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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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 -COMPONENTS THAT MOVE. WARNING : WEAR AND ATTACH A SAFETY HARNESS WHEN YOU WORK ON HIGH SECTIONS. A
_______
 FALL CAN INJURE OR KILL YOU.

 WARNING : DO NOT GET THE COMPOUND ON YOUR SKIN.
_______
 IF YOU DO:

 -RUB IT OFF IMMEDIATELY WITH A CLEAN CLOTH
 -WASH THE SKIN WITH SOAP AND RINSE WITH CLEAN WATER.
 CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF

_______
 CARBONFIBER REINFORCED PLASTIC.

 NOTE : The installation of the servo control unit 34CE1 is shown. The
____ installation of the servo control units 34CE2, 34CE3 and 34CE4 are the same. For the correct location of the servo control units compare the identification placards.
 1.
 Reason for the Job

__________________
 Self Explanatory


 2.
 Job Set-up Information

 


______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific  Torque Wrench : range 1.00 to 10.00 m.daN
 (8.00 to 75.00 lbf.ft) SL90-313-5625 1 TOOL - INSTALLATION, TAB WASHERS STA-LOK NSA5454 SL90-313-6250 1 TOOL- INSTALLATION, TAB WASHERS STA-LOK NSA5454 SL90-315-5625 1 WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 SL90-374-6250 1 WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 98D27309003000 1 DEVICE-LOCKING, ELEVATOR

R  98D27309009000 2 COLLAR-ELEVATOR SERVO CONTROL SAFETY 98D27903500000 2 PIN-SIDE STICK LOCKING
 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. 05-002  USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00)
 Material No. 05-005  USA MIL-C-16173 GRADE II
 CORROSION PREVENTIVE (Ref. 20-31-00)

 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION  |IPC-CSN
 -------------------------------------------------------------------------------
20 cotter pin 27-34-07 11 -030 24 cotter pin 27-34-07 11 -020A 25 cotter pin 27-34-07 11 -020A 38 cotter pin 27-34-07 12C-020 D. Referenced Information


 -------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------- -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
20-22-00-400-001  Installation of STA-LOK Nuts and Lockwashers
 20-28-00-912-004 27-34-00-820-001 27-34-00-820-002 27-34-00-820-003 29-10-00-864-001 29-10-00-864-002 29-10-00-864-003 55-13-11-000-001 55-13-11-400-001 27-34-51-991-001  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)-Adjustment of the Elevator and Hydraulic Actuation (with the reference triangle on the tail cone)Adjustment of the Elevator and Hydraulic Actuation after Removal/Installation of one ServocontrolAdjustment of the Elevator and Hydraulic Actuation to 0.5 Degrees Nose-Up with the Gauge-Elevator Neutral Setting (98D27309006000)Depressurize the Green Hydraulic SystemDepressurize the Yellow Hydraulic SystemDepressurize the Blue Hydraulic SystemRemoval of the THS Trailing Edge Access PanelsInstallation of the THS Trailing Edge Access PanelsFig. 401

 **ON A/C 001-003, 052-054,
R  27-34-51-991-010 Fig. 402 **ON A/C 004-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 27-34-51-991-010-A **ON A/C 051-051, Fig. 402A
R  27-34-51-991-010-B Fig. 402B **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 27-34-51-991-011  Fig. 403

 


R **ON A/C 051-051,
R 27-34-51-991-011-A Fig. 403A R **ON A/C ALL
 3. Job Set-up
__________
 Subtask 27-34-51-860-063

 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the hydraulic systems are depressurized (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-10-00-864-002), (Ref. TASK 29-10-00-864-003).

 (2)
 Make sure that the PIN-SIDE STICK LOCKING (98D27903500000) is in the CAPT and F/O side stick controllers.
 
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