__________
 Subtask 27-60-00-860-050

 A. Aircraft Maintenance Configuration
 (1)
 Extend the slats and flaps (Ref. TASK 27-50-00-866-008) (Ref. TASK 27-80-00-866-004).

 (2)
 Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is in position on the flap/slat control lever

 (3)
 Put the warning notice on the HYD section of the panel 40VU to tell persons not to pressurize the aircraft hydraulic systems.


 Subtask 27-60-00-010-051
 B. Get Access
 (1)
 Put the access platform in position at the access door 822.

 (2)
 Open the access door 822.

 (3)
 On the battery power center 105VU:

 -loosen the two screws and remove the protective cover.

 (4)
 Put the access platform in position :

 (a)
 
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