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Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais.

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Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais. Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais.
Description
  • Categoria Avião monomotor
  • Fabricante Cessna Aircraft
  • Modelo 206H Stationair TC
  • Ano 2010
  • Horas Totais 2.975
  • Assentos 6
  • Motor Lycoming TIO-540-AJ1A
  • Combustível Avgas
  • Condição Usado

Horas disponíveis de motor 1.125h.

Sem ar condicionado.

Equipamentos:
Garmin G1000
GDU-1040 Primary Flight Display (PFD)
GDU-1040 Multi-function Display (MFD)
GMA-1347 Digital Audio Panel with Marker Beacon/Intercom
CI-102 Marker Beacon Antenna
GIA-63 NAV/COM/GPS with Glideslope #1
GIA-63 NAV/COM/GPS with Glideslope #2
CI-2480 VHF/GPS Antenna with Internal Notch Filter (2)
CI-120 NAV Antenna
GTX-33 Transponder – Mode S with TIS
CI-105 Transponder Antenna
GEA-71 Engine/Airframe Computer
• CHT/EGT Sensors – All Cylinders
• Fuel Flow Meter
• Manifold/Tachometer/Vacuum Sensors
GRS-77 AHRS
GDC-74 Air Data Computer with OAT Probe
GMU-44 Magnetometer
KAP-140 Dual Axis Autopilot
• Altitude Preselect
• GPS Roll Steering
• KCM-100 Configuration Mode
• KS-270C Pitch Axis Servo Actuator
• KS-271C Roll Axis Servo Actuator
• KS-272C Pitch Trim Servo Actuator
GDL-69A XM Satellite Data / Radio Receiver
3000-11 Emergency Locator Transmitter
Emergency Locator Transmitter External Antenna
Emergency Locator Transmitter Remote Mounted Switch
WX-500 Stormscope
NY-163 Stormscope Antenna
Control Wheel Push-To-Talk Switch – Pilot/Copilot
Mic & Phone Jacks – Pilot/Copilot/Passengers
Auxiliary Stereo Input Jack
Blind Turn Coordinator for KAP-140
Avionics Circuit Breaker Panel
Single Engine Driven Vacuum Pump System
Backup Mechanical Instruments
• Attitude (Vacuum Gyro)
• Airspeed
• Altimeter
Magnetic Compass
Pitot System – Heated
Static System
Alternate Static Source
Audible Stall Warning System – Heated

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
PERFORMANCE
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
X (best angle of climb) 69 KIAS
Y (best rate of climb) 89 KIAS
A (design maneuvering) 125 KIAS
FE (max flap extended) 140 KIAS
NO (max structural cruising) 149 KIAS
NE (never exceed) 182 KIAS
R (rotation) 55 KIAS
S1 (stall, clean) 50 KIAS
SO (stall, in landing configuration) 39 KIAS
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