3-54 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Enroute
Flight Load Acceleration Limits:
Flaps Up . . . . . . . . . . . . . . . . . . . . . . . . . . . . +3.00 TO -1.0 G
Flaps Down. . . . . . . . . . . . . . . . . . . . . . . . . . .+2.00 TO 0.0 G
These acceleration values limit the bank angle in a coordinated
turn to 70°, flaps up; and 60°, flaps down. In addition, pullups
and pushovers must be limited to these values.
Systems Limitations
Avionics and Communication
The autopilot must not be engaged below 1,000 ft above the
terrain enroute and not below 190 ft above runway threshold
elevation when coupled to the ILS glideslope.
Electrical System
Whenever an engine start using a starter has been performed,
accomplish the Battery Charging bus current limiter and starter
disengagement checks as outlined in Starting Engines, Starter
Assist Airstarts, and/or Before Takeoff procedures in AFM Sec-
tions II and III. These checks require that both engines be oper-
ating to perform the check.
To Next Page
Loading...
