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时间:2011-03-27 12:52来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific warning notice No specific access platform 3 m (9 ft. 10 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-50-00-866-009 Retraction of the Flaps on the Ground 57-55-11-991-005 Fig. 407
 1EFF : ALL 1 57-55-11Page 438 1 1 May 01/04R 1 1 1CES 1


 3. Job Set-up
__________
 (Ref. Fig. 407/TASK 57-55-11-991-005) Subtask 57-55-11-941-059
 A. Safety Precautions
 (1) Put a warning notice in the cockpit to tell persons not to operate the flaps or slats.
 (2) Put the safety barriers in position. Subtask 57-55-11-860-060
 B. Aircraft Maintenance Configuration
 (1)
 Make sure that the flaps are fully retracted (Ref. TASK 27-50-00-866-009).

 (2)
 Install the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) on the slat/flap control-lever.

 (3)
 Put an access platform below the applicable flap track 3 or 4, zone 532 (632) or 533 (633).


 Subtask 57-55-11-865-069
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
 4. Procedure
_________ Subtask 57-55-11-010-050
 A. Lowering of the Flap Track Fairing
 (Ref. Fig. 407/TASK 57-55-11-991-005)

 (1)
 Remove the screws (2) and the top cover (1).

 (2)
 Remove the bolt (9), the washer (10) and disconnect the end of the bonding strap (8).


 1EFF : ALL 1 57-55-11Page 439 1 1 May 01/04R 1 1 1CES 1


 Flap-Track No. 3 & No. 4 Movable Fairing - Location and Detail
 Figure 407/TASK 57-55-11-991-005

 1EFF : ALL 1 57-55-11Page 440 1 1 May 01/04R 1 1 1CES 1


 (3)
 Remove and discard the cotter pin (6).

 (4)
 Disconnect the flap track fairing: WARNING : SUPPORT THE UNIT/ASSEMBLY OR IT WILL FALL AND BECOME


_______ DAMAGED OR INJURE PERSONNEL. THE UNIT/ASSEMBLY IS HEAVY.
 NOTE : The weight of the flap fairings is approximately 18kg (40lb).
____
 (a) Hold the movable fairing and remove the nut (3), the washer (4), the sliding bush (5) and the bolt (11).
 (5) Lower the flap track fairing: CAUTION : MOVE THE MOVABLE FAIRING SLOWLY. DO NOT LET THE MOVABLE
_______ FAIRING TURN TOO FAR VERTICALLY BECAUSE THIS WILL CAUSE DAMAGE.
 (a) Carefully lower the movable fairing until it is held by the applicable ground support equipment.
 1EFF : ALL 1 57-55-11Page 441 1 1 May 01/04R 1 1 1CES 1


 TASK 57-55-11-410-002
 To Lift the Flap Track No. 3 & No. 4 Movable Fairings after Access
 WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
 NOTICES ARE IN POSITION.

 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 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  warning notices
 No specific access platform 3.0 m (9 ft. 10 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 05-064 GB ABP1-4053 RELEASE AGENT (Ref. 20-31-00)
 Material No. 09-016  USA MIL-PRF-81733D TYPE II CLASS B
 CORROSION INHIBITING FILLET CONSISTENCY
 (Ref. 20-31-00)

 Material No. 09-018  USA AMS 3267/3
 CORROSION INHIBITING LOW ADHESION SEALANT
 (Ref. 20-31-00)

 Material No. 09-019  USA AMS 3267/3
 LOW ADHESION CORROSION INHIBITING SEALANT
 (Ref. 20-31-00)
 
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