Cessna 206H Model, Pod Installation Document Aerocet Form
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People also ask
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How many miles per gallon does a Cessna 206 get?
Cessna 206 Stationair Performance. Top cruise speeds will run in the 145-knot area while burning 17 gallons per hour or more. Throttling back to a leisurely 135 knots cuts gas consumption to a more reasonable 13 GPH. -
What is the climb rate of the Cessna 206?
Initial climb rate 1,050 fpm. Service Ceiling 27,000. Takeoff distance (50′) 1,740. -
What is the approach speed of a Cessna 206?
The 206 likes 90 to 100 knots in the VFR pattern. Just be ready for a bit of a pitch up when those flaps start to extend. In a typical VFR approach ending in full flaps, we planned to cross the threshold at 70 to 75 knots. -
How many miles per gallon does a Cessna 206 get?
Cessna 206 Stationair Performance. Top cruise speeds will run in the 145-knot area while burning 17 gallons per hour or more. Throttling back to a leisurely 135 knots cuts gas consumption to a more reasonable 13 GPH. -
What is the cruise speed of the Cessna 206h?
The CESSNA T206H, manufactured from 1998 - to present, requires a 1 person crew and can transport up to 5 passengers. The aircraft has a maximum operating altitude of 27,000', a normal cruise speed of 152 KTS/175 MPH, and a 698 NM/804 SM seats-full range. -
How much does a Cessna 206H cost per hour?
Based on 450 annual owner-operated hours and $6.75-per-gallon fuel cost, the CESSNA 206H has total variable costs of $101,250.00, total fixed costs of $85,170.00, and an annual budget of $186,420.00. This breaks down to $414.27 per hour. -
What is the cruise speed of a Cessna 206H Stationair?
SPEC SHEET Cessna T206H Stationair Standard equipped price: $400,500 Average equipped price: $463,150SpecificationsRate of climb, sea level1,050 fpmCruise speed/range w/45-min rsv, std fuel (fuel consumption) @ 75% power, 10,000 ft @ 68% power, 24,000 ft150 kt/530 nm (19.2 gph) 160 kt/600 nm (17.3 gph)39 more rows • Feb 1, 2006 -
How much does a Cessna 206 weight?
Original 206 model, six seats, powered by a Continental IO-520-A of 285 hp (213 kW), with a gross weight of 3,300 lb (1,497 kg) landplane, 3,500 lb (1,588 kg) seaplane and certified on 19 July 1963.
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