Learjet 35 - Before Landing

2B-48 Developed for Training Purposes Leerjet 35/36
December 1998
CAE SimuFlite
Before Landing
Spoilers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACTED
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED 8° or 20°
Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
Engine Sync . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
If the engine sync is on and gear extended, the ENG SYNC
annunciator illuminates when nose gear is down and locked.
The ENG SYNC annunciator is wired through the downlock
switch.
Anti-Skid. . . . . . . . . . . . . . . . . . ON/LIGHTS EXTINGUISHED
Landing/Taxi Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Dee Howard Thrust Reversers
(below 200 KIAS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARMED
Cabin. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
Hydraulic Pressure . . . . . . . . . . . . . . . . . . . . . . . . CHECKED
Air Ignition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Autopilot. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISENGAGED
Yaw Damper . . . . . . . . . . . . . . . . . . . . . . . . . . . DISENGAGED
FC 200 autopilot: The yaw damper should be disengaged
in the landing flare.
FC 530 autopilot: With full flaps, the yaw damper disen-
gages through the squat switch relay at touchdown. With
flaps other than full down, disengage the yaw damper prior
to landing.