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时间:2011-03-21 08:13来源:蓝天飞行翻译 作者:admin
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 D. Operational test of the GPCU without the CFDS.
 (1) Start the engine 1(2) automatically (Ref. TASK 71-00-00-710-003).
 (2) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
 (3) On the ECAM control panel: - push the ELEC key to get the ELEC system page.

 

 (4) On the lower ECAM display unit, make sure that there is the green line between GEN1(2) and AC1(2).
 (5) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002)
 (6) Stop the engine 1 (2) (Ref. TASK 71-00-00-710-028).
 **ON A/C 106-149, 229-299, 303-399,
 Subtask 24-22-34-710-051-A
 D. Operational test of the GPCU without the CFDS.
 (1) Start the engine 1(2) automatically (Ref. TASK 71-00-00-710-043).
 (2) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
 (3) On the ECAM control panel: - push the ELEC key to get the ELEC system page.
 (4) On the lower ECAM display unit, make sure that there is the green line between GEN1(2) and AC1(2).
 (5) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002)
 (6) Stop the engine 1(2) (Ref. TASK 71-00-00-710-018). 
R  **ON A/C 401-499, 
R  Subtask 24-22-34-710-051-B 
R  D. Operational test of the GAPCU without the CFDS. 
R  (1) Start the engine 1(2) automatically (Ref. TASK 71-00-00-710-043). 
R R  (2) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001). 
R R  (3) On the ECAM control panel: - push the ELEC key to get the ELEC system page.

 

R R  (4) On the lower ECAM display unit, make sure that there is the green line between GEN1(2) and AC1(2). 
R R  (5) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002) 
R  (6) Stop the engine 1(2) (Ref. TASK 71-00-00-710-018).
 **ON A/C ALL
 5. Close-up________
 Subtask 24-22-34-410-050
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Close the access door 811.
 (3) Remove the warning notice(s).
 (4) Remove the access platform(s).

 

 MODULE - LIGHTNING PROTECTION (19XU1,19XU2) - REMOVAL/INSTALLATION
__________________________________________________________________
 TASK 24-22-51-000-001
 Removal of the Lightning Protection Modules (19XU1, 19XU2)

 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notices
 No specific access platform 0.5 m (1 ft. 8 in.)

 B. Referenced Information -------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------25-11-41-000-001 Removal of the Third Occupant Seat **ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,
 24-22-51-991-001 Fig. 401 R **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
 24-22-51-991-001-A Fig. 401A FOR FIN 19XU1 24-22-55-000-001 Removal of the Contactors (9XU1, 9XU2, 11XU1, 11XU2) FOR FIN 19XU2 24-22-55-000-001 Removal of the Contactors (9XU1, 9XU2, 11XU1, 11XU2) **ON A/C ALL


 3. Job Set-up
__________
 **ON A/C 001-049, 051-062, 101-105, 151-152, 201-205,

 Subtask 24-22-51-010-050
 A. Get Access
 (1)
 FOR 19XU1
 Remove the contactor 9XU1.
 (Ref. TASK 24-22-55-000-001)


 (2)
 FOR 19XU2
 Remove the contactor 9XU2.
 (Ref. TASK 24-22-55-000-001)

 


R **ON A/C 063-099, 106-149, 153-199, 206-299, 301-399, 401-499,
 Subtask 24-22-51-010-050-A
 A. Get Access
 (1)
 Remove the Third Occupant seat (Ref. TASK 25-11-41-000-001).

 (2)
 On the L lower side of the panel 120VU, remove the access door.

 (3)
 Put the access platform in position at the access door 121AL.


 (4) Open the access door 121AL.
 Subtask 24-22-51-860-053

 B. Safety Precautions
 (1)
 Make sure that the external power connector is not connected to the aircraft EXT PWR receptacle.


 
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