Learjet 35 - Avionics and Communications; Systems Limitations

Leerjet 35/36 Developed for Training Purposes 3-23
February 1998
Limitations
Systems Limitations
Avionics and Communications
J.E.T. FC-200 Flight Control System
(Autopilot/Flight Director)
Maximum operating speed is V
MO/MMO.
When using autopilot, pilot or copilot must be in respective seat
with seat belts fastened.
Autopilot pitch and roll axis must not be used for takeoff or
landing.
Do not extend spoilers with autopilot engaged.
If heavy precipitation or severe turbulence is encountered, dis-
engage SPD, V/S, ALT, and G/S modes and engage yaw
damper, LVL and SOFT modes.
Autopilot may not be used unless the pitch and roll monitors
are checked and operational.
If, upon retraction of flaps after takeoff, APPR light stays on or
illuminates in the clean configuration, do not use the roll or
pitch modes. In maneuvers that involve the flaps beyond 13°
(ILS), the complete autopilot may be used.
J.E.T. FC-530 Autopilot/Flight Director
Maximum operating speed is V
MO/MMO.
Autopilot/flight director system approved for Category I ILS
approaches.
When using autopilot, pilot or copilot must be in respective seat
with seat belts fastened.