確定日付の確度: 確定確定として発表情報源が日付をどれだけ確定的に述べているか：確定、予定、推定、延期、未確認。「確定」のピンをすべて表示確度 82%総合信頼度: 82%ピンの情報源と参照がその日付をどれだけ裏付けているか。出典を含む 5 件の資料がピンの開始・終了時刻をどれだけ強く裏付けているかの加重平均。最新の資料より180日古くなるごとに重みは半分になります確度75%以上のピンをすべて表示
EASA type-certificate data sheet A.172 lists 'Initial Certification Date: A300 B2-1A: 15 March 1974'; Wikipedia[2] says certificates were granted by German and French authorities that day.Airbus A300B2 Wins Type Certification
主な競合製品
- McDonnell Douglas DC-10 · McDonnell Douglas
About 270 seats in two classes (399 maximum) - DC-10-10 range 3,500 nmi (6,500 km), DC-10-30 up to 5,200 nmi (9,600 km) - three engines - in service since 5 August 1971
出典 - Lockheed L-1011 TriStar · Lockheed
Up to 400 passengers - range over 4,000 nmi (7,410 km) - three Rolls-Royce RB211 engines - entered service with Eastern Air Lines on 26 April 1972
出典
The Airbus A300B2-1A received its initial type certificate on 15 March 1974, clearing Airbus's first production wide-body for airline service two months before its first delivery.
- EASA's current data sheet for the A300 family dates the first production variant, the A300B2-1A, to 15 March 1974; the B2-1C followed on 2 October 1974 and the two-prototype A300B1 only on 12 November 1974[1]
- Wikipedia records that French and German authorities issued the certificates that day and that FAA certification followed on 23 May 1974[2]
- The test campaign used four aircraft and about 1,580 flight hours and was described as relatively problem-free, though early flight testing had turned up an over-sensitive turn response on 6 December 1972 that nearly derailed the programme[2][4]
- Simple Flying notes that Air France had committed to six airframes in 1970, four years before the plane would debut in passenger service[3]
Notable features
- Variant: A300B2-1A, certified 15 March 1974 with two General Electric CF6-50A turbofans; the B2-1C with CF6-50C followed on 2 October 1974[1]
- Weights (basic WV 00): MTOW 137,000 kg, maximum landing 127,500 kg, zero fuel 116,500 kg; limits Mach 0.86 and 360 KIAS[1]
- Fuel: 44,000 litres with high-level shut-off (outer 9,230 L, inner 34,770 L)[1]
- Airbus's planning chart for the B2-101 shows 269 passengers and baggage at about 1,300 nm, 2,050 nm at maximum fuel capacity, cruise Mach 0.78 and a sea-level takeoff field of roughly 5,800 ft at MTOW (read from graph)[5]
- Fuselage 5.64 m in diameter, eight-abreast seating and two LD3 containers side by side; length 53.61 m and wing span 44.84 m[2]
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