RAYTHEON PREMIER 1
(1) Ensure that the nose gear strut and the main gear struts are not flat prior to towing the airplane. Refer
to LANDING GEAR SERVICING procedures to service the struts (Ref. 12-10-25. 301).
(2) Visually check the nose and main gear tires for proper serviceability and condition. Refer to
LANDING GEAR SERVICING procedures to service the tires (Ref. 12-10-25_301).
CAUTION: The torque link must be in the fully collapsed position before towing. Damage to the nose landing
gear door and torque link could occur if the link is not fully collapsed.
(3) Remove the safety clip
(6)
and quick release pin
(7)
and disconnect the lower end of the torque link
(5)
from the nose gear fork
(8)
. Rotate the torque link
(5)
and align it with the tabs on the upper torque
link. Reinstall the quick release pin
(7)
and safety clip
(6)
securing the torque link
(5)
.
(4) Attach the tow bar
(3)
(015 or 016. Table 201) to the nose wheel axle
(1)
and install the lock pin
(2)
.
(5) Assign a ground crew member to operate the airplane brakes as required.
(6) Station an observer at each wing tip and at the tail, if required, when backing the airplane or in
congested areas near buildings or other airplanes.
(7) Close the passenger door and secure other open doors or panels.
(8) Remove all wheel chocks and disconnect the static ground wire.
(9) Verify the parking brake is released by depressing the button on the end of the parking brake handle
and place the handle in the stowed position.
Summary of Contents for PREMIER 1
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