Airbus A318

The Airbus A318 is a two-engined short- to medium-range narrowbody airliner with a capacity of maximum 136 Passengers produced by the European manufacturer Airbus S.A.S.. The A318 is the smallest model of the A320-singe-aisle-family.
The Airbus A318 is a shortened (minus 6 meters / 20 ft) development of the A320. It is powered by either Pratt & Whitney PW6000 or CFM International CFM56-5 engines.
Crew 2
Passengers 107 / 117
Propulsion 2 Turbofan Engines
Engine Model CFM Intl. CFM56-5
Engine Power (each) 96,1 kN 21600 lbf
alternative Engine Variant
Engine Model Pratt & Whitney PW6000
Engine Power (each) 96,1 kN 21600 lbf
Speed 900 km/h 486 kts
559 mph
Mmo (max. Mach) Mach 0.82
Service Ceiling 12.131 m 39.800 ft
Range 5.950 km 3.213 NM
3.697 mi.
Empty Weight 34.500 kg 76.059 lbs
max. Takeoff Weight 59.000 kg 130.073 lbs
max. Landing Weight 56.000 kg 123.459 lbs
Wing Span 34,10 m 111 ft 11 in
Wing Area 122,6 m² 1320 ft²
Length 31,44 m 103 ft 2 in
Height 12,56 m 41 ft 2 in
First Flight 15.01.2002
Production Status in production
Developed from Airbus A320
ICAO Code A318
IATA Code 318 32C
FAA TCDS A28NM
EASA TCDS A.064
Data for (Version) Airbus A318
Variants A318?111, A318?112, A318?121, A318?122

 



Boeing 787 dreamliner

The Boeing 787-8 Dreamliner is a two-engined long-range widebody airliner with a capacity of 210 – 250 passengers produced by the American manufacturer Boeing Commercial Airplanes. The 787-8 is a member of the Boeing 787 Dreamliner Familie (787-8, 787-9 und 787-10).
The 787 is the world’s first airliner using composite materials for most of its construction (approx. 50 percent). The fuselage is built as one-piece composite barrel construction. The 787 does not use any bleed air from the engines. Hydraulics systems, wing anti-ice, air conditioning and pressurization are electrical powered. Available 787-8 engine options: Rolls-Royce Trent 1000-A, 1000-C, 1000-E, General Electric GEnx-1B64, -1B67, -1B70.
Crew 2
Passengers typ. 242, max. 359
Propulsion 2 Turbofan Engines
Engine Model Rolls-Royce Trent 1000-E
Engine Power (each) 265,1 kN 59600 lbf
alternative Engine Variant
Engine Model General Electric GEnx-1B70
Engine Power (each) 321,6 kN 72300 lbf
max. Cruise Speed 902 km/h 487 kts
560 mph
Mmo (max. Mach) Mach 0.9
Service Ceiling 13.137 m 43.100 ft
Range 13.621 km 7.355 NM
8.464 mi.
Empty Weight 104.099 kg 229.500 lbs
max. Takeoff Weight 227.930 kg 502.500 lbs
max. Landing Weight 172.365 kg 380.000 lbs
Wing Span 60,12 m 197 ft 3 in
Wing Area 325,0 m² 3498 ft²
Length 56,72 m 186 ft 1 in
Height 16,90 m 55 ft 5 in
First Flight 15.12.2009
Production Status in production
ICAO Code B788
IATA Code 788
FAA TCDS T00021SE
EASA TCDS IM.A.115
Data for (Version) Boeing 787-8 (Trent)