Cessna T206H Stationair - Ano 2010 - 710 H.T.

Home | Aeronaves | Cessna T206H Stationair – Ano 2010 – 710 H.T.

Imprimir

Cessna T206H Stationair – Ano 2010 – 710 H.T.

Avião monomotor

REF:

AS5571

US$700,000.00

Status

Disponível

Fabricante

Cessna Aircraft

Modelo

T206H Stationair

Motor

Lycoming TIO-540-AJ1A

Combustível

Avgas

Ano

2010

Horas totais

710

Assentos

Condição

Usado

Localização

Brasil

Ano

2010

Horas totais

710

Assentos

Condição

Usado

Localização

Brasil

Galeria do PDF (Não visível na página normal)

Visão geral

Especificações

Visão geral

Especificações

PERFORMANCE
Powerplant	Lycoming TIO-540-AJ1A, 310 hp @ 2,500 rpm
Recommended TBO	2,000 hr
Propeller	McCauley 3-blade, constant-speed, 79-in dia
Length	28 ft 3 in
Height	9 ft 3 in
Wingspan	36 ft
Wing area	174 sq ft
Wing loading	20.7 lb/sq ft
Power loading	11.6 lb/hp
Seats	6
Cabin length	12 ft 1 in
Cabin width	3 ft 8 in
Cabin height	4 ft 2 in
Empty weight	2,274 lb
Empty weight, as tested	2,355 lb
Maximum ramp weight	3,617 lb
Maximum gross weight	3,600 lb
Useful load	1,343 lb
Useful load, as tested	1,262 lb
Payload w/full fuel	815 lb
Payload w/full fuel, as tested	734 lb
Maximum takeoff weight	3,600 lb
Maximum landing weight	3,600 lb
Fuel capacity, std	92 gal (88 gal usable) 552 lb (528 lb usable)
Oil capacity	11 qt
Baggage capacity	180 lb
Takeoff distance, ground roll	910 ft
Takeoff distance over 50-ft obstacle	1,740 ft
Max demonstrated crosswind component	20 kt
Rate of climb, sea level	1,050 fpm
Maximum level speed, 17,000 ft	178 kt
Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption)
@ 75% power, best economy 20,000 ft	164 kt/3.5 hr (114 pph/19 gph)
@ 65% power, best economy 24,000 ft	153 kt/4.1 hr (97 pph/16.2 gph)
@ 55% power, best economy 24,000 ft	137 kt/4.9 hr (85 pph/14.1 gph)
Service ceiling	27,000 ft
Landing distance over 50-ft obstacle	1,395 ft
Landing distance, ground roll	735 ft
LIMITING AND RECOMMENDED AIRSPEEDS
V _X (best angle of climb)	69 KIAS
V _Y (best rate of climb)	89 KIAS
V _A (design maneuvering)	125 KIAS
V _FE (max flap extended)	140 KIAS
V _NO (max structural cruising)	149 KIAS
V _NE (never exceed)	182 KIAS
V _R (rotation)	55 KIAS
V _S1 (stall, clean)	50 KIAS
V _SO (stall, in landing configuration)	39 KIAS

Visão geral

Descrição

Em excelente condição
Piloto + 5 passageiros

Avionicos

Garmin G1000 IFR Noturno completo
Tela PFD Garmin 10” (Primary Flight Display)
Tela MFD Gramin 10” (Multi-Function Display)
SVT (Visão Sintética do Terreno)
Painel de Áudio Garmin GMA-1347
Transponder Garmin GTX-33ES
Duplo GIA-63W NAV/COM/GPS/WAAS
GEA-71 Monitoramemto de motor e combustível
GDC-74A ADC (Air Data Computer)
Stormscope WX500
TAS 600 Informação de proximidade de trafego
TAWS Informação de proximidade de terreno
Piloto Automático Garmin GFC700
Sistema de Oxigênio
Ar Condicionado
GRS-77 AHRS (Attitude & Heading Reference
System)
Cartas Eletrônicas de Aproximação IFR
(assinatura Requerida)

Célula, Motor e Hélice

Horas Totais de Célula: 710
Horas Motor: 710
Hélice: 710

Exterior e Interior

Exterior: Branco e Cinza
Interior: Couro Claro

A aeronave acima é de terceiros, os dados estão sujeitos a verificação.

Especificações

PERFORMANCE
Powerplant	Lycoming TIO-540-AJ1A, 310 hp @ 2,500 rpm
Recommended TBO	2,000 hr
Propeller	McCauley 3-blade, constant-speed, 79-in dia
Length	28 ft 3 in
Height	9 ft 3 in
Wingspan	36 ft
Wing area	174 sq ft
Wing loading	20.7 lb/sq ft
Power loading	11.6 lb/hp
Seats	6
Cabin length	12 ft 1 in
Cabin width	3 ft 8 in
Cabin height	4 ft 2 in
Empty weight	2,274 lb
Empty weight, as tested	2,355 lb
Maximum ramp weight	3,617 lb
Maximum gross weight	3,600 lb
Useful load	1,343 lb
Useful load, as tested	1,262 lb
Payload w/full fuel	815 lb
Payload w/full fuel, as tested	734 lb
Maximum takeoff weight	3,600 lb
Maximum landing weight	3,600 lb
Fuel capacity, std	92 gal (88 gal usable) 552 lb (528 lb usable)
Oil capacity	11 qt
Baggage capacity	180 lb
Takeoff distance, ground roll	910 ft
Takeoff distance over 50-ft obstacle	1,740 ft
Max demonstrated crosswind component	20 kt
Rate of climb, sea level	1,050 fpm
Maximum level speed, 17,000 ft	178 kt
Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption)
@ 75% power, best economy 20,000 ft	164 kt/3.5 hr (114 pph/19 gph)
@ 65% power, best economy 24,000 ft	153 kt/4.1 hr (97 pph/16.2 gph)
@ 55% power, best economy 24,000 ft	137 kt/4.9 hr (85 pph/14.1 gph)
Service ceiling	27,000 ft
Landing distance over 50-ft obstacle	1,395 ft
Landing distance, ground roll	735 ft
LIMITING AND RECOMMENDED AIRSPEEDS
V _X (best angle of climb)	69 KIAS
V _Y (best rate of climb)	89 KIAS
V _A (design maneuvering)	125 KIAS
V _FE (max flap extended)	140 KIAS
V _NO (max structural cruising)	149 KIAS
V _NE (never exceed)	182 KIAS
V _R (rotation)	55 KIAS
V _S1 (stall, clean)	50 KIAS
V _SO (stall, in landing configuration)	39 KIAS