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时间:2011-03-26 09:15来源:蓝天飞行翻译 作者:admin
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 from the External Power 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 36-12-00-860-002 Pressurization of the Bleed System through the HP
 Ground Connector
 36-12-41-000-001 Removal of a Bleed-Air Duct
 36-12-41-400-001 Installation of a Bleed-Air Duct


R  49-00-00-860-003 APU Start by External Power (GTCP 36-300)
R  49-00-00-860-004 APU Shutdown by External Power (GTCP 36-300) 49-00-00-860-008 APU Start by External Power (131-9(A)) 49-00-00-860-009 APU Shutdown by External Power (131-9(A)) 53-35-13-000-001 Removal of the Belly Fairing Access Panels
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 36-12-00Page 538 1201-210, 1May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------


REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
53-35-13-000-002 Removal of the Quick-Release Access Panels from the
 Belly Fairing Structure 53-35-13-400-001 Installation of the Belly Fairing Access Panels 53-35-13-400-002 Installation of the Quick-Release Access Panels on
 the Belly Fairing Structure 20-26-00-910-002 Installation of Expansion Joints (for corrective action)

R **ON A/C 001-049, 051-099, 101-105, 201-210,
 36-12-00-991-001 Fig. 501
 **ON A/C 151-199,
 36-12-00-991-001-A Fig. 501A

R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,
 3. Job Set-up
__________

R **ON A/C 001-049, 051-099, 101-105, 201-210,
 Subtask 36-12-00-010-054
 A. Get Access
 (Ref. Fig. 501/TASK 36-12-00-991-001)

 (1)
 Get access to the APU bleed-air ducts between FR34 and FR36.

 (a)
 Put the access platform in position below the access panels 191BB, 191EB 192FB and 192EB.

 (b)
 Remove the access panels 191BB, 191EB, 192FB and 192EB (Ref. TASK 53-35-13-000-002).

 

 (2)
 Get access to the APU bleed-air ducts between FR36 and FR42.


 (a) Put the access platform in position below the access panels 191JB, 192KB and 196AB.
R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 36-12-00Page 539 1201-210, 1May 01/05 1 1 1CES 1


 (b) Remove the access panel 191JB, 192KB and 196AB (Ref. TASK 53-35-13-000-001).
 (3) Get access to the APU bleed-air ducts between FR42 and FR50.
 (a)
 Put the access platform in position below the access panels 147AB, 147EB, 147FB and 197BB.

 (b)
 Remove the access panels 147AB, 147EB, 147FB and 197BB (Ref. TASK 53-35-13-000-001).


 **ON A/C 151-199,
 Subtask 36-12-00-010-054-A
 A. Get Access
 (Ref. Fig. 501A/TASK 36-12-00-991-001-A)

 (1)
 Get access to the APU bleed-air ducts between FR34 and FR36.

 (a)
 Put the access platform in position below the access panels 191BB, 191EB, 192FB and 192EB.

 (b)
 Remove the access panels 191BB, 191EB, 192FB and 192EB (Ref. TASK 53-35-13-000-002).

 

 (2)
 Get access to the APU bleed-air ducts between FR36 and FR42.

 (a)
 Put the access platform in position below the access panels 191JB, 192KB and 196AB.

 (b)
 Remove the access panel 191JB, 192KB and 196AB (Ref. TASK 53-35-13-000-001).

 

 (3)
 Get access to the APU bleed-air ducts between FR42 and FR54.

 (a)
 Put the access platform in position below the access panels 147AB, 147EB, 147FB and 197BB.

 (b)
 Remove the access panels 147AB, 147EB, 147FB and 197BB (Ref. TASK 53-35-13-000-001).

 


R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 36-12-00Page 540 1201-210, 1May 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-210,

 

 Subtask 36-12-00-865-057
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU AIR BLEED/X FEED/VALVE/BAT 2HV D13 49VU AIR BLEED/ENG 1/CTL 3HA1 D12 49VU AIR BLEED/ENG 1/MONG 2HA1 D11 121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41 122VU AIR BLEED/ENG 2/CTL 3HA2 Z23 122VU AIR BLEED/ENG 2/MONG 2HA2 Z22 122VU AIR BLEED/X FEED VALVE/NORM 1HV Z20
 Subtask 36-12-00-860-062
 C. Aircraft Maintenance Configuration
 (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).
 
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