Learjet 35A - Maximum Allowable Takeoff Weight; Maximum Certified Landing Weight

11 .... 1 ••••••
WEIGHT AND C.G. UNITS (CONT)
MAXIMUM AU.OWABLE TAKEOFF WEIGHT
The takeoff weight is limited by the most restrictive of the following re:-
quirements:
• Maximum Certified Takeoff Weight.
• Maximum Takeoff Weight (Climb or Brake Energy limited) for
altitude
and temperature as determined from the applicable figure
entitled
TAKEOFF WEIGHT UMITS in Section V.
• Maximum Takeoff Weight for the runway and ambient conditions
as determined from the applicable figure entitled
TAKEOFF
DlST ANCE in Section V.
• Maximum Takeoff Weight for obstacle clearance as determined from
the applicable
TAKEOFF FUGHT PATH and CUMB GRADIENT
figures in Section V. (FAR 121 and 135 as applicable to U.S. registered
aircraft.)
MAXIMUM CERTIFIED lANDING WEIGHT
MODEL 35A:
• Serials 35-067 thru 35-344 not incorporating
AAKBO-3 .............................. .
• Serials 35-067 thru 35-344 when incorporating
AAKBO-3 .......................... .... .
• Se~als 35-345 and subsequen~ .............. .
MODEL 36A:'
•
Serials 36-018 thru 36-045 not incorporating
AAKBO-3 .............................. .
• Serials 36-018 thru 36-045 when incorporating
AAKBO-3 .............................. .
• Serials 36-046 and subsequent .............. .
14,300 Pounds
6,486 kg
15,300 Pounds
6,940 kg
15,300·Pounds
6,940 kg
14,300 Pounds
6,486 kg
15,300 Pounds
6,940 kg
15,300 Pounds
6,940 kg
1-4
FAA APPROVED 4-30-76
REISSUED 2-25-81, CHANGE 6