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CESSNA AIRCRAFT COMPANY FOR TRAINING USE ONLY MODEL 152 MAXIMUM CERTIFICATED WEIGHTS Takeoff: 1670 lbs. Landing: 1670 lbs. Weight in Baggage Compartment: Baggage Area 1 (or passenger on child’s seat) – Station 50 to 76: 120 lbs.
Soft or rough field takeoffs are performed with the maximum flap setting permitted for takeoff, for the Cessna 152 this is 10 degrees. The aircraft should be lifted off the ground as soon as practical in a slightly tail-low attitude to reduce the large frictional drag caused by the runway surface. Page 82: Crosswind Takeoff
is the horizontal distance from the reference datum to the center of gravity (C.G.) of an item. Moment Moment is the product of the weight of an item multiplied by its arm. (Moment divided by the constant 1000 is used in this handbook to simplify balance calculations by reducing the number of digits.) Center of Gravity (C.G.) Center of Gravity
CESSNA SECTION 4 MODEL 152 NORMAL PROCEDURES TAKEOFF POWER CHECK It is important to check full-throttle engine operation early in the takeoff run. Any sign of rough engine operation or sluggish engine acceleration is good cause for discontinuing the takeoff.
Distance de décollage et atterrissage Masse et centrage Vérifier si dans les limite de l’enveloppe. Poids max : 1670 Temps Vents Alt. Pression Décollage Atterrissage roulage roulage Obstacle (50’) Obstacle (50’) Poids Levier Moment Aéronef à vide Pilote et passager 39.11 Bagage 1 63.82 Bagage 2 84.00
MODEL 152 RANGE PROFILE 45 MINUTES RESERVE SECTION 5 PERFORMANCE 24.5 GALLONS USABLE FUEL CONDITIONS: 1670 Pounds Recommended Lean Mixture for Cruise Standard Temperature Zero Wind NOTES. 1. This chart allows for the fuel used for engine start, taxi, takeoff and climb, and the distance during climb. 2.
The following figures are based on the pilot's operating handbook and it is the pilot's responsibility to verify the information before use. Indicated airspeeds in knots are based on the maximum takeoff/landing weight of 1670 lbs and may be used for any lower weight.
