Aeronaves

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Avião King Air C90 GT – Ano 2007 – 1450 H.T.

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  • 2 Tubes EFIS: Collins EFIS-84 Pro Line II
  • Garmin GPS-530 c/ Move map
  • COMMS: Dual Collins VHF-22C
  • COMPASS: Collins MCS-65
  • NAVS: Dual Collins VIR-32
  • DME: Collins DME-42
  • ADF: Collins ADF-60A
  • RMI: Collins RMI-30
  • F/DIR: Collins APS-65H IFCS
  • AP: Collins APS-65H
  • TPDR: Dual Collins TDR-94 Mode S
  • Radio Altimeter: Collins ALT-1000
  • Altimeter: IS&S encoding / Aerosonic counter-pointer encoding (millibar)
  • TAWS: Bendix King IHAS 8000
  • TCAS: Bendix King IHAS 8000
  • CVR: L3 FA2100
  • Radar: Honeywell RDR2100VP
  • Shadin ADC-2000 fuel/air data computer
  • Artex C406 ELT
  • 2 Motores Pratt & Whitney PT6A – 750 SHP Cada

Design Weights

Max. Ramp Weight .................................................................. 10,160 lb. (4,608 kg.)

Max. Takeoff Weight .............................................................. 10,100 lb. (4,581 kg.)

Max. Landing Weight ................................................................ 9,600 lb. (4,354 kg.)

Max. Zero Fuel Weight * .......................................................... 9,368 lb. (4,249 kg.)

Fuel Capacity.............................................................................. 2,573 lb. (1,167 kg.)

* No Flight Manual zero fuel weight. Zero fuel weight estimated for comparison purposes only. Calculated weight based on MTOW minus fuel required to fly 1.5 hours at HSC.

Weight Breakdown

Typically Equipped Basic Empty Weight ** .......................... 6,950 lb. (3,152 kg.)

1 pilot.............................................................................................. 200 lb. (91 kg.)

Typically Equipped Basic Operating Weight ....................... 7,150 lb. (3,243 kg.)

Max. Payload ***........................................................................ 1,934 lb. (877 kg.)

Useful Load ................................................................................ 3,010 lb. (1,365 kg.)

** Typically Equipped Basic Empty Weight includes standard interior, avionics, unusable fuel and oil *** As limited by Max. Landing Weight with NBAA IFR reserves (100 nm alternate)

 

Takeoff Field Length (Flaps Approach)

Max. TO Wt., SL, ISA .............................................................. 2,392 ft. (729 m)

Max. TO Wt., 5,000 ft. elevation, 25°C ................................. 3,372 ft. (1,028 m)

Accelerate-Stop Distance (Flaps Approach)

Max. TO Wt, SL, ISA .............................................................. 3,382 ft. (1,031 m)

Max. TO Wt, 5,000 ft. elevation, 25°C .................................. 4,411 ft. (1,344 m)

Landing Distance Max Landing Wt., SL, ISA ...................................................... 2,355 ft. (717 m)

VAPPROACH ...................................................................................... 101 kt.

Climb Performance (Max Takeoff Weight)

Time to Climb / Altitude ......................................... 17 min / FL 250

Climb Rate (Flaps Up) ........................................................... 1,953 fpm (595 m/min)

Climb Gradient (Flaps Up).................................................. 715 ft/ nm (118 m/km)

Engine-out Rate (Flaps Up) .................................................... 474 fpm (144 m/min)

Engine-out Gradient (Flaps Up) ........................................ 259 ft/nm (43 m/km)

Ceilings

Certified .................................................................................... 30,000 ft. (9,144 m)

All Engine Service ................................................................... 30,000 ft. (9,144 m)

Engine-out Service .................................................................. 19,170 ft. (5,843 m)

Cruise Performance

High Speed Cruise Speed ............................................................................ 270 kt/311 mph (500 km/hr)

Fuel Flow ................................................................................ 612 lb./hr. (278 kg./hr)

Altitude ......................................................................................... FL 200

Long Range Cruise Speed ............................................................................. 208 kt/239 mph (385 km/hr)

Fuel Flow ................................................................................. 332 lb/hr. (151 kg/hr)

Altitude ......................................................................................... FL 260

Inspeções

Totalmente revisado pela TAM Jundiaí, IAM, SBs e ADs cumpridos.

Horas voadas nos últimos 12 meses: 40 horas.

Preço: US$2,000,000.00
Categoria: Avião Turboélice
Fabricante: Beechcraft
Modelo: King Air C90 GT
Assentos: 7
Ano: 2007
Horas Totais: 1450
Combustível: Jet-A
Motorização: P&W PT6A-135A
Condição: Usado
Cor Externa: Pintura Branca com faixa azul e dourada
Cor Interna: Em couro cor bege
Ref: GP2637

A aeronave acima é de terceiro e como tal sujeita a venda prévia e/ou alteração sem aviso prévio. Dados fornecidos pelo proprietário, sujeitos a verificação.

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