operating at a throttle position corresponding to ap-
proximately 18 to 20 inches or less of manifold pressure
depending on setting.
2. Landing Gear Retraction - With the landing gear safety
system switch in the ON position, the landing gear will
not retract unless: (1) the landing gear position switch is
in the UP position (2) the airspeed is above approxi-
mately 78 kts/90 mph IAS and (3) the engine is operating
at a throttle position corresponding to approximately 18
to 20 inches or more of manifold pressure depending on
setting.
NOTE
If landing gear retraction is desired before the
indicated airspeed reaches approximately 78
kts/90 mph, the landing gear safety system must
be inactivated by placing the switch in the OFF
position, preferably before placing the landing
gear position switch in the UP position.
PERFORMANCE
No change
Approved:
FAA Approved
Revised: April 1981
P/N 35-590110-13
W. H. Schultz
Beech Aircraft Corporation
DOA CE-2
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