(a)
Remove and discard the cotter pin (15).
(b)
Remove the nut (16) and the washer (17) from the screw (19).
(c)
Remove the screw (19).
(d)
Move the control rod (2) clear of the lever arm (4).
(e)
Safety the bush (18) in the lever arm (4) with lockwire 0.6 mm
(0.024 in.)
(3)
Disconnect the cable quadrant (1) from the aircraft structure.
(a)
Remove and discard the cotter pins (5).
(b)
Remove the nuts (6) and the washers (7) from the screws (8),(9).
(c)
Hold the cable quadrant (1) in position.
(d)
Remove the screws (8) from the top connection positions.
(e)
Remove the screws (9) from the bottom connection positions.
(f)
Remove the cable quadrant (1).
NOTE : Identify the screws (8) and the screws (9) for
____ installation in the same positions.
1EFF : ALL 1 27-21-46Page 411 1 1 May 01/04R 1 1 1CES 1
TASK 27-21-46-400-001
Installation of the Cable Quadrant
WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL MATERIALS
_______
ONLY WITH A GOOD SUPPLY OF AIR.
OBEY THE MANUFACTURERS INSTRUCTIONS.
PUT ON PROTECTIVE CLOTHING.
DO NOT GET THEM IN YOUR MOUTH.
DO NOT SMOKE.
DO NOT BREATHE THE GAS.
THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT.
GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
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 2.06 m (6 ft. 9 in.)
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) 98A27901002000 1 PIN, RIGGING - RUDDER CONTROL 98D27207547000 1 PIN - RIGGING 98D27207548000 1 PIN - RIGGING
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. 11-002 USA MIL-PRF-680
DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT)
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
-------------------------------------------------------------------------------
5 cotter pins 27-21-04 07 -060 15 cotter pin 27-21-04 21 -120
D. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 27-21-00-820-002 Adjustment of the Rudder Control-Cables Length 27-24-00-710-001 Operational Test of the Rudder Hydraulic Actuation 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action 51-75-13-916-002 Repair to a layer of Corrosion Preventive Compound 52-41-00-010-002 Open the Avionics Compartment Doors for Access 52-41-00-410-002 Close the Avionics Compartment Doors after Access 53-22-12-400-001 Installation of the Cabin Floor Panels 53-32-12-400-002 Installation of the Cabin Floor Panels
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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