Leerjet 35/36 Developed for Training Purposes 2B-49
February 2004
Expanded Normal Procedures
Landing
After touchdown:
Spoilers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXTENDED
Brakes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
Thrust Reversers or Drag Chute . . . . . . . . . . . AS DESIRED
Below 45 kts:
Nosewheel Steering. . . . . . . . . . . . . . . . . . . . AS REQUIRED
Go-Around/Missed Approach
Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISENGAGED
Thrust Levers . . . . . . . . . . . T.O. POWER OR AS REQUIRED
SPOILER Switch . . . . . . . . . . . . . . . . . . . . . . . . RETRACTED
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20°
Landing Gear Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
Climb. . . . . . . . . . . . . . . . . . . . . . APPROACH CLIMB SPEED
When clear of obstacles:
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . V
REF + 30
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
WARNING: When the Fuel Quantity gage indicates 600
pounds or less remaining in either wing tank, prolonged
nose-up attitude of 10° or more may cause fuel to be
trapped in the aft area of the wing tank outboard of the
wheel well. Fuel starvation and engine flameout may occur.
For go-around conditions with low fuel, on first steady indi-
cation by the LOW FUEL warning light, reduce climb atti-
tude and thrust to minimum required.