Turbo Hélice Beechcraft King Air C90 GT ano 2007
Inspeções:
Totalmente revisado pela TAM Jundiaí, IAM, SBs e ADs cumpridos.
Horas voadas nos últimos 12 meses: 40 horas.
Configuração:
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
PREÇO: US$2,000,000.00
A aeronave acima é de terceiro e como tal sujeita a venda prévia e/ou alteração de preço. Dados fornecidos pelo proprietário, sujeitos a verificação.
