Leerjet 35/36 Developed for Training Purposes 5-7
October 2001
Flight Planning
Maximum Allowable Landing Gross
Weight Determination
Charts in the Aircraft Flight Manual (AFM) Performance Section
facilitate determination of approach and landing climb perfor-
mance, landing field length requirements, and approach speed
values. The flow chart below illustrates the steps to determining
maximum allowable landing gross weight.
AIRPLANE CONDITIONS
AIRPORT CONDITIONS
ATMOSPHERIC CONDITIONS
LANDING DISTANCE
PERFORMANCE
SECTION 5
LANDING WEIGHT
LIMITS (APPROACH
CLIMB, BRAKE ENERGY)
PERFORMANCE
SECTION 5
MAXIMUM LANDING
WEIGHT (DESIGN
STRUCTURAL LIMIT)
LIMITATIONS
SECTION 1
COMPARE AND SELECT
LOWEST WEIGHT
FINISHED
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