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Cessna T206H Stationair TC – Ano 2010 – 2.975 Horas Totais.
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Ano
Horas totais
Assentos
Condição
Localização
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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 | |
| 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 |
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 | |
| 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 |
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