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The A400M is being
developed to meet a shortfall in strategic
airlift among EU states and to replace
the C-130 Hercules and the C-160 Transall.
Originally known as the Future Large
Aircraft (FLA), the A400M will be
powered by four TP400-D6 turboprop
engines and will have a longer range
and bigger payload than rival aircraft
like the C-130 Hercules. The aircraft
will be capable of carrying up to
25 tonnes in the air cargo role or
up to 120 paratroopers. For medical
evacuation (Medevac) operations, it
will be able to carry up to 66 stretchers
plus up to 25 medical staff. It will
also be capable of Air-to-Air Refuelling
(AAR) using two wing-mounted pods
equipped with a drogue system as well
as a centre-line hose drum unit. The
aircraft will normally have three
aircrew, comprising a pilot, co-pilot
and a loadmaster.
Airbus Military
Sociedad Limitada (AMSL) is responsible
for the development and production
of the aircraft. It is owned by Airbus
(69.44%), EADS Casa (20.56%), Turkish
Aerospace Industries (TAI) (5.56%)
and Belgium's Flabel Corporation (4.44%).
Flabel is composed of Belgium's leading
aerospace companies -- Sabca, Sonaca,
Asco Industries, Barco Avionics and
Sabca Limburg.
The development
and construction of the A400M is involving
more than 50 companies and employing
more than 3,000 people. Fuselage assembly
is being undertaken by Airbus Deutschland
at Bremen with Italy's Alenia building
the aft fuselage. The tail section
is being constructed at Hamburg and
Stade in Germany, and EADS Casa at
Tablada in Spain. EADS Military Air
Systems (MAS) at Augsburg is supplying
the aircraft's cargo doors. The nose
fuselage section is being constructed
by Airbus France at Méaulte and St
Nazaire. Airbus UK at Filton has developed
the A400M wings and is supplying the
aircraft's composite wing boxes, constructed
out of carbon-fibre reinforced plastic
material (CRFP). The UK's GKN Aerospace
is supplying wing spars. Other major
companies providing parts of the A400M
include Flabel (flight surfaces),
Safran Group’s Messier-Bugatti and
Messier-Dowty (landing gear, wheels
and brakes), TAI (fuselage parts),
Saab Aerostructures (crew access door),
Thales (avionics, flight management
system) and Northrop Grumman (AN/APN-241E
colour weather/navigation radar).
Europrop International
(EPI) is responsible for managing
the development of the 11,000shp (8,250
kW) three-shaft TP400-D6 turboprop
engine. EPI comprises the UK’s Rolls-Royce
(28%), Germany’s MTU Aero Engines
(28%), France’s Snecma (28%) and Spain’s
Industria de Turbo Propulsores (ITP)
(16%). Workshare is based on each
country's procurement of the A400M
with Snecma responsible for 32%, Rolls-Royce
25%, MTU 22% and ITP 21%.
Snecma's workshare
includes powerplant installation,
engine testing as well as the manufacture
of the engine's combustor and high-pressure
(HP) turbine. Snecma has sub-contracted
other Safran Group companies like
Hispano-Suiza (accessory gearbox and
components), Sagem Défense Sécurité
(inertial navigation system), Sofrance
(fuel and oil filters) and the Belgium-based
Techspace Aero (lubrication systems)
to undertake some of its share of
work on the TP400.
Rolls-Royce is responsible
for engine integration and the manufacture
of the HP compressor, low-pressure
(LP) shaft, intermediate casing and
bearing support structure with work
undertaken in the UK and Germany.
Snecma, MTU and Hispano-Suiza have
developed the engine's Full Authority
Digital Engine Control (FADEC) system
(developed with BAE Systems). IPT
is responsible for the LP turbine,
test equipment and exhaust nozzle,
working with Turkey's Tusas Engine
Industries (TEI). EPI has subcontracted
Italy's Avio to provide the power
gearbox. MTU's workshare includes
the intermediate-pressure (IP) spool
(includes the IP compressor and turbine)
and the company's Ludwigsfelde facility
will undertake final assembly of the
engine, which will be fitted with
an eight-blade composite FH386 propeller
supplied by France’s Ratier-Figeac.
The first TP400
engine to be test flown by an aircraft
is due to take place in the first
quarter of 2008 when the UK's Marshall
Aerospace will use a modified C-130
Hercules. The engine was delivered
to Marshall Aerospace in November
2007. It is estimated that more than
760 engines will be delivered to the
air forces of the project partners.
A total of 180 aircraft
have been ordered by Belgium (7),
France (50), Germany (60), Luxembourg
(1), Spain (27), Turkey (10) and the
UK (25). Belgium will operate Luxembourg’s
single aircraft. The A400M now has
orders outside Europe, comprising
Malaysia (4) and South Africa (8),
bringing the total order book to 192
aircraft.
Italy and Portugal
were originally partners in the project
but withdrew over costs. Italy had
planned to order 44 aircraft but pulled
out in 2001, instead procuring a combined
total of 37 C-130J/J-30 Hercules and
C-27J Spartan transport aircraft in
2002. Portugal planned to order three
aircraft with deliveries in 2016,
but withdrew in 2003, instead announcing
plans to acquire six new C-130J Hercules
to replace the Portuguese Air Force's
ageing C-130H/H-30 fleet. The order
did not materialise in the end. The
Portuguese government has since indicated
that it may procure some A400Ms in
the future, but may in the meantime
upgrade its current Hercules fleet.
Chile also placed an order for three
aircraft, but this has reportedly
been cancelled following the country's
decision to defer procurement.
South Africa and
Malaysia joined the project in 2005.
South Africa's Denel Aviation is responsible
for building fuselage parts, including
the aircraft's composite wing-fuselage
fairing, while Aerosud has been tasked
with design and the development of
parts of the cockpit, wing and fuselage.
Composites Technology Research Malaysia
(CTRM) has been sub-contracted by
Sonaca to build parts, including the
main landing gear doors.
Full assembly of
test and production models will take
place at EADS Casa's newly-constructed
facility at San Pablo in Seville with
five models planned to be used for
flight testing. The first test flight
had originally been planned for late
2007, but a static model for testing
(A/C 5000) was assembled by EADS Casa
at Getafe near Madrid in July 2007
with the first flying prototype (MSN001)
leaving the Final Assembly Line (FAL)
jigs in January 2008 with its maiden
flight due in July 2008. Deliveries
were due to begin in late 2009 beginning
with the French Air Force (Armée
de L’Air), but EADS confirmed
in October 2007 that these will be
delayed until 2010/11 due to problems
with the TP400's development. Full
deliveries are expected to be completed
by about 2017.
Data
Specifications
Overall length: 45.1 m
Wing span: 42.4 m
Overall height: 14.7 m
Weights
Max take-off weight: 136.5
tonnes (300,982 lb)
Max landing weight: 120 tonnes
(264,600 lb)
Max payload: 37 tonnes (81,585
lb)
Max internal fuel: 46.7 tonnes
(102,974 lb)
Performance
Powerplant: 4 x 11,000 shp
(8,250 kW) EPI TP400-D6(8) turboprop
engines
Max speed: 300 knots (560 km/h)
Range with max payload: 3,300
km
Range with 30 tonnes payload:
4,800 km
Max operating altitude: 11,300
m (37,000 ft)
Crew: 3-4
+ 116 troops or up to 66 stretchers
and 25 medical personnel
Status: undergoing development;
on order for: Belgium (7), France
(50), Germany (60), Luxembourg (1),
Spain (27), Turkey (10), the UK (25),
Malaysia (4), South Africa (8).
A400M main
workshare
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| Airbus
(prime
contractor) |
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| fuselage
assembly, tail section,
wings, cockpit, testing |
|
|
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| centre
fuselage, digital map generator
system (DMGS) |
|
|
|
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|
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| systems
prime contractor, mission
management computer (MMC),
defensive aid computer (DAC);
terrain masking low level
flight (TMLLF) system (for
German A400M fleet) |
|
|
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| sponsons,
main landing gear fairings,
nose landing gear |
|
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| ramp
door, cockpit seating |
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| wing
flap support composite skins |
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| wing
fixed leading edges, wing
anti-icing system, leading
edge cowlings |
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| forward
centre fuselage, rear fuselage
upper shell, parachute doors,
emergency exit doors, tail
cone |
|
|
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| nose
fuselage flexible lining,
cargo hold lining, cockpit
linings, wing tip, rigid
bulkhead |
|
| Denel
Aviation (South
Africa) |
|
| composite
wing-fuselage fairing, fuselage
components |
|
|
|
| main
landing gear doors, horizontal
stabiliser trailing edge
panels, vertical tail plane
leading edge panels |
|
|
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| TP400-D6
turboprop engine |
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*
Part of the Fabel Corporation.
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| Patria
Aerostructures
(Fin) |
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| vertical
tail plane tip fairing |
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|
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| avionics,
cockpit control and display
system (CDS), multifunction
displays, integrated modular
avionics (IMS) system (with
Diehl Aerospace) |
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|
|
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|
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| forward
lateral panels, forward
ditching door |
|
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| TP400-D6
FADEC with BAE Systems |
|
|
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| nose
fuselage and cockpit electrical
harnesses |
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| Leach
International
(Fra) |
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| primary
electrical power distribution
system |
|
|
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|
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| IMS system,
ramp door controller (RDC),
doors management system
(DSMS) |
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| FLASH
(Flying Laser Self-Defence
System Against Infrared
Seeker Head Missiles) |
|
|
|
| primary
flight control actuators |
|
| Pfalz
Flugzeugwerke
(Ger) |
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| structural
floor and the drainage system |
|
Rheinmetall
Defence Electronics
(Ger) |
|
| loadmaster
control system |
|
|
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| M3AR
HF/VHF/UHF airborne transceivers |
|
| Aciturri
Aeronautica (Spa) |
|
|
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|
hydraulic
landing gear, door and ramp
actuators, nose landing
gear, hot air pneumatic
system (with Liebherr Aerospace
and EADS), assembly and
testing of
TP400-D6 subsystems, design
of TP400-D6 fixtures and
tools |
|
|
|
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| Sener
Ingenieria & Sistemas
(Spa) |
|
|
Sistemas
Integrales de
Producción (Spa) |
|
|
|
|
| audio
management system (AMS),
MIDS interface computer
(MIC), windscreen heating
system |
|
| Tusas
Engine Industries
(Turkey) |
|
| TP400
front bearing structure,
primary nozzle |
|
| Dunlop
Aircraft Tyres
(UK) |
|
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| in-flight
refuelling probe |
|
|
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| wing
spars, wing trailing edge
assembly, wing leading edge
panels, trailing edge panels |
|
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| active
noise and vibration control
system |
|
|
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| TP400-D6
engine sensors (with UK's
Safetech Engineering) |
|
|
|
| cockpit
integrated control panels
(ICP) system, lighting system
|
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| Saab
Aerostructures
(Swe) |
|
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| terrain
masking low-level flight
computer (for TMLLF system
to equip German A400M fleet),
Lifetime Monitoring System
(LTMS) |
|
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| high-lift
control & monitoring
system |
|
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| cargo
loading systems, aerial
delivery system |
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| electrical
power generation system
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| integrated
passenger and crew oxygen
system |
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| Esterline
Technologies
(US) |
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| TP400-D6
engine sensors (see Weston
Aerospace), primary
power system sensors |
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| Goodrich
Corporation (US/UK)
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| air data
system, flap actuation system |
|
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| skin
composite materials (produced
in France) |
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| Meggitt
Safety Systems
(US) |
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| TP400-D6
nacelle air door actuators,
fire detection system |
|
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| primary
flight control servoactuators
|
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| cockpit
transparencies, landing
and taxi light lenses |
|
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| HF-9500
high-frequency communications
system, avionics full duplex
ethernet (ADFX), avionics
communications router (ACR) |
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This information
is reproduced from the EU Defence
Industry market report. Click
here for further information and
to purchase online.
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