إيرباص إيه 310
(تم التحويل من ايرباص A310)
طائرة إيرباص إيه 310 هي طائرة تجارية صغيرة تشبه سلفها إيرباص إيه 300 إلا أنها أنحف وأسرع منها قليلا. تقدر سرعتها ب 1216 كم بالساعة.
| A310 | |
|---|---|
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| |
| An A310, gear and flaps extended, from Air Transat, formerly one of its largest operators | |
| الدور | Wide-body jet airliner |
| دولة المنشأ | Multinational[1] |
| الصانع | Airbus |
| أول تحليق | 3 April 1982 |
| التقديم | April 1983 with Swissair |
| الوضع | In limited service |
| المستخدم الرئيسي | Mahan Air Air Transat (historical) Yemenia Iran Air |
| المنتـَج | 1983–1998 |
| العدد المنتج | 255[2] |
| تطورت من | Airbus A300 |
| تنويعات | Airbus A310 MRTT Airbus CC-150 Polaris |
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
المواصفات
| Model | A310-200 | A310-300 |
|---|---|---|
| Cockpit Crew | Two | |
| 2-class | 220 passengers (20F + 200Y)[4] | |
| 1-class | 237Y 8-abreast | 243Y 8-abreast / 265Y 9-abreast |
| Exit limit | 275 passengers[5] | |
| Lower deck | 14 LD3 containers | |
| Length | 46.66 m (153 ft 1 in) | |
| Height | 15.8 m (51 ft 10 in) fuselage | |
| Wing | 43.9 m (144 ft) span, 219 m2 (2,360 sq ft) area, 28 ° sweep[6] 8.8 aspect ratio | |
| Cross section | 5.64 m (18 ft 6 in) | |
| Maximum Payload | 32,834 kg (72,387 lb) | 37,293 kg (82,217 lb) |
| MTOW | 144,000 kg (317,466 lb) | 164,000 kg (361,558 lb) |
| OEW | JT9D: 77.4 t (171,000 lb), PW4000/CF6-80: 79.2 t (175,000 lb) | |
| Max fuel | 47,940 kg / 105 689 lb | |
| Engines | JT9D-7R4 / GE CF6-80 | JT9D-7R4E1 / PW4000 / CF6-80C2 |
| Thrust (×2) | 203.8–257.4 kN (45,800–57,900 lbf)[5] | |
| speed | Mach 0.8 (459 kn; 850 km/h) cruise,[7] Mach 0.84 (482 kn; 892 km/h) MMO[5] | |
| Ceiling | 41,100 ft (12,527 m)[5] | |
| Range | 3,500 nmi (6,500 km) [أ] | 5,150 nmi (9,540 km) [ب] |
تنويعات الموديل
| Model | Certification Date | Engines |
|---|---|---|
| A310-203 | 11 March 1983 | GE CF6-80A3 |
| A310-203C | 27 November 1984 | GE CF6-80A3 |
| A310-204 | 23 April 1986 | GE CF6-80C2A2 |
| A310-221 | 11 March 1983 | PW JT9D-7R4D1 |
| A310-222 | 22 September 1983 | PW JT9D-7R4E1 |
| A310-304 | 11 March 1986 | GE CF6-80C2A2 |
| A310-308 | 5 June 1991 | GE CF6-80C2A8/A2 |
| A310-322 | 5 December 1985 | PW JT9D-7R4E1 |
| A310-324 | 27 May 1987 | PW4152 |
| A310-325 | 6 March 1992 | PW4156A |
انظر أيضاً
تطورات ذات صلة
طائرات شبيهة
قوائم ذات صلة
المراجع
الهامش
- ^ Final assembly in France
- ^ خطأ استشهاد: وسم
<ref>غير صحيح؛ لا نص تم توفيره للمراجع المسماةAirbus_Deliveries - ^ "A310 Airplane Characteristics for Airport Planning" (PDF). Airbus. ديسمبر 2009.
- ^ "Out-of-production / A310". Airbus.
- ^ أ ب ت ث ج "Type Certificate Data Sheet" (PDF). EASA. 21 سبتمبر 2017. Archived from the original (PDF) on 29 نوفمبر 2018. Retrieved 29 نوفمبر 2018.
- ^ "Airbus Aircraft Data File". Civil Jet Aircraft Design. Elsevier. يوليو 1999.
- ^ "A310". Aircraft Technical Data & Specifications. Airliners.net.
ببليوگرافيا
- Endres, Günter (Spring 2004). "Classic Airliner: Airbus A300". Flightpath: The International Journal of Commercial Aviation. Norwalk, Connecticut, USA: AIRtime Publishing (Volume 3): 36–85. ISBN 1-880588-73-0.
- Gunston, Bill (فبراير 2010). Airbus: The Complete Story. Sparkford, Yeovil, Somerset, UK: Haynes Publishing, 2009. ISBN 978-1-84425-585-6.
- Norris, Guy and Mark Wagner (1999). Airbus. St. Paul, Minnesota: MBI Publishing, 1999. ISBN 0-7603-0677-X.
- Pitt, Ivan L. and John Randolph Norsworthy. Economics of the U.S. Commercial Airline Industry: Productivity, Technology and Deregulation. "Springer", 2012. ISBN 1-4615-5031-9.
- Senguttuvan, P. S. Fundamentals of Air Transport Management. "Excel Books India", 2006. ISBN 81-7446-459-X.
- Simons, Graham. The Airbus A380: A History. "Pen and Sword", 2014. ISBN 1-78303-041-0.
- "World Airliner Census". Flight International, Volume 184, Number 5403, 13–19 August 2013, pp. 40–58.
Notes
- ^2 The fuselage is 14 frames (7.42m) shorter than the A300 fuselage, but the rear bulkhead was set 2 frames farther into the tailcone, so that only 12 frames of seating capacity were lost in the shortened version.
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