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时间:2011-03-25 17:50来源:蓝天飞行翻译 作者:admin
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_______ GEAR.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice No specific access platform 2.0 m (6 ft. 7 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 08-048 D DA-2-657-4 ADHESIVE (Ref. 20-31-00) Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
 Material No. 15-008  AIB TN 10138 TYPE II GRADE 2 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
 Material No. 19-003  USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 1EFF : ALL 1 32-11-46Page 412 1 1 Aug 01/05R 1 1 1CES 1


 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-28-00-912-004 24-41-00-862-002  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-De-energize the Aircraft Electrical Circuits Supplied from the External Power
 32-00-00-481-001  Installation of the Safety Devices on the Landing Gears
 32-12-00-010-001 32-12-00-410-001  Open the Main Gear Doors for AccessClose the Main Gear Doors after Access
 32-42-00-710-001 32-42-00-720-002  Operational Check of the Normal Braking SystemFunctional test of the tachometers
 32-47-00-710-001 32-48-00-710-001 32-49-00-710-001 32-69-00-740-001  Operational Test of the Brake Temperature SystemFunctional Test of The Brake Cooling SystemOperational Test of the Tire Pressure Indicating System (TPIS)BITE Check Landing Gear Control Interface Unit (LGCIU) using MCDU to Ensure that Continuous BITE is Operative

 **ON A/C 001-049, 051-060, 101-101,
 32-11-46-991-001 Fig. 401


R **ON A/C 061-099, 102-149, 151-199, 201-299, 401-499,
 32-11-46-991-001-A Fig. 401A
 **ON A/C 301-399,
 32-11-46-991-001-B Fig. 401B

 1EFF : ALL 1 32-11-46Page 413 1 1 Aug 01/05 1 1 1CES 1 **ON A/C ALL


 3. Job Set-up
__________ Subtask 32-11-46-941-051-A
 A. Safety Precautions
 (1)
 Make sure that the safety barriers are in position.

 (2)
 Make sure that the ground safety locks are on the landing gear (Ref. TASK 32-00-00-481-001).

 (3)
 On the panel 400VU:

 -
make sure that the landing-gear control-lever 6GA is in the DOWN position

 -
make sure that the warning notice is in position to tell persons not to operate the landing gear.

 


 Subtask 32-11-46-860-050-A
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the access platform is below the applicable zone 730 or 740.

 (2)
 Make sure that the MLG door is open (Ref. TASK 32-12-00-010-001).

 (3)
 Make sure that the GROUND LOCK SLEEVE (460005835) is on the applicable MLG door actuator.


 Subtask 32-11-46-865-051
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 WARNING : OPEN CIRCUIT BREAKERS 1JH, 2JH1, 2JH2, 3JH1 AND 3JH2 (ENGINE 1
_______ AND 2 IGNITION SYSTEMS). THEN OPEN CIRCUIT BREAKERS 2KS1 AND 2KS2 (FADEC A AND EIU 1 AND 2) AND 4KS1 (FADEC B AND EIU 1). IF YOU DO NOT OBEY THIS SEQUENCE, THE ENGINE AUTOMATIC IGNITION- SYSTEM WILL OPERATE. THIS CAN CAUSE INJURY TO MAINTENANCE PERSONNEL.
 1EFF : ALL 1 32-11-46Page 414 1 1 Aug 01/05R 1 1 1CES 1


 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
 -------------------------------------------------------------------------------
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 49VU FUEL/XFR VALVE1/WING/R  2QP  A11
 49VU FUEL/XFR VALVE1/WING/L  1QP  A10 
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 
R
 49VU L/G/Y BRK/PRESS/IND  61GG  C10 

R  **ON A/C ALL 
R  49VU FUEL/X FEED/VALVE/MOT1  2QE  A12 
 
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