Learjet 35 - Crosswind Consideration; Landing

2B-84 Developed for Training Purposes Leerjet 35/36
December 1998
CAE SimuFlite
Landing
Slick Runway Landing Procedure:
Approach Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . V
REF
Touchdown. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .FIRM
Spoilers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXTEND
Nosewheel . . . . . . . . . . . . . . . . . . . . . . . . . ON THE RUNWAY
Brakes. . . . . . . . . . . . . . . . . . . APPLY REQUIRED BRAKING
Thrust Reversers . . . . . . . . . . . . . . . . . DEPLOY AND APPLY
Drag chute may be used in place of reversers.
The nosewheel on the runway improves directional control.
Spoilers should be deployed immediately after touchdown.
The anti-skid system automatically controls the brakes to
prevent skids and provides maximum braking for the runway
condition. Consider the use of the drag chute, if installed.
High reverse thrust can result in directional control difficul-
ties. Be prepared to reduce power to idle reverse if direc-
tional control is adversely affected. If snow or ice is present
while applying moderate to heavy braking, do not use nose-
wheel steering above 10 knots ground speed.
Crosswind Consideration
On a slick runway, directional control can become a problem in
crosswinds much lower than the maximum demonstrated. The
thrust reversers may be preferable to the drag chute. Nose-
wheel steering is more effective if forward control pressure is
applied; however, the brakes are more effective if the controls
are held more aft.