Airbus A330-200MRTT Tanker
One of the greatest attributes of the Airbus A330 as a tanker aircraft is its massive internal fuel capacity, the 111.000 kg / 122 tons of fuel is held in the wings which leaves the lower deck available for cargo. With under floor tanks the fuel capacity can be further increased while retaining main deck cargo capacity or seating for strategic transport. The A330-200MRTT can be fitted with a variety of refueling options, from a new air refueling boom system developed by EADS or two wing pods, to a combination of wing pods and a center fuselage refueling unit (hose and drogue) and/or boom system.
-The fly-by-wire technology boom is 11,28 m. long, and it extends to a length of 17,68 m. for refueling, transfer rate of 4.542 liter/min at a pressure of 50 psi. Boom operations are managed from a station in the cockpit. The operator’s position is optimized for man-machine interface and utilizes a 3-D stereoscopic enhanced vision system for day/night boom operation.
-The under fuselage centerline hose & drogue unit delivers fuel though an 25,91 m.-long hose, with an off-load rate 2.271 liter/min at a pressure of 50 psi.
-Two under wing pods have a transfer rate of 1.590 liter/min at a pressure of 50 psi., and their hoses extend to a distance of 27,43 m.
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Royal Australian Air Force ordered 5 aircraft.
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Royal Saudi Air Force ordered 6 aircraft.
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United Arab Emirates Air Force ordered 3 aircraft.
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United Kingdom: Royal Air Force will lease 14 aircraft.
Australia
The RAAF’s five aircraft will be equipped with both an Aerial Refuelling Boom System (ARBS) and two Cobham 905E under-wing refuelling pods. Australia was initially to procure four aircraft with an option to obtain a fifth, however it has since decided to go ahead with the procurement of the fifth aircraft in order to allow for two simultaneous deployments of two aircraft, with the fifth providing contingency cover. All of Australia’s Airbus A330 MRTT aircraft will be operated by No. 33 Squadron RAAF based at RAAF Base Amberley.
Following a 12–15 month delay, the first two Australian aircraft are now due to be delivered in mid-2010, with a third by the end of the year and the remaining two in 2011 and 2012 respectively. The Australian aircraft are designated KC-30A Multi-Role Tanker Transports.
Saudi Arabia
Saudi Arabia finalized an agreement to purchase three A330 MRTT equipped with both an Aerial Refuelling Boom System (ARBS) and two Cobham 905E under-wing refuelling pods, on 3 January 2008. In July 2009 it was released that Saudi Arabia ordered three additional A330 MRTT tankers.
United Arab Emirates
In 2007, the United Arab Emirates announced it had signed a memorandum of understanding with Airbus to purchase three A330 MRTT. EADS, Airbus’s parent company, announced the signing of a contract with UAE in February 2008. The UAE aircraft will be equipped with both an Aerial Refuelling Boom System (ARBS) and two Cobham 905E under-wing refuelling pods.
United Kingdom
On 27 March 2008, the UK Ministry of Defense signed a deal to lease 14 aircraft from EADS-led consortium AirTanker, with the first aircraft due to enter service in 2011. All of the RAF aircraft will be fitted with two Cobham 905E under-wing refuelling pods and 7 will be capable of being fitted with one Cobham 805E Fuselage Refuelling Unit (FRU).
A330-200 MRTT facts:
- Developing nation: Europe
- Manufacturer / designer: EADS – Airbus Industries
- Production line: Toulouse – Blagnac, France
- Type Aircraft: A33-200 MRTT Aerial tanker and transport
- First flight(s): A330-200 MRTT – June 15 2007
- First delivery: A330-200 MRTT – year 2010 (Royal Australian Air Force)
- Crew: Two pilots, two boom-operators
- Aero medical evacuation: 130 stretchers or 70 stretchers and 6 intensive care units.
- Cabin length: 45,00 m.
- Cabin diameter: 5,28 m.
- Cabin height: 2,54 m.
- Cargo volume: Under floor 136 m³
- LD3 containers in belly: 26x
- Standard pallets (2,24 x 3,17 m.): In belly 8x including 2 LD3 containers.
- NATO pallets (2,24 x 2,75 m.): 34x
- Wing span: 60,30 m. with winglets
- Wing area: 361,60 m²
- Wing sweep: 30 degrees
- Fuselage length: 59,00 m.
- Fuselage diameter: 5,64 m.
- Height: 17,40 m.
- Wheelbase: 22,20 m.
- Track: 10,69 m.
- Engines: 2x General Electric CF6-80E1A4 rated 297.44 kN. / or: 2x Rolls Royce Trent 772B rated 315.9 kN
- Weight empty: 120.520 kg.
- Fuel: 139.090 liters
- Max. Payload: 48.988 kg.
- Max. take off weight: 239.950 kg.
- Max. landing weight: 181.982 kg.
- Cruise speed: 860 Kph.
- Max. speed: 880 Kph.
- Service ceiling: 12.497 m.
- Max. ceiling: 12.497 m.
- Max. range: 13.057 Km.
- Centerline flying boom: 11,28 m. long, extends to a length of 17,68 m, rated 4.542 liter/min. at a pressure of 50 psi.
- Centerline hose drum unit: 25,91 m. long, rated 2.271 liter/min. at a pressure of 50 psi.
- Under wing pods (x2): 27,43 m. long, rated 1.590 liter/min. at a pressure of 50 psi.
- Wing tank: 91.298 liters.
- Center tank: 41.559 liters.
- Trim tank: 6.230 liters.
Military Systems
The A330 MRTT also features a suite of advanced military avionics and mission systems integrated with the civil avionics, and can also be provided with a comprehensive survivability package including a Defensive Aid System, fuel tank inerting and cockpit armouring.
Airbus A400M
The A400M program is a direct result of a commonly expressed need by 8 European air forces for a new generation military airlifter.
Airbus A400M timeline:
The Airbus A400M development started in the seventies as the Future Large Aircraft project. Request for Proposal August 1997.
Memorandum of Understanding is signed June 19, 2001 at the Le Bourget Air show.
On May 27, 2003, a contract was signed between Airbus Military and OCCAR (Organization Conjointe de Cooporation en Matire d’Armement), representing Belgium, France, Germany, Luxembourg, Spain, Turkey, and United Kingdom for a total of 180 aircraft.
The industrial program was formally launched on May 31, 2003.
Start production January 2005.
First Roll out: June 26, 2008
First Flight December 11, 2009, and the first deliverywill be in 2012.

First Flight December 11, 2009
The A400M Common Standard Aircraft (CSA) is capable of performing:
strategic operations (long range, large capacity, high cruise speed).
tactical missions (soft-field performance, autonomous ground operation, low speed / low level operations, aerial delivery).
“in-theatre” tanking operations (receiving as well as dispensing fuel).
The A400M is designed to civil certification standards complemented where appropriate by specific military requirements. The aircraft design incorporates leading state-of-the-art technology including:
Fly-by-wire Flight Control System with side stick controllers.
Flight envelope protection system, already proven in Airbus commercial aircraft.
Advanced structural design incorporating extensive use of composite materials.
High performance turboprop engines, allowing operation in civil air traffic control environment.
High flotation landing gear, allowing operation from short, unpaved airfields.
The Airbus A400M will play an essential role in enhancing Europe’s airlift capabilities, whilst enabling the establishment of common support, training and operational procedures and greater interoperability in multi-national humanitarian and peace-keeping missions.
Air-to-Air Refueling:
The A400M is also quickly convertible into a tactical tanker. The flight envelope of the A400M allows it to refuel a wide range of aircraft and helicopters, at the altitudes appropriate to their missions.
A two-point trailing drogue system can be installed within two hours by fitting two standard air-to-air refueling pods (optional) to the multi-role attachment points on the wings. Each pod provides a fuel flow of up to 1200kg/min.
A centre-line pallet-mounted hose drum unit can be fitted in the rear cargo bay. It provides a fuel flow of 1800kg/min.
| Developing nation: | European Nations. |
| Manufacturer/designer: | Airbus Military. |
| Production line: | Sevilla, Spain |
| Type aircraft: | Military transporter. |
| First flight: | December 11, 2009 |
| First delivery: | 2012 |
| Airbus A400M | |
| Cockpit crew: | 2 pilots, 1 loadmaster |
| Troops: | 120 |
| Cabin length: | 17,71 m. |
| Cabin diameter: | 4,00 m. |
| Cabin height: | 3,85 m. |
| Ramp length: | 5,40 m. |
| Cargo volume: | 356 m³. |
| Wing span: | 42,4 m |
| Wing area: | 221,5 m². |
| Fuselage length: | 43,8 m. |
| Fuselage diameter: | 4,10 m. |
| Height: | 14,6 m. |
| Engines: | - four Europrop International TP400-D6?each rated 11.000 Hp. |
| Propeller: | Ratier FH386 eight blades 5,33 m diameter. |
| Weight: | - empty: 70.000 Kg. - fuel: 46.700 kg. - max. payload: 37.000 Kg. |
| Max. take off weight: | 130.000 Kg. |
| Max. landing weight: | 114.000 Kg. |
| Cruise speed: | mach 0,68. |
| Max. speed: | mach 0,72. |
| Service ceiling: | 8.840 m. |
| Max. ceiling: | 12.190 m. |
| Max. range: | 9.260 km. |
| Performance: | - take-off run 940 m at max. take-off weight.- landing run 625 m at max. landing weight. |
| Airbus A400M order book: | |
| Belgium
Chile France Germany Luxembourg South-Africa Spain Turkey United Kingdom |
7
3 50 60 1 4 8 27 10 25 |
Luxembourg
Malaysia
Spain
Turkey
United Kingdom
1
4
27
10
25
Airbus A350
The Airbus A350 (Airbus response to the Boeing 787) is based on the A330, but with substantial improvements to boost range. It offers a maximum of operational commonality with the current A330/A340 line – including Common Type Rating with the A330.
New technologies used in the Airbus A350 are taken from other Airbus programs, mainly the A380. Airbus proven expertise in the development and application of composites and innovative new materials will be used to incorporate a high percentage of lightweight structural materials, such as Carbon Fiber Reinforced Plastic (CFRP) and aluminum-lithium alloys. For example, the A350 wing will be largely manufactured using CFRP. Furthermore, the Airbus A350 wing will deliver exceptional low and high-speed efficiency thanks to cutting-edge design and manufacturing techniques and the integration of droop nose’ technology from the A380.
The Airbus A350 will further enhance Airbus’ reputation for providing the most comfortable long-range cabins in the sky, featuring solid-state lighting technology to enable maximum customization and passenger comfort, and full compatibility with the latest generation In-Flight Entertainment (IFE) systems. Cabin services will be controlled through the unique Airbus Cabin Intercommunication Data System (CIDS). Both versions of the aircraft may be fitted with spacious crew rest facilities for up to two pilots and eight cabin crew, facilities which have already proved successful on A340-500/-600 aircraft currently in service.
Airbus A350 time-line:
- October 2004 – further information filtering through indicated that Airbus is planning two A350 variants, based on the fuselage lengths of the A330-200 (250 seats) and the A330-300 (295 seats).
- December 10, 2004 – Airbus has received approval from its shareholders, EADS and BAE Systems to begin making firm commercial offers to launch customers for two new members of its wide-body Family.
- October 6, 2005 – Following approval by its shareholders, EADS and BAE Systems, Airbus has formally launched the new passenger long-range A350 aircraft, for which it has already received 140 firm order commitments from nine world-renowned customers.
A350-800
| AIRCRAFT DIMENSIONS | ||||||
| metric | imperial | |||||
| Overall length | 60.54 m | 198 ft. 7.5 in. | ||||
| Height | 17.05 m. | 55 ft. 11.3 in. | ||||
| Fuselage length | 58.9 m. | 193 ft. 3 in. | ||||
| Fuselage height | 6.09 m | 19 ft. 11 in. | ||||
| Cabin width (Between armrest) | 5.59 m | 18 ft. 4 in. | ||||
| Cabin length | n/a | |||||
| Wing span | 64.8 m | 212 ft. 5 in. | ||||
| Wing area (reference) | 443 m2 | 4,740 ft2. | ||||
| Sweep (25% chord mid-wing) | 31.9 degrees | 31.9 degrees | ||||
| Wheelbase | 24.86 m | 81 ft. 7 in. | ||||
| Track | 10.6 m | 34 ft. 9 in. | ||||
| BASIC OPERATING DATA | ||||||
| metric | imperial | |||||
| Engines | RR | RR | ||||
| Thrust | 75,000 lb. slst | 75,000 lb. slst | ||||
| Typical seating (level 0) | 270 | 270 | ||||
| Range (w/max. passengers) | 15.400 km | 8,300 nm. | ||||
| Typical cruise speed | 0.85 (Mmo) | 0.85 (Mmo) | ||||
| Ceiling | 43,100 ft. | |||||
| LD3 Capacity Underfloor | 28 | 28 | ||||
| Max. Pallet Number Underfloor | 9 | 9 | ||||
| Bulk hold volume | 11.3 m3 | 400 ft3 | ||||
| Optimum Configuration (+bulk) | n/a | n/a | ||||
| DESIGN WEIGHTS | ||||||
| tonnes | lb x 1000 | |||||
| Max. ramp weight | 248.9 | 548.7 | ||||
| Max. take-off weight | 248 | 546.7 | ||||
| Maximum landing weight | 185 | 407.9 | ||||
| Maximum zero fuel weight | 173.5 | 382.5 | ||||
| Maximum fuel capacity | 129.000 Litres | 34,082 US gal. | ||||
| Typical operating weight empty | n/a | n/a | ||||
| Typical volumetric payload | n/a | n/a | ||||
Airbus A350-900
| AIRCRAFT DIMENSIONS | ||||||
| metric | imperial | |||||
| Overall length | 73.88 m | 242 ft. 4.7 in. | ||||
| Height | 17.05 m | 55 ft. 11.3 in. | ||||
| Fuselage length | 72.3 m | 237 ft. 1 in. | ||||
| Fuselage width | 5.96 m | 19 ft. 6 in. | ||||
| Fuselage height | 6.09 m | 19 ft. 11 in. | ||||
| Cabin width (Between armrest) | 5.59 m | 18 ft. 4 in. | ||||
| Cabin length | ||||||
| Wing span | 64.8 m | 212 ft. 5 in. | ||||
| Wing area (reference) | 443 m2 | 4,767 ft2. | ||||
| Sweep (25% chord mid-wing) | 31.9 degrees | 31.9 degrees | ||||
| Wheelbase | 33.1 m | 108 ft. 7 in. | ||||
| Track | 10.7 m | 35 ft. 2 in. | ||||
| BASIC OPERATING DATA | ||||||
| metric | imperial | |||||
| Engines | RR | RR | ||||
| Thrust | 93,000 lb. slst | 93,000 lb. slst | ||||
| Typical seating (level 0) | 350 | 350 | ||||
| Range (w/max. passengers) | 14.800 km | 8,000 nm. | ||||
| Typical cruise speed | 0.85 (Mmo) | 0.85 (Mmo) | ||||
| Ceiling | 41,450 ft | |||||
| LD3 Capacity Underfloor | 44 | 44 | ||||
| Max. Pallet Number Underfloor | 14 | 11 | ||||
| Bulk hold volume | 11.3 m3 | 400 ft3 | ||||
| Optimum Configuration (+bulk) | n/a | n/a | ||||
| DESIGN WEIGHTS | ||||||
| tonnes | lb x 1000 | |||||
| Max. ramp weight | 298.9 | 659.0 | ||||
| Max. take-off weight | 298 | 657.0 | ||||
| Maximum landing weight | 228.5 | 503.8 | ||||
| Maximum zero fuel weight | 213.5 | 470.7 | ||||
| Maximum fuel capacity | 156.000 Litres | 41,215 US gal. | ||||
| Typical operating weight empty | n/a | n/a | ||||
| Typical volumetric payload | n/a | n/a | ||||
A350-1000
| AIRCRAFT DIMENSIONS | ||||||
| metric | imperial | |||||
| Overall length | 66.89 m | 219 ft. 5.5 in. | ||||
| Height | 17.05 m | 55 ft. 11.3 in. | ||||
| Fuselage length | 65.3 m | 214 ft. 1 in. | ||||
| Fuselage width | 5.96 m | 19 ft. 6 in. | ||||
| Fuselage height | 6.09 m | 19 ft. 11 in. | ||||
| Cabin width (Between armrest) | 5.59 m | 18 ft. 4 in. | ||||
| Cabin length | ||||||
| Wing span | 64.8 m | 212 ft. 5 in. | ||||
| Wing area (reference) | 443 m2 | 4,767 ft2. | ||||
| Sweep (25% chord mid-wing) | 31.9 degrees | 31.9 degrees | ||||
| Wheelbase | 28.67 m | 94 ft. 1 in. | ||||
| Track | 10.6 m | 34 ft. 9 in. | ||||
| BASIC OPERATING DATA | ||||||
| metric | imperial | |||||
| Engines | RR | RR | ||||
| Thrust | 84,000 lb. slst | 84,000 lb. slst | ||||
| Typical seating (level 0) | 314 | 314 | ||||
| Range (w/max. passengers) | 15.000 km | 8,100 nm. | ||||
| Typical cruise speed | 0.85 (Mmo) | 0.85 (Mmo) | ||||
| Ceiling | 43,100 ft. | |||||
| LD3 Capacity Underfloor | 36 | 36 | ||||
| Max. Pallet Number Underfloor | 11 | 11 | ||||
| Bulk hold volume | 11.3 m3 | 400 ft3 | ||||
| Optimum Configuration (+bulk) | n/a | n/a | ||||
| DESIGN WEIGHTS | ||||||
| tonnes | lb x 1000 | |||||
| Max. ramp weight | 268.9 | 592.8 | ||||
| Max. take-off weight | 268 | 590.8 | ||||
| Maximum landing weight | 205 | 451.9 | ||||
| Maximum zero fuel weight | 192 | 423.3 | ||||
| Maximum fuel capacity | 138.000 Litres | 36,460 US gal. | ||||
| Typical operating weight empty | n/a | n/a | ||||
| Typical volumetric payload | n/a | n/a | ||||


