(b)
Remove the locking devices (31).
(c)
Remove the half shells (30).
R 1EFF : 151-199, 301-399, 401-499, 1 27-21-61Page 424 1 1 Aug 01/05 1 1 1CES 1
(2)
Removal of the cable guides on frame 70 (Refer to Detail H, section JJ).
(a)
Remove the clamp (26) and release the sleeve (27) from the cable guide.
(b)
Cut and remove the lockwire from the bolts (28).
(c)
Remove the bolts (28) and the washers (29). Release the flange
(24)
and remove the half shells (25).
(3)
Removal of the pulley cover (Refer to Detail M).
(a)
Remove the bolts (35), the washers (36) and the plate (37).
(b)
Remove the bolts (38) and the washers (39).
(c)
Remove the cover (42).
(4)
Removal of the cables from the cable quadrant.
(a)
Remove the two pins (40).
(b)
Remove the four pins (49) from the pulleys (50) and (51) (Refer to Detail R).
CAUTION : MONITOR THE END OF THE CABLE WHEN YOU PULL IT.
_______
(c)
Release the cables (21) and (22) from the cable quadrant (45). Pull them until they touch the frame 70.
(d)
On the frame 70, remove the sleeve (27) and the flanges (23) and
(24)
(Refer to Section JJ).
(e)
In zone 310, pull and remove the cables (21) and (22).
R 1EFF : 301-399, 1 27-21-61Page 425 1 1 May 01/05 1 1 1CES 1
**ON A/C ALL
TASK 27-21-61-400-001
Installation of the Rudder Control Cables
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.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific tensiometer No specific warning notices No specific access platform 1.6 m (5 ft. 3 in.) No specific access platform 2.8 m (9 ft. 2 in.) FE171901 1 TOOL - LOCKING 98A27901002000 1 PIN, RIGGING - RUDDER CONTROL 98D27207516000 1 RIGGING PIN SET 98D27207547000 1 PIN - RIGGING 98F27003500000 1 LOCKING TOOL-CABLE
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific Lockwire corrosion resistant steel dia 0.8 mm (0.03 in.)
Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
1EFF : ALL 1 27-21-61Page 426 1 1 May 01/05R 1 1 1CES 1
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
6 cotter-pins 27-21-01 12B-010
11 cotter-pin 27-21-01 13A-045
16 cotter-pins 27-21-01 12B-170
32 cable ties 27-21-04 04 -070
32 cable ties 27-21-04 04A-070
32 cable ties 27-21-04 05A-060
32 cable ties 27-21-04 05A-070
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power
25-54-12-400-001 Installation of the FWD Cargo Compartment Partition FR34
25-54-12-400-002 25-55-11-400-002 25-55-12-400-001 Installation of the Ceiling Panels in the FWD Cargo CompartmentInstallation of the Ceiling Panels in the AFT Cargo Compartment -FR47/FR59Installation of the AFT Cargo Compartment Partition FR65
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