SOLOY TURBINE PAC SECTION 2
POHS CESSNA T206H/206H LIMITATIONS
2-4
F.A.A. Approved May 23, 2003
AIRSPEED INDICATOR MARKINGS
Airspeed indicator markings and their color code significance are
shown in Figure 2-2.
Full flap operating range. Lower limit is
maximum weight stalling speed in landing
configuration V
so
. The transition point from
narrow to wide arc is the stall speed with
wing flaps in up position. Upper limit is the
maximum speed permissible with flaps
extended.
Maximum speed for all operations.
Figure 2-2. Airspeed Indicator Markings
POWERPLANT LIMITATIONS
Engine Manufacturer: Soloy Corporation/Rolls Royce
Engine Model Number: Soloy Turbine Pac, 780-1000-1
Engine Horsepower Rating:
Takeoff Power, 5 Minutes: 418 SHP
Maximum Continuous: 368 SHP
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