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时间:2011-03-25 18:04来源:蓝天飞行翻译 作者:admin
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 LANDING GEAR ALTERNATE BRAKING SYSTEM (95GG) - REMOVAL/INSTALLATION
___________________________________________________________________ TASK 32-43-34-000-001 Removal of the Alternate Braking Control Unit (ABCU) (95GG)
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
 No specific circuit breaker(s) safety clip(s)
 No specific access platform 1.8 m (5 ft. 11 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001  Energize the Ground Service Network from the External Power 32-43-34-991-002 Fig. 401
 3. Job Set-up
__________ Subtask 32-43-34-861-050
 A. Energize the Ground Service Network (Ref. TASK 24-42-00-861-001)
 1EFF : 401-499, 1 32-43-34Page 401 1 1 Aug 01/05 1 1 1CES 1 Subtask 32-43-34-865-050


 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU ABCU &/Y BRK/PRESS IND 61GG C10 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY 4GG M36 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/CTL 3GG M35 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/CTL 1GG M34 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY 2GG M33 121VU ABCU/HOT BUS/SPLY 110GG P30
 Subtask 32-43-34-010-051
 C. Get Access to the Avionics Compartment
 (1)
 Put an access platform in position at the access door 822.

 (2)
 Open the access door 822.


 4. Procedure
_________ (Ref. Fig. 401/TASK 32-43-34-991-002) Subtask 32-43-34-020-050
 A. Removal of the ABCU
 (1)
 Disconnect the electrical connectors (1) and (2).

 (2)
 Put blanking caps on the disconnected electrical connectors.

 (3)
 Hold the ABCU (6) and loosen the screw (5), the washer (3) and the bonding braid (8).

 (4)
 Loosen the screws (4) and the washers (3).

 (5)
 Remove the ABCU (6) from its bracket (7).

 (6)
 Retain the parts for installation.


 1EFF : 401-499, 1 32-43-34Page 402 1 1 Aug 01/05 1 1 1CES 1


 Alternate Braking Control Unit (ABCU) (95GG)
 Figure 401/TASK 32-43-34-991-002

 1EFF : 401-499, 1 32-43-34Page 403 1 1 Aug 01/05 1 1 1CES 1 TASK 32-43-34-400-001


 Installation of the Alternate Braking Control Unit (ABCU) (95GG)
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.8 m (5 ft. 11 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 07-001 ELECTRICAL BONDING COATING (BLUE COLOR) (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
22-97-00-710-001 Operational Test of the LAND CAT III Capability 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 32-42-00-710-001 Operational Check of the Normal Braking System 32-46-00-740-001 BITE Test of the BSCU 32-46-00-740-003 BITE Test of the BSCU - LRU Identification 32-51-00-720-003 Functional Test of the Nose Wheel Steering with the
 Handwheel. 34-10-00-860-004 IR Alignment Procedure ESPM 205125 (for corrective action) 32-43-34-991-002 Fig. 401
 1EFF : 401-499, 1 32-43-34Page 404 1 1 Aug 01/05 1 1 1CES 1


 3. Job Set-up
__________ Subtask 32-43-34-860-050
 A. Aircraft Maintenance Configuration
 
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