Full Authority Digital Engine Control (FADEC) FADEC = ECU or EEC + HMU or FMU With more than 25 years experience, BAE Systems is a world leader in the design, development, and production of FAE!s" FAE!s" We#re We#re a preferred prefe rred supplier to $E and have an installed %ase of 25,&&& engines" We offer comprehensive overhaul programs designed to extend the life of FAE!s" FAE!s"
A Rich Heritage
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'ore than 25 years experience designing and certifying FAE! FAE! for commercial and military aircraft An installed %ase of more than 25,&&& engines
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FAE! FAE! (nternational )oint venture with Sagem
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FAE! FAE! Alliance partnership with $E and Sagem
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Benefits •
Electronic management of essential power systems for optimi*ed engine performance Efficient engine status monitoring minimi*es fleet disruptions
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'ulti+generation product family approach
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Aftermaret service and support with a trusted -E' through our FAE! FAE! overhaul program
FADEC Proucts (clic! each for etails)
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FAE! . •
FAE! 2
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FAE! / •
!F/0 FAE!
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1EA FAE!
FADEC "
(ntroduced in .34, the evolution of our FAE! FAE! engine controls %egan with the development of the FAE! FAE! . 6 designed to accommodate multiple Boeing and Air%us commercial platforms" 7he FAE! FAE! . is manufactured and supported %y FAE! FAE! (nternational, a )oint venture %etween BAE Systems and Sagem"
Engine Moels •
!F+4&!2 !F'5+5A
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!F'5+5B
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Aircraft Aircraft #u$$orte • •
Boeing 808, 88 'connell ouglas '..
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FADEC %
(ntroduced in .343, our FAE! FAE! 2 models were %uilt for %oth narrow and wide+%ody aircraft manufactured %y Boeing and Air%us"
7he FAE! FAE! 2 is produced and supported %y FAE! FAE! (nternational, a )oint venture %etween BAE Systems and Sagem"
Engine Moels •
$E3&+30B !F+4&E2
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!F'5+8B
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!F'5+5!
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Aircraft Aircraft #u$$orte • •
Boeing 8/8, 888 Air%us A//&, A/0&
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FADEC &
7he FAE! FAE! / was developed to support %oth commercial and military platforms" 7he first FAE! FAE! / was introduced in 2&&& %ut has had additional products developed, in 2&&4, 2&.., 2&.., and 2&.2" 7he FAE! FAE! / is manufactured and supported %y FAE! FAE! (nternational, a )oint venture %etween BAE Systems and Sagem"
Engine Moels •
$E3&+..5 !F'5+8B
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!F+4&1 .F
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$Enx+.B
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$Enx+2B
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$82&&
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Aircraft Aircraft #u$$orte •
Air%us A/4& Boeing 8/89$, 808+4&&, 888, 848
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1ocheed 'artin !5
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CF&' FADEC
-ur !F/0 FAE! FAE! units are installed insta lled on regional aircraft airc raft manufactured %y Bom%ardier and Em%raer" 7his 7his FAE! is produced and supported %y BAE Systems"
Engine Moels •
!F/0+4! !F/0+4E
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!F/0+.&E
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Aircraft Aircraft #u$$orte • •
Bom%ardier !:; 8&&, 3&&, .&&& Em%raer .3&, .35
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EAP EAP FADEC FADEC
!oming in 2&. 6 the newest evolution of the FAE! FAE! 6 the 1EA family of engine controls" 7hese FAE!s FAE!s are %eing produced for f or commercial aircraft now in development from Air%us, Boeing, Bom%ardier, and !-'A!" 1EA FAE!s FAE!s are designed and %uilt %y FAE! Alliance Alliance 6 a partnership %etween $E, BAE Systems, and Sagem"
Engine Moels •
1EA+.A
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1EA+.B
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1EA+.!
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assport
Aircraft Aircraft #u$$orte •
Air%us /2&neo Boeing 8/8'A<
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Bom%ardier $lo%al 8&&& and 4&&&
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!-'A! !3.3
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Flight Controls
With more than /& years of experience 6 and an installed %ase of .5,&&& aircraft 6 we#re a maret leader in the design, development, and production of Flight !ontrol Systems =F!S> for commercial aircraft" We were the first to introduce Fly+By+Wire =FBW> in civil applications with the Air%us /.& aircraft"
ur Flight Control Portfolio •
rimary Flight !ontrol =Fly+By+Wi = Fly+By+Wire re ?FBW?> Secondary@Slats and Flaps =igh 1ift> Flight !ontrols and 'onitoring
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Actuator !ontrol Electronics
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:emote Electronics nits
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:udder and Caw !ontrol
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Sta%ili*er !ontrol and 'onitoring
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Spoiler !ontrol Electronics and 'onitoring
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Active (nceptor Systems
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#u$$orte Aircraft •
Air%usD A/2& BoeingD 8/8, 808, 88, 888, and 808+4 =in production>
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Bom%ardierD !:; and !Series
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Em%raerD 1egacy 0&&@5&& and !+/3& =in development>
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'itsu%ishiD ':;
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earn *ore aout our Flight Control Proucts (clic! each for etails) •
rimary Flight !ontrol !omputers
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Active !ontrol Sidestics •
Slat Flap Electronic !ontrol nit
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Actuator !ontrol Electronics •
:emote Electronics nits
Pri*ary Flight Control Co*$uters
WeGre proud to offer a portfolio of stic+to+surface flight control avionics designed with WeGre performance and safety in mind"
Ca$ailities •
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7he rimary Flight !ontrol !omputers =F!!> 6 sometimes referred to as rimary Flight !ontrol Electronics =F!E> 6 are located in the aircraft electronic eHuipment =EE+Bay> 9ormally three F!!s are installed on an airplane 7he F!! computes and transmits all normal mode primary flight control surface actuator commands =rudder, elevators, ailerons, flaperons, and hori*ontal sta%ili*er as well as the multi+functional spoilers and ground spoilers> to control and maintain normal flight for use %y the Actuator !ontrol Electronics =A!E> F!!s are designed to provide full flight functions 7he F!! performs pre+flight functions to verify the electronics dispatch integrity as well as ground maintenance functions
Data ,nterface Ca$ailities •
A:(9! gateways ata concentration and distri%ution
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Flight data acHuisition
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Acti-e Control #iestic!s
-ur Active !ontrol Sidestics =A!S> 6 also called c alled Active (nceptor Systems =A(S> 6 provide pilots with the tactile cues they want, giving them the ultimate in situational awareness and control while flying the aircraft"
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Ena%les the future integration of flight control functions tili*es position sensing and smart actuation =rather than springs and dampers, as in a passive stic or inceptor> to change forces felt %y the pilot in real time Force feed%ac can %e used to provide cues, warn of mode engagements or impending flight envelop limits
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7he associated gradients and stops are fully programma%le in real time
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7he varia%le feel can also cater for a wide pilot range
Benefits •
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A%ility to lin controls across the cocpit so that each pilot can feel the forces and see the displacements generated %y each other -ffers significant weight and volume savings over mechanical controls
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#lat . Fla$ Electronic Electronic Control Units
Slat Flap Electronic !ontrol nits =SFE!> are also referred to as igh 1ift or Secondary Flight !ontrols" 7hese units limit tae+off and landing speeds %y increasing wing high lift"
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7he SFE! is installed in the eHuipment %ays in the %ody of the aircraft 7he SFE! controls the slats and flaps =on the wings> that are utili*ed during tae+ offs and landings 7he primary purpose of the slats and flaps is to mae the area of the wing %igger, thus ena%ling the aircraft to fly slower 7he slats and flaps do not mae the aircraft fly slower, they increase lift which ena%les the pilot to control the speed 7he slats and flaps are extended and retracted, whereas the spoilers are raised and lowered
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Actuator Control Electronics
Actuator !ontrol Electronics =A!E> are part of the flight+critical and essential Fly+By+Wire =FBW> system" Actuators have one purpose 6 they move something" 7hey may rotate an o%)ect, open or close a device, or push a surface up or down, %ut they always put something into motion"
Ca$ailities •
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7he Actuator !ontrol Electronics are located in the aircraft electronic eHuipment %ay =EE+Bay> A!Es either directly control or indirectly control =via :emote Electronics nits> the aircraft#s primary flight+critical surface =rudder, elevators, ailerons, flaperons, and hori*ontal sta%ili*ers> as well as the multi+functional spoilers and ground spoilers to control and maintain normal flight 7he A!Es A!Es wor in con)unction with the rimary Flight !ontrol !omputers =F!!s> to provide all aspects of normal flight control modes and handling handling Hualities
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Re*ote Electronics Units
:emote Electronics nits =:E> are distri%uted electronics that reside close to or are mounted on the actuator to provide local control of the actuator" 7he :E receives commands and processes incoming and outgoing signals for the functions functions necessary to control the actuators"
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Each :E controls two hydraulic actuators and one electro+mechanical channelI in the event of a flight control computer failure, the :Es tae over primary control of the aircraft surfaces 7he :Es area a dual lane, control+monitor design that ensures integrity of the actuator command Based on the platform flight control architecture, there are up to .. :Es per aircraft :Es weigh approximately four pounds and have %een designed for non+pressuri*ed in+wing applications
