Leerjet 35/36 Developed for Training Purposes 2B-35
December 1998
Expanded Normal Procedures
L Fuel Computer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
L FUEL CMPTR annunciator extinguishes and engine RPM
stabilizes.
Right Thrust Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
The right fuel control governor check is the same as the left.
Anti-Skid . . . . . . . . . . . . . . . . . . ON/LIGHTS EXTINGUISHED
Spoileron/Spoilers . . . . . . . . . . . . . . . . . . . . . CHECKED/RET
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DN
Aileron Augmentation Check:
Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CENTER
Spoileron Reset Switch. . . . . . . . . . . . . . . . HOLD IN RESET
Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . ROTATE LEFT
Apply left aileron until AUG AIL annunciator illuminates, then
hold the control wheel stationary. Observe the deflection
angle.
Spoileron Reset Switch. . . . . . . . . . . . . . . . . . . . . .RELEASE
Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CENTER
Spoileron Reset Switch. . . . . . . . . . . . . . . . HOLD IN RESET
Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . ROTATE RIGHT
Apply right aileron until AUG AIL annunciator illuminates,
then hold the control wheel stationary. Observe the deflec-
tion angle; it should be approximately the same angle as the
left.
Spoileron Reset Switch. . . . . . . . . . . RESET AND RELEASE
Control Wheel . . . . . . . . . . . . . . .ROTATE LEFT AND RIGHT
The controls should be rotated full deflection left and right;
the AUG AIL annunciator should not illuminate.
Spoiler Check:
Spoilers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .EXTEND