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Adjustment Completion - BOMBARDIER Chalenger 604 Supplemental Maintenance Manual

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(1)
Set cable assembly swivel fittings to provide equal adjustment forward and aft, and tighten
jam nuts.
(2)
Release aft and forward most clamps on forward fuel control cable assembly.
(3)
Ensure fuel control lever on the engine is in the idle position (15
supplied in the Power Plant Rigging Kit, GSE 71-00-32.
(4)
Set throttle levers at idle, against the stops.
(5)
Install vendor-supplied rig pin to position ATS clutch and bell crank in the idle position
(6)
Connect upper end of control rod to throttle lever using existing hardware.
(7)
Remove the rig pin and exercise throttle lever through full travel to ensure smooth operation,
and verify that the control rod does not foul on any structure. Position throttle lever in the idle
position against the stop. Reinstall rig pin.
(8)
Check witness hole on clevis end of forward fuel control cable assembly. Approximately 1/2
inch of thread should be exposed.
(9)
Align clevis hole on cable end with bell crank outer arm using clevis pin. When alignment is
complete, install clevis pin, and secure with circular clip and cotter pin. Tighten clamps on
fuel control cable. Remove rig pin.
(10) Repeat steps 3.B.(1) through 3.B.(9) for the other fuel control cable.
(11) Ensure that all jam nuts, rod ends, and clevis bolts are secured with lockwire or cotter pins.
F.
Throttle Lever Split Adjustment
(1)
Check throttle lever split. Throttle lever split is to be less than 1/8" per CL-604 AMM.
(2)
Release aft and forwardmost clamps on the forward cable assembly.
(3)
To retard a throttle lever, adjust cable housing at the swivel fitting aft.
(4)
To advance a throttle lever, adjust cable housing at the swivel fitting forward.
(5)
Verify throttle cushion for max power, idle, and shut-off.
(6)
Tighten jam nuts and secure with lockwire.
(7)
Tighten aft and forwardmost clamps on the forward cable assembly.
2.
A
C
DJUSTMENT
OMPLETION
A.
Remove all equipment used for maintenance.
B.
Perform test per section 6.
C.
Return the aircraft to its initial condition.
EFFECTIVITY: TE-22305001-SMM-2
CL-604 SUPPLEMENTAL MAINTENANCE MANUAL
Prepared by DAS-605786-NM
o
o
- 18
) using the protractor
22-30-00
(Figure
402).
Page 502
Dec 3/03

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