Selkirk College IATPL Program Manual
Beech 95 POH Effective September 1, 2005 Appendix 14 - 20
Maneuver Limits
This is a normal category airplane. Acrobatic maneuvers, including spins, prohibited.
Flight Load Factor Limits
At design gross weight:
Positive 4.4g; negative 3.0g (flaps up)
Positive 2.0g); negative 0.0g (flaps down)
Gust limits: positive 4.32g; negative 2.32g (flaps up)
Kinds of Operation Limits
These airplanes are equipped for day and night VFR and IFR operations. CAR 605.18
specifies the equipment that must be installed and serviceable for IFR operation.
Flight into known icing conditions is prohibited.
Fuel Limitations
Each airplane has four fuel tanks – two main tanks and two auxiliary fuel tanks. There is
one main tank and one auxiliary tank in each wing.
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