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[ CESSNA 5Y-CAK ]
C150 (2) SEATER
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5Y-CAK
2 SEATER
Based in MALINDI AND WILSON
2 SEATER
Based in MALINDI AND WILSON
The Cessna 150 is a two-seat tricycle gear general aviation airplane that was designed for flight training, touring and personal use In 1977, it was succeeded in production by the Cessna 152, a minor modification to the original design.
The Cessna 150 is the fifth most produced aircraft ever, with 23,839 produced.[The Cessna 150 was offered for sale in named configurations that included the Standard basic model, the Trainer with dual controls, and the deluxe Commuter, along with special options for these known as Patroller options. Later, these configurations were joined by the top-end Commuter II and the aerobatic Aerobat models.
Fuel Capacity 26 gallons (98 L)
Max Gross Weight 1,500 lbs (680.38 kg)
Length 23 ft 11 in (7.29 m)
Height 8 ft 6 in (2.59 m)
Wingspan 33 ft (10.06 m)
Max Gross Weight 1,500 lbs (680.38 kg)
Length 23 ft 11 in (7.29 m)
Height 8 ft 6 in (2.59 m)
Wingspan 33 ft (10.06 m)
Blue and white markings
[ CESSNA 5Y-CCN]
C172N (4) SEATER
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5Y-CCN
4 SEATER
Based in WILSON AND MALINDI
4 SEATER
Based in WILSON AND MALINDI
The Cessna 172 Skyhawk is an American four-seat, single-engine, high wing, fixed-wing aircraft made by the Cessna Aircraft Company. First flown in 1955, more 172s have been built than any other aircraft. It was developed from the 1948 Cessna 170 but with tricycle landing gear rather than conventional landing gear. The Skyhawk name was originally used for a trim package, but was later applied to all standard-production 172 aircraft, while some upgraded versions were marketed as the Cutlass.
Measured by its longevity and popularity, the Cessna 172 is the most successful aircraft in history. Cessna delivered the first production model in 1956, and as of 2015, the company and its partners had built more than 44,000 units.] The aircraft remains in production today.
Cessna 172 Specifications.
Dimensions: Length: 27′ 2″ Height: 8′ 11″ Wingspan: 36′ 1″
Weights: Max. Ramp Weight: 2,558 lb.
Max Performance: Maximum Cruise Speed: 124 ktas.
Maximum Range: 640 nm. ...
Baggage Capacity: Weight: 120 lb.
Powerplant: Manufacturer: Lycoming. Model: 10-360-L2A.
Weights: Max. Ramp Weight: 2,558 lb.
Max Performance: Maximum Cruise Speed: 124 ktas.
Maximum Range: 640 nm. ...
Baggage Capacity: Weight: 120 lb.
Powerplant: Manufacturer: Lycoming. Model: 10-360-L2A.
Blue and white markings
[ PIPER 5Y-BIA ]
PA34 -200 (6) SEATER
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5Y-BIA
6 SEATER
Based in MALINDI AND WILSON
6 SEATER
Based in MALINDI AND WILSON
The Seneca was developed as a twin-engined version of the Piper Cherokee Six. The prototype was a Cherokee Six that had wing-mounted engines installed, retaining its nose engine. The prototype was flown as a tri-motor aircraft in the initial stages of the test-flying program.[
Exterior
Exterior Height: 9 ft 10 in
Wing Span: 38 ft 11 in
Length: 28 ft 7 in
Occupancy Crew: 1-2 Passengers: 6
Operating Weights Max T/O Weight: 4000 Lb Empty Weight: 3212 Lb
Performance Rate of Climb: 1360 fpm Max Speed: 170 kts Normal Cruise: 160 kts Economy Cruise: 144 kts
Power Plant Engines: 2 Engine Mfg: Lycoming Engine Model: IO-360-C1E6
Occupancy Crew: 1-2 Passengers: 6
Operating Weights Max T/O Weight: 4000 Lb Empty Weight: 3212 Lb
Performance Rate of Climb: 1360 fpm Max Speed: 170 kts Normal Cruise: 160 kts Economy Cruise: 144 kts
Power Plant Engines: 2 Engine Mfg: Lycoming Engine Model: IO-360-C1E6
White and Brown markings