Learjet 35 - Maximum Allowable Landing Weight

5-8 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Maximum Allowable Landing Weight
Landing Weight Limitation: The maximum allowable
landing weight is limited by the most restrictive of the fol-
lowing:

Structure

Landing weight limit (approach climb, brake energy)

Landing distance.
LANDING DISTANCE
EFFECTIVE RUNWAY LENGTH
THRESHOLD
APPROACH—CLIMB
(ENGINE—OUT
2.1% MIN GRADIENT)
50’
V
REF
= 1.3 V
SO