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时间:2011-03-21 08:16来源:蓝天飞行翻译 作者:admin
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 31-60-00-860-001 EIS Start Procedure
 31-60-00-860-002 EIS Stop Procedure
 32-12-00-010-001 Open the Main Gear Doors for Access
 32-12-00-410-001 Close the Main Gear Doors after Access
 24-24-51-991-001 Fig. 401

 3. Job Set-up
__________
 Subtask 24-24-51-860-052
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the blue hydraulic system is depressurized (Ref. TASK 29-00-00-864-001).

 (2)
 Make sure that the reservoir of the blue hydraulic system is depressurized (Ref. TASK 29-14-00-614-001).

 (3)
 Make sure that the LH and RH Main Landing Gear (MLG) is opened (Ref. TASK 32-12-00-010-001).

 (4)
 Make sure that the stepladder is in position at the MLG bay.


 Subtask 24-24-51-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------105VU ELEC/CSM/G /EV AUTO/SPLY 7XE C01 106VU CSM/G /EV/MAN/SPLY 6XE B04 122VU ELEC/EMER GEN AUTO/2 9XE Z26 122VU ELEC/EMER GEN AUTO/1 11XE Z25


 4. Procedure
_________
 (Ref. Fig. 401/TASK 24-24-51-991-001) Subtask 24-24-51-420-051
 A. Installation of the CSM/G
 (1)
 Put the CSM/G (1) in position on the support mounts (9) on top of the keel beam.

 (2)
 Attach the CSM/G (1) with new lockwashers (8) , the screws (5), the washer (6) and the bonding strap (7) on the support mounts (9) (Ref. TASK 20-28-00-912-004).

 (3)
 Tighten the screws (5).

 (4)
 Safety the screws (5) with the lockwashers (8).

 (5)
 Make sure that the hydraulic line end-fittings are serviceable.

 (6)
 Remove the blanking plugs and connect the hydraulic pipes (11),(12) and (15) to the CSM/G (1).

 (7)
 Remove the blanking plugs and connect the flexible drain hoses (4) and (10) to the CSM/G (1).

 (8)
 Remove the blanking caps and connect the electrical connectors (2), (3), (13) and (14) to the CSM/G (1).


 Subtask 24-24-51-865-055
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6XE, 7XE, 9XE, 11XE.
 Subtask 24-24-51-860-051
 C. Preparation for Test
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).


 (2)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 (3)
 Pressurize the Blue Hydraulic System

 (a)
 Pressurize the reservoir of the Blue hydraulic system (Ref. TASK 29-14-00-614-002).

 (b)
 Pressurize the Blue hydraulic system either with the electric pump or a ground hydraulic cart (Ref. TASK 29-10-00-863-003).

 

 


 Subtask 24-24-51-710-051
 D. Test
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the overhead panel 21VU: On the lower ECAM display unit:
 - open the guard, press and hold - the ELEC page comes into view pushbutton switch EMER GEN TEST automatically. 23XE. - the green lines between the AC1 and
 the DC ESS busbar and the DC1 and the DC ESS busbar go out of view,
 -the EMER GEN and ESS TR indications are shown in white. The parameters are shown in green.
 -green lines come on between: EMER GEN and AC ESS, EMER GEN and ESS TR, ESS TR and DC ESS indications.
 -the SHED indication comes into view below the AC ESS and DC ESS busbar indications.
 NOTE : If the essential TR is not in
____ line:
 -its related parameters are shown in amber,
 -the green line between the ESS TR and the DC ESS busbar is not shown.
 During the CSM/G test (when the CSM/G is running), push the TR RESET pushbutton switch (15PU) on the panel 103VU to reset the essential TR.
 2. On the overhead panel 21VU: On the overhead panel 21VU:

 

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-release the pushbutton switch  - make sure that the safety guard is EMER GEN TEST. back in place.
 On the lower ECAM display unit:
 -the Blue electrical hydraulic pump stops and the generator is disconnected from its network automatically,
 
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