OUR FLEET
Beirut Wings operates one of the largest and the most modern fleets of any Flight Training Organization in Lebanon. Here is the list of our aircrafts:
Tecnam P2006T Multi Engine AC – G950
Tecnam P2010 Single Engine G1000
The Cessna 152:
American two-seat, fixed tricycle gear, general aviation airplane, used primarily for flight training and personal use.
General characteristics
- Crew: 1 pilot
- Capacity: 1 passenger
- Length: 24 ft 1 in (7.3 m)
- Wingspan: 33 ft 4 in (10.2 m)
- Height: 8 ft 6 in (2.6 m)
- Wing area: 160 ft² (14.9 m²)
- Empty weight: 1,081 lb (490 kg)
- Max. takeoff weight: 1,670 lb (757 kg)
- Powerplant: 1 × Lycoming O-235-L2C flat-4 engine, 110 hp (82 kW) driving a 69-inch (175 cm), two-blade, fixed-pitch McCauley propeller or a 72-inch, two-blade, fixed-pitch Sensenich propeller
Performance
- Maximum speed: 126 mph (110 knots, 204 km/h)
- Cruise speed: 123 mph (107 knots, 198 km/h)
- Stall speed: 49 mph (43 knots, 79 km/h) unpowered, flaps down
- Takeoff roll: 725 ft (221 m)
- Range: 477 mi (414 nm, 768 km)
- Extended range:795 mi (690 nm, 1,280 km) with long-range tanks
- Service ceiling: 14,700 ft (4,480 m)
- Rate of climb: 715 ft/min (3.6 m/s)
- Max. wing loading: 10.44 lb/ft² (51 kg/m²)
- Minimum power/mass: .066 hp/lb (108 W/kg)
The Cessna 172 Skyhawk:
four-seat, single-engine, high-wing fixed-wing aircraft made by the Cessna Aircraft Company. First flown in 1955 and once again in production, more Cessna 172s have been built than any other aircraft. This model is marketed under the name Skyhawk SP, although the Type Certification data sheet specifies it is a 172S.
General characteristics
- Crew: one
- Capacity: three passengers
- Length: 27 ft 2 in (8.28 m)
- Wingspan: 36 ft 1 in (11.00 m)
- Height: 8 ft 11 in (2.72 m)
- Wing area: 174 sq ft (16.2 m2)
- Aspect ratio: 7.32
- Airfoil:modified NACA 2412
- Empty weight: 1,691 lb (767 kg)
- Gross weight: 2,450 lb (1,111 kg)
- Fuel capacity: 56 US gallons (212 litres)
- Powerplant: 1 × Lycoming IO-360-L2A four cylinder, horizontally opposed aircraft engine, 160 hp
- Propellers: 2-bladed metal
Performance
- Cruise speed: 122 kn (140 mph; 226 km/h)
- Stall speed: 47 kn (54 mph; 87 km/h) (power off, flaps down)
- Never exceed speed:163 kn (188 mph; 302 km/h) (IAS)
- Range: 696 nmi (801 mi; 1,289 km) with 45 minute reserve, 55% Power, at 12,000 ft
- Service ceiling: 13,500 ft (4,100 m)
- Rate of climb: 721 ft/min (3.66 m/s)
- Wing loading: 14.1 lb/sq ft (68.6 kg/m²)
The Cessna 172 Skyhawk:
four-seat, single-engine, high-wing fixed-wing aircraft made by the Cessna Aircraft Company. First flown in 1955 and once again in production, more Cessna 172s have been built than any other aircraft. This model is marketed under the name Skyhawk SP, although the Type Certification data sheet specifies it is a 172S.
General characteristics
- Crew: one
- Capacity: three passengers
- Length: 27 ft 2 in (8.28 m)
- Wingspan: 36 ft 1 in (11.00 m)
- Height: 8 ft 11 in (2.72 m)
- Wing area: 174 sq ft (16.2 m2)
- Aspect ratio: 7.32
- Airfoil:modified NACA 2412
- Empty weight: 1,691 lb (767 kg)
- Gross weight: 2,450 lb (1,111 kg)
- Fuel capacity: 56 US gallons (212 litres)
- Powerplant: 1 × Lycoming IO-360-L2A four cylinder, horizontally opposed aircraft engine, 160 hp
- Propellers: 2-bladed metal
Performance
- Cruise speed: 122 kn (140 mph; 226 km/h)
- Stall speed: 47 kn (54 mph; 87 km/h) (power off, flaps down)
- Never exceed speed:163 kn (188 mph; 302 km/h) (IAS)
- Range: 696 nmi (801 mi; 1,289 km) with 45 minute reserve, 55% Power, at 12,000 ft
- Service ceiling: 13,500 ft (4,100 m)
- Rate of climb: 721 ft/min (3.66 m/s)
- Wing loading: 14.1 lb/sq ft (68.6 kg/m²)
Avionics
- Garmin G1000