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时间:2011-03-21 13:53来源:蓝天飞行翻译 作者:admin
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 (b)
 Remove the nut (17), the washer (18) and the bolt (20).

 (c)
 Move the rocker assembly (15) from between the sides of the regulator (8).

 (d)
 Remove and discard the cotter pins (28).

 (e)
 Remove the nuts (27) and the washers (26).

 (f)
 Remove the screw (24), the bolt (25), the spacers (23) and the rocker assembly (15).

 


 NOTE : Do not disassemble other items of the rocker assembly (15)
____ or remove the pulleys (21) unless a repair or a new installation is necessary.
 (5) Remove the regulator (8) as follows: NOTE : Do not remove the nuts (7) and the bushes (19) from the
____
 regulator (8) unless a repair or a new installation is
 necessary.

 (a)
 Remove the nuts (14), the washers (13) and the bolts (11).

 (b)
 Remove the regulator (8) and the shims (12) from the structure. NOTE : Identify the shims (12) for installation in the same


____
 positions.

 1EFF : ALL 1 27-41-42Page 408 1 1 May 01/04R 1 1 1CES 1


 TASK 27-41-42-400-001
 Installation of the Cable Tension Regulator
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS


 -COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
 CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.

 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 5.5 m (18 ft. 1 in.) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) R
 0U190360 1 PIN - RIGGING
 98D27403500000 1 PITCH TRIM CONTROL LOCKING
 98D27407532000 1 RIGGING PIN - THS MECHANICAL CONTROL

 

 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 04-004  USA MIL-PRF-23827 TYPE I
 SYNTH.ESTER BASED GREASE HIGH PRESSURE
 (Ref. 20-31-00)

 Material No. 05-005 USA MIL-C-16173 GRADE II
 CORROSION PREVENTIVE (Ref. 20-31-00)
 Material No. 08-029 USA MIL-R-46082 TYPE I
 ADHESIVE (Ref. 20-31-00)

 Material No. 09-013  USA MIL-PRF-81733 TYPE I CLASS A
 CORROSION INHIBITING BRUSH CONSISTENCY
 (Ref. 20-31-00)

 Material No. 16-003  F ASNB70720
 COATING (OBSOLETE USE 16-021) (Ref. 20-31-00)

 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
16 cotter pin 27-41-42 01 -220 28 cotter pins 27-41-42 01 -110
 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
20-24-11-100-001 Cleaning and Protection of the Cables 20-24-12-200-001 Check of the Control Cables 27-41-00-220-002 Check of the Correct Tension of the THS Mechanical
 Control Cables
 29-10-00-864-001 Depressurize the Green Hydraulic System
 29-10-00-864-002 Depressurize the Yellow Hydraulic System

R  53-22-12-000-001 Removal of the Cabin Floor Panels
R  53-22-12-400-001 Installation of the Cabin Floor Panels 53-32-12-000-002 Removal of the Cabin Floor Panels 53-32-12-400-002 Installation of the Cabin Floor Panels -------------------------------------------------------------------------------


REFERENCE DESIGNATION
 -------------------------------------------------------------------------------

R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
 27-41-42-991-002 Fig. 401
 **ON A/C 301-399,
 27-41-42-991-002-A Fig. 401A
 **ON A/C ALL
 27-41-42-991-001 Fig. 402
 
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