Section II
Limitations
BEECHCRAFT Bonanza
V35, V35A & V35B thru D-9947
CENTER OF GRAVITY LIMITS (Gear Down)
I
Loading calculations shall be checked before each flight to
ensure that the Weight and Center of Gravity remain within
the approved limits during flight.
Forward: 77.0 inches aft of datum to 2900 lbs with straight
line variation to 82. 1 inches at 3400 lbs.
Aft: 85.7 inches aft of datum to 3000 lbs with straight line
variation to 84.4 inches at 3400 lbs.
REFERENCE DATUM
Datum is 83.1 inches forward of center line through forward
jack points.
MAC leading edge is 66.7 inches aft of datum.
MAC length is 65.3 inches.
~PPROVED MANEUVERS (3400 POUNDS)
MANEUVER ENTRY SPEED (CAS)
Chandelle ....................... 132 kts/152 mph
Steep Turn ...................... 132 kts/152 mph
Lazy Eight ....................... 132 kts/152 mph
Stall (Except Whip) ........... Use slow deceleration
Minimum fuel for above maneuvers - 10 gallons each main
tank.
Spins are prohibited.
FLIGHT LOAD FACTORS (3400 POUNDS)
Positive Maneuvering Load Factors
Flaps Up ................................... 4.4G
Flaps Down ................................ 2.0G
MINIMUM FLIGHT CREW
One ( 1) Pilot
2-10
March, 1987
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