Leerjet 35/36 Developed for Training Purposes 3-13
February 1998
Limitations
Maximum Allowable Takeoff Weight
Takeoff weight limited by most restrictive of following:
Q
maximum certified takeoff weight
Q
maximum takeoff weight (climb or brake energy limited)
for altitude and temperature as determined from the
applicable figure entitled Takeoff Weight Limits in AFM
Section V
Q
maximum takeoff weight for the runway and ambient con-
ditions as determined from the applicable figure entitled
Takeoff Distance in AFM Section V
Q
maximum takeoff weight for obstacle clearance as deter-
mined from the applicable Takeoff Flight Path and Climb
Gradient figures in AFM Section V (FAR 121 and 135 as
applicable to U.S. registered aircraft).
Maximum Certified Landing Weight
Perform Hard or Overweight Landing Inspection (Chapter 5, Main-
tenance
Manual) if maximum certified landing weight is exceeded.
WEIGHT LBS UNITS
14,300
35-002 to 355 without AAK 80-3;
36-002 to 046 without AAK 80-3
15,300
35-002 to 355 with AAK 80-3; 35-356 and
subsequent; 36-002 to 046 with AAK 80-3;
36-047 and subsequent
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