Airbus A300-608ST Super Transporter
The A300-600ST Super Transporter (nicknamed Beluga) based on the A300-600 airliner was designed to replace Airbus Industries Super Guppy transports, used by the consortium to ferry oversize components such as wings and fuselage sections between Airbus’ partners’ plants throughout western Europe.
The Airbus Super Transporter features the widest fuselage cross-section of any aircraft, civil of military, and his main deck cargo volume is greater than the Lockheed C-5B Galaxy, Antonov 124 and Boeing C-17.
Airbus A300B4-608ST Super Transporters are also available for charter flights for third parties. Air Transports Internationals home base is in Toulouse, France adjacent to Airbus.
In 1999 the Beluga carried a famous very large painting from the Mus?e du Louvres in Paris to Tokyo. In February 2003, it transported three helicopters for Eurocopter to Australia, while in 2004 it made three trips to Ba?konur, the historical Russian launch site, to deliver three Astrium satellites. In September 2005, the Beluga contributed to the Hurricane Katrina, New Orleans, USA, emergency relief effort with 30 tonnes of tents, blankets, camp beds and a mobile hospital.
The “Beluga” has flown two new production NH90 helicopters from Marseille, France to Berlin in Germany, the transport of two operational United Nations CH-53s from Larnaka in Cyprus to Frankfurt, Germany, and the shipment of an EH-101 from Milan, Italy to Fairbanks, Alaska.
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Developing nation: |
Europe. |
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Manufacturer/designer: |
EADS – Airbus Industry. |
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Production line: |
Toulouse-Blagnac, France. |
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Type aircraft: |
Oversize cargo freighter. |
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First flight: |
September 13, 1994. F-WAST. |
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First delivery: |
October 25, 1995. |
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Airbus A300-608ST “Beluga” |
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Cockpit crew: |
Two pilots. |
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Cargo length: |
37,7 m. |
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Cargo cylindrical length: |
21,34 m. |
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Cargo diameter: |
7,10 m. |
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Cargo volume: |
- Maine deck 1.400 m³. |
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Wing span: |
44,84 m. |
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Wing area: |
260 m². |
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Fuselage length: |
56,16 m. |
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Fuselage diameter: |
7,31 m. |
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Height: |
- 17,24 m. - Cargo nose door 16,78 m. |
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Engines: |
Two General Electric CF6-80C2A8 rated 262,4 kN. |
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Weight: |
- Max. payload: 47.000 Kg. |
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Max. Take off weight: |
155.000 Kg. |
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Max. Landing weight: |
140.000 Kg. |
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Cruise Speed: |
745 km/h. |
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Max. ceiling: |
10.670 m. |
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Max. Range: |
- 47.000 kg 1.667 km - 40.000 kg 2.779 km - 26.000 kg 4.632 km |
Airbus A300-608ST Production:
5 in service at October 2004.
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Airbus A300-608ST operator: |
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5 – Airbus Transport International. |
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All pictures courtesy of Zijde Aviation Photo and Publishing, Marcel van Leeuwen and Rob Vogelaar.
Airbus A300-600
The A300-600 was further developed into the longer range A300-600R, its extended range courtesy of a fuel trim tank in the tail plane and higher maximum takeoff weights. First flight was on December 9 1987, first delivery was April 20, 1988 to American Airlines.
The first new build pure freighter A300, one of 44 ordered for Federal Express, flew in December 1993. UPS is another major A300-600F customer, following its September 1998 order for 90. Also Air Hong Kong ordered 9 A300-600F.
| Developing nation: | Europe. |
| Manufacturer/designer: | EADS – Airbus Industries. |
| Production line: | Toulouse-Blagnac, France. |
| Type aircraft: | Medium range wide body airliner. |
| First flight: |
July 8th, 1983, F-WZLR. |
| First delivery: | March 1984. |
| Airbus A300-600 | |
| Cockpit crew: | Two pilots. |
| Passengers two class: |
- 26 business class. |
| Cabin length: | 40,70 m. |
| Cabin diameter: | 5,28 m. |
| Cargo volume: |
- Maine deck 304,6 m³. |
| LD3 Containers in belly: | 22. |
| Standard 2.24m x 3.17m pallets: |
- in belly 4, with 8 LD3 Containers. |
| Wing span: | 44,85m. |
| Wing area: | 260m². |
| Wing sweep: | 28 degrees. |
| Fuselage length: | 54,08 m. |
| Fuselage diameter: | 5,64 m. |
| Height: | 16,62 m. |
| Wheelbase: | 18,62 m. |
| Track: | 9,60 m. |
| Engine (s): |
- Two General Electric CF6-80C2A1s rated 262.4 kN. |
| Weight: |
- Empty:90.065 Kg. |
| Max. Take off weight: | 165.900Kg. |
| Max. Landing weight: | 134.000Kg. |
| Cruise Speed: | 850km/h. |
| Max. Speed: | 889km/h. |
| Service ceiling: | 10.668 m. |
| Max. Range: | 6.670 km. |
| Airbus A300-600R* | |
| Engine (s): |
- Two General Electric CF6-80C2A5 rated 273.6 kN. |
| Weight: |
- Empty 90.965 Kg. - Max. payload: 41.100 Kg. |
| Max. Take off weight: | 171.700 Kg. |
| Max. Landing weight: | 140.000 kg. |
| Cruise Speed: | 875km/h. |
| Max. Speed: | 897km/h. |
| Max. Range: |
- 7.505 km with CF-6′s. |
* Generally similar to the Airbus A300-600 except in the following particulars.
| Airbus A300-600F* | |
| Engine (s): |
- Two General Electric CF6-80C2A5 rated 273.6 kN. |
| Weight: |
- Empty:78.335 Kg. |
| Max. Take off weight: | 170.500Kg. |
| Max. Landing weight: | 140.000Kg. |
| Cruise Speed: | 875 km/h. |
| Max. Speed: | 897 km/h. |
| Max. Range: |
- 7.505 km with CF-6′s. |
* Generally similar to the Airbus A300-600 except in the following particulars.
Delivered 279 Airbus A300-600, on order 56, approximately 271 A300-600/R/F variants in service at September 30, 2004.
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A300-600 built of each type: |
| A300-601 – 6 |
| A300-603 – 11 |
| A300-605R – 73 |
| A300-620 – 16 |
| A300-622 – 5 |
| A300-622R – 95 |
| A300F-605R – 42 |
| A300F-622R – 90 |
| Airbus A300B2/B4 & A300-600 civil operators*: | |
| 44 – Federal Express. |
5 – Indian Airlines. |
| 38 – UPS. | 4 – Monarch. |
| 33 – American Airlines. | 3 – Islandsflug. |
| 21 – Thai Airways. | 3 – Mahan Air. |
| 19 – Japan Air Lines Domestic. | 3 – Tunis Air. |
| 14 – Lufthansa. | 3 – Aero Union. |
| 14 – European Air Transport – DHL. | 3 – Air Contractors – DHL. |
| 13 – China Eastern. | 3 – Air Hong Kong. |
| 12 – China airlines. | 3 – Ariana Afghan Airlines. |
| 12 – Saudia – Saudi Arab Airlines | 3 – Channel Express – TNT. |
| 10 – Japan Air system. | 3 – Olympic Air Lines. |
| 10 – Korean Air. | 2 – AMC Aviation. |
| 9 – Onur Air. | 2 – Orex – Orbit Express. |
| 8 – Qatar Airways. | 1 – Paradise International. |
| 8 – Egypt Air. | 1 – Afriqiyah Airways. |
| 7 – Astar Air Cargo. | 1 – Air France. |
| 7 – PIA-Pakistan International Airways. | 1 – Air Macao. |
| 7 – Fly Air. | 1 – Air Scandic. |
| 7 – MNG Cargo. | 1 – Baron Air Cargo. |
| 6 – Iran Air. | 1 – China Southern Airlines. |
| 6 – Express net Airlines. | 1 – Saga Airlines. |
| 6 – TNT Airways. | 1 – Sogerma. |
| 6 – Tradewinds Airlines. | 1 – Sudan Airways. |
| 5 – China Northern Airlines. | 1 – Tristar Air. |
| Airbus A300-600 Military operator*: | |
| 1 – State of Kuwait |
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All pictures courtesy of Zijde Aviation Photo and Publishing
Airbus A380 “Big Goose”
First flight:The first flying aircraft MSN01 F-WWOW will remain the property of Airbus. At the first flight on April 27, 2005 the A380 took off at a weight of 421.000 kg, the highest ever of any civil airliner to date. During the flight, which took the aircraft around South West France, the six crew members explored the aircrafts flight envelope as expected. They tested the A380s handling using both direct and normal flight control laws with the landing gear up and down, and with all flaps and slats settings during the part of the flight at cruise altitude. They made an initial evaluation of the comfort levels in both the main and upper decks, confirming that the cabin was very quiet and the ride smooth.
This maiden voyage, during which all primary flight test objectives were met, marks the beginning of a rigorous test flight campaign involving five A380s, including one for the certification of the Engine Alliance GP7200 engine on the A380, and some 2.500 flight hours. It will culminate in the aircrafts certification followed by its entry into airline service in the second half of 2006 with first operator Singapore Airlines. The scope and rigour of the A380 ground and flight test program should also prepare for a smooth entry into service, planned for 2006.
Future models will include the shortened, 480 seat A380-700, and the stretched, 656 seat, A380-900. (The -700, -800, and -900 designations were chosen to reflect that the A380 will enter service as a “fully developed aircraft” and that the basic models will not be soon replaced by more improved variants).
The A380 assembly building (Toulouse) is one of the largest in the world, measuring 500 m by 250 m, with a height of 46 m. It is the largest of several buildings on the site which, together, incorporate more than 32.000 tons of steel the equivalent of four Eiffel towers or the Millau viaduct – plus 250.000 cubic meters of concrete.
Fuselage:
The A380 has a twin deck configuration with new lighter and even more resistant material is also being used for the first time on a civil airliner after intensive trials. The upper fuselage shell of the A380 is fashioned from GLARE, a laminate alternating layers of aluminum and glass-fiber reinforced adhesive. In addition to being some ten per cent less dense than aluminum – for a weight-saving of around 800 kg – GLARE has proven superior in terms of fatigue as well as fire and damage resistance.
Engines:
The Rolls-Royce Trent 900 is being certificated at 80,000lb thrust, a rating considerably higher than the requirement at entry into service, allowing substantial margin for potential growth. Last year the engine achieved 88,000lb thrust in the early stages of testing.
The Trent 900 will enter service in Spring 2006 with Singapore Airlines and has also been selected by Qantas, Virgin Atlantic and Lufthansa, giving it a 48 per cent share of firm and option orders.
Developed under the Engine Alliance joint venture of Pratt & Whitney and General Electric, the GP7200 benefits from technology mastered by America?s two largest jet powerplant manufacturers. Pratt & Whitney is responsible for the GP7200s low-pressure system, including its large main fan with highly swept titanium blades a key element in the engine?s low noise output. General Electric developed the core section for the GP7200, which incorporates the companys experience in lowering jet engine emissions and boosting operational efficiency. Airbus customers selecting the GP2700 for their A380s are Air France, Emirates, FedEx and International Lease Finance Corporation.
As the choice of launch customer Singapore Airlines (SIA), the Trent 900 is the leading engine for the A380 development program.
| Developing Nation: | Europe. |
| Manufacturer/Designer: | EADS / Airbus Industries. |
| First Flight: |
April 27, 2005 F-WWOW. |
| First passengers flight: | September 4, 2006 (500 passengers) |
| First Delivery: | October 15th 2007 (Singapore Airlines). |
| First Operational: | October 25th 2007 (Singapore-Sidney). |
| A380-800 passengers aircraft | |
| Crew: | 2. |
| Passengers: | 555 in three-class. |
| Cabin Length: | 50,68 m. |
| Fuselage Diameter: | 7,14 m. |
| Max. Cabin Width Main Deck: | 6,58 m. |
| Max. Cabin Width Upper Deck: | 5,92 m. |
| Cargo volume: | 171 m³, (38 LD3 containers) |
| Wing Span: | 79,8 m. |
| Wing Area: | 845 m. |
| Wing sweep: | 33.5 degrees. |
| Length: | 73 m. |
| Height: | 24,1 m. |
| Wheel base: | 30,4 m. |
| Wheel track: | 14,3 m. |
| Engine (s): |
4 Rolls-Royce Trent 900 or 4 GP 7200 Turbofans with 311kN trust. |
| Weight: |
- Empty: 276.800 Kg. - Zero fuel weight: 361.000 Kg. - Internal fuel: 310.000 liters. - Max. payload: 66.400 Kg. |
| Max. Take off weight: | 560.000 Kg. |
| Max. Landing weight: | 386.000 Kg. |
| Cruise Speed: | 902 km/h. |
| Max. Speed: | 945 km/h. |
| Service ceiling: | 13.106 m. |
| Max. Range: | 15.000 km. |
Freighter:
The A380 Freighter has three decks of standard containers, accessible simultaneously through five doors, and offers more payload and more range capability than current freighters.
| A380-800F Freighter | |
| First Delivery: | 2008. |
| Crew: | 2. |
| Total cargo volume: | 4.04 m³. |
| Containers upper-deck: | 17 – 25. |
| Containers main-deck: | 29 – 33 |
| Containers lower-deck: | 13 |
| Wing Span: | 79,8 m. |
| Wing Area: | 845 m². |
| Length: | 73 m. |
| Height: | 24,1 m. |
| Engine (s): |
4 Rolls-Royce Trent 900 or 4 GP 7200 Turbofans with 340 kN trust. |
| Weight: |
- Empty: 252.200 Kg. - Zero fuel weight: 402.000 Kg. - Internal fuel: 310.000 liters. - Max. payload: 152.400 Kg. |
| Max. Take off weight: | 590.000 Kg. |
| Max. Landing weight: | 427.000 Kg. |
| Cruise Speed: | 910 km/h. |
| Max. Speed: | 0,89 mach. |
| Service ceiling: | 13.106 m. |
| Max. Range: | 10.400 km. |
















