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Atlas Editions Silver Classics – Airbus A318 – 2002

599 Kč

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Katalogové číslo: MAG HB18 Kategorií: , , , , , , , ,
Výrobce: Atlas Edition Silver ClassicsMěřítko: 1:200Letecká společnost: Silver Classics Aviation

Popis

-sběratelský model letadla Airbus A318  1/200
-provedení: kovový postříbřené model ( váha-0,4 kg.)
 -model je v kvalitním provedení 
-součástí balení je stojánek

Airbus A318

The Airbus A318 is the smallest member of the Airbus A320 family of short- to medium-range, narrow-body, commercial passenger twin-engine jet airliners manufactured by Airbus.The A318 carries up to 132 passengers and has a maximum range of 3,100 nmi (5,700 km; 3,600 mi).Final assembly of the aircraft took place in Hamburg, Germany. It is intended primarily for short-range service, although British Airways uses the aircraft on a London City Airport to New York-JFK Airport transatlantic route (albeit with a stopover in Shannon for refueling on the westbound leg).

Role Narrow-body jet airliner
National origin Multi-national
Manufacturer Airbus
First flight 15 January 2002
Introduction 2003 with Frontier Airlines
Status In service
Primary users Air France
Avianca Brasil
Avianca
TAROM
Produced 2001–2013
Number built 80
Unit cost
US$77.4 million, €63 million (2018)
Developed from Airbus A319
Airbus A318 specifications
Cockpit crew Two
Exit Limit 136
1-class max. seating 132 at 29–30 in (74–76 cm) pitch
1-class, typical 117 at 32 in (81 cm) pitch
2-class, typical 107 (8F @ 38 in, 99Y @ 32 in)
Cargo capacity 21.2 m3 (750 cu ft)
Length 31.44 m (103 ft 2 in)
Wingspan 34.10 m (111 ft 11 in)
Wing area 122.4 m2 (1,318 sq ft)
Wing sweepback 25 degrees
Tail height 12.56 m (41 ft 2 in)
Cabin width 3.70 m (12 ft 2 in)
Fuselage width 3.95 m (13 ft 0 in)
Operating empty weight 39,500 kg (87,100 lb)
Maximum zero-fuel weight (MZFW) 54,500 kg (120,200 lb)
Maximum landing weight (MLW) 57,500 kg (126,800 lb)
Maximum take-off weight (MTOW) 68,000 kg (150,000 lb)
Cruising speed Mach 0.78 (829 km/h; 515 mph)
Maximum speed Mach 0.82 (871 km/h; 541 mph)
Range, typical payload 3,100 nmi, 5,750 km
ACJ range 4,200 nmi, 7,800 km
Takeoff (MTOW, SL, ISA) 1,780 m (5,840 ft)
Landing (MLW, SL, ISA) 1,230 m (4,040 ft)
Fuel capacity 24,210 L (5,330 imp gal; 6,400 US gal)
Ceiling 39,100–41,000 ft (11,900–12,500 m)
Engines (×2) CFM56-5B, 68.3 in (1.73 m) fan
PW6000A, 56.5 in (1.44 m) fan
Thrust (×2) 96–106 kN (22,000–24,000 lbf)

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