Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 23

CESSNA
MODELT210M
SECTION 2
LIMITATIONS
PLACARDS
The following information is displayed in the form of composite or
individual placards.
1. In full view of the pilot: (The "DAY•NIGHT-VFR-IFR" entry,
shown on the example below, will vary as the airplane
is
equipped.)
This airplane must be operated as a normal category airplane in
compliance with the operating limitations as stated in the form of
placards, markings, and manuals.
- - - - - - - - MAXIMUMS - - - - - - - -
MANEUVERING SPEED (IAS)
GROSS WEIGHT . . . .
FLIGHT LOAD FACTOR Flaps Up
Flaps Down
. 119 knots
. 3800 lbs.
. +3.8, -1.52
. +2.0
No acrobatic maneuvers, including spins, approved. Altitude loss
in a stall recovery - 300 ft. Flight into known icing conditions
prohibited. This airplane is certified for the following flight
operations as of date of original airworthiness certificate.
DAY - NIGHT - VFR - IFR
2. On control lock:
CONTROL LOCK - REMOVE BEFORE STARTING ENGINE.
3. On fuel selector valve (at appropriate locations):
OFF.
LEFT ON - 44.5 GAL.
RIGHT ON - 44.5 GAL.
TAKEOFF AND LAND ON FULLER TANK.
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