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2009 Apollo Fox
| Overview | |||
| Listing Status: | Inactive | ||
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Awesome Almost New!! Apollo Ultralight Aircraft is a Hungarian aircraft manufacturer based in Eger. The company specializes in the design and manufacture of ultralight aircraft, gyroplanes, and ultralight trikes, in the form of kits for amateur construction and ready-to-fly aircraft. This aircraft its been hangered all its life. It also comes with parachutes. The Apollo Fox is built according to the "BCAR" Section S construction norm. The aircraft has welded steel alloy tube fuselage covered with "ceconite" fabric. The wings are made of aluminum alloy both spars and ribs and then covered with "ceconite". Wing can be folded backward. One pilot can do it within 10 minutes. The landing gear is aluminum plate sheet system, like on all Cessna. Wheels are equipped with hydraulic discs or mechanic drum brakes. Apollo Fox has very good rudder harmony and very easy to fly and land. |
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| Price: | N/A | ||
| Offered By: | USA Aircraft Brokers Inc. | ||
| Registration: | N158AP | ||
| S/N: | 00006 | ||
| Location: |
Venice Beach, Florida United States 
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| Airframe | |||
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Fiberglass and Fabric (Wings) Welded Fuselage Foldable Wings Autopilot |
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| Total Time: | 1,365 Hours | ||
| Avionics | |||
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The aircraft has traditional steam gauges and with glass panel. Standard pricing includes all-day VFR flight instruments and engine monitors. Apollo Fox meets the specific requirements of the ASTM design standard for night VFR flight. Thus with certain optional instruments, night VFR flight is allowed, opening the door for private pilots who’s like to use it for night VFR flight. |
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| Additional Equipment | |||
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Power: 65 - 100 Hp Max take off weight: 450 kg Weight/Hp relation: 5.625 kg/LE Empty weight: 265-285 kg Max payload: 180 kg Wingspan: 9,15 m Wing area: 11,4 m2 Lenght: 5,80 m Lenght with folded wings: 6,47 m Total width with folded wings: 2,39 m Height: 1.7 m Fuel capacity: 60 l Stall speed: 64km/h Maximal speed: 200 km/h Cruise speed: 150 km/h Take off lenght: 120 m Landing lenght: 200 m Range: 800 km Max G: +4; -2 Max cabin width: 1,1 m Empty weight: 604 lbs (274 kg) MTOW: 992 lbs (450 kg) Stall speed: 35 kts (40 mph) (65 kph) Cruise speed: 81 kts (93 mph) (150 kph) VNE: 97 kts (112 mph) (180 kph) Take-off distance: 459 ft (140 m) Landing distance: 656 ft (200 m) |
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| Engines & Props | |||
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Rotax 912ULS (100 HP) Serial 5651808 Slipper Clutch Heavy Duty Starter Propeller Sensenich 2A0R570E-2 |
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| Interior & Exterior | |||
| Tan / White | |||
| White / Red | |||
| Aircraft Documents | |||
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