Cessna 206H - Page 9

SOLOY TURBINE PAC PERFORMANCE
POHS CESSNA T206H/206H SPECIFICATIONS
vii
F.A.A. Approved November 17, 2015
PERFORMANCE – SPECIFICATIONS
RATE OF CLIMB AT SEA LEVEL (3600 LBS)
MCP
1,447 FPM
APPROVED CEILING
20,000 FT.
TAKEOFF PERFORMANCE:
Ground Roll
Total Distance Over a 50’ Obstacle
570 FT.
1,063 FT.
LANDING PERFORMANCE:
Ground Roll
Total Distance Over a 50’ Obstacle
553 FT.
1,094 FT.
STALL SPEEDS (CAS):
Flaps Up, Power Off
58 KNOTS
Flaps Down, Power Off
52 KNOTS
MAXIMUM WEIGHT
3,617 LBS.
TAKEOFF WEIGHT
3,600 LBS.
STANDARD EMPTY WEIGHT
2,274 LBS.
MAXIMUM USEFUL LOAD
1,343 LBS.
BAGGAGE ALLOWANCE
180 LBS.
WING LOADING
20.7 PSF
POWER LOADING
8.61 LBS/SHP
FUEL CAPACITY: TOTAL
92 GAL.
OIL CAPACITY
9 U.S. QTS.
ENGINE: Soloy Turbine Pac
418 SHP @ 1810 RPM (5 Minute Takeoff
Rating)
321 SHP @ 1810 RPM (Maximum
Continuous Rating)
780-1000-1
PROPELLER: 3-Bladed, Auto-Feather, Full
Feathering, Constant Speed
95 IN. DIA.
UNCONTROLLED
COPY