3-14 Developed for Training Purposes Leerjet 35/36
February 1998
CAE SimuFlite
Maximum Allowable Landing Weight
Landing weight limited by most restrictive of following:
Q
maximum certified landing weight
Q
maximum landing weight for the runway and ambient
conditions as determined from the applicable Landing
Distance chart in AFM Section V
Q
maximum landing weight (approach climb or brake
energy limited) for altitude and temperature as deter-
mined from the applicable figure entitled Landing Weight
Limits in AFM Section V.
Zero Wing/Tip Fuel Weight
Maximum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .13,500 LBS
. . . . . . . . . . . . . . . . . . . . . . . . .(6,124 KG)
All weights in excess of 13,500 lbs must consist of wing and tip
tank, except as follows:
Q
Maximum zero wing and tip fuel weight may be increased
to 14,000 lbs by adding up to 500 lbs of additional fuse-
lage fuel.
Q
Additional fuselage fuel must be transferred prior to
reaching a total wing quantity of 2,250 lbs. In the event
the fuselage fuel cannot be transferred, V
MO must be
reduced to 325 KIAS.
To Next Page
Loading...
