Learjet 35 - Parking; Before Landing

Leerjet 35/36 Developed for Training Purposes 2B-55
December 1998
Expanded Normal Procedures
Before Landing
Spoilers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACTED
Flaps . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED (8° OR 20°)
Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
Engine Sync . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Anti-Skid . . . . . . . . . . . . . . . . . . ON/LIGHTS EXTINGUISHED
Landing/Taxi Lights . . . . . . . . . . . . . . . . . . . . AS REQUIRED
Aeronca Thrust Reversers . . . . . . . . . . . . . . . . . . . . TESTED
Dee Howard Thrust Reversers
(below 200 KIAS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARMED
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
Hydraulic Pressure . . . . . . . . . . . . . . . . . . . . . . . . CHECKED
Yaw Damper (FC 200 autopilot) . . . . . . . . . . . DISENGAGED
Parking
Under normal weather conditions, the aircraft may be parked
and headed in a direction to facilitate servicing without regard
to prevailing winds. For extended parking, head aircraft into the
wind.
Aircraft . . . . . . . . . . . . . PARK ON HARD, LEVEL SURFACE
Nose Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CENTERED
Parking Brake. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
Main Gear Wheels . . . . . . . . . . . . . . . . . . . . . . . . . CHOCKED
Flaps and Spoilers . . . . . . . . . . . . . . . . . . . . . . . RETRACTED
Static Ground Cables . . . . . . . . . . . . . . . . . . . .CONNECTED
Protective Covers . . . . . . . . . . . . . . . . . . . . . . . . INSTALLED
Gust Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALLED
Tail Stand . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALLED
Cabin Door . . . . . . . . . . . . . . . . . . . . .CLOSED and LOCKED