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Computer used for engine control in aerospace engineering
In aviation, a full authority digital engine (or electronics) control (FADEC) (/ˈfeɪdɛk/) is a system consisting of a digital computer, called an "electronic
FADEC
American piston aircraft engine
in 1983 and the type remains in production. The IOF-550 is an Aerosance FADEC equipped version of the same basic engine, the TSIO-550 is a dual turbocharged
Continental_IO-550
Helicopter crash in Scotland
replaced due to a FADEC incident.[clarification needed] Five days later, that same engine had to be replaced due to a second FADEC incident. On 10 May
1994 Mull of Kintyre Chinook crash
1994_Mull_of_Kintyre_Chinook_crash
Turbofan aircraft engine family
F404-GE-102 turbofan engine with Full Authority Digital Engine Control (FADEC) system; the engine is similar to the F404-402, but with additional redundancies
General_Electric_F404
Gas turbine phenomenon
electronic control systems such as full authority digital engine control (FADEC). Modern compressors are carefully designed and controlled to avoid or limit
Compressor_stall
Series of Diesel cycle aircraft engines for general aviation
control (SLPC) associated with a full authority digital engine control (FADEC). This simplifies engine management for the pilot, as well as improving
Thielert_Centurion
Regional jet airliner family
engines are controlled by a dual Full Authority Digital Engine Controls (FADEC) arrangement, which is capable of controlling virtually all aspects of the
Embraer_ERJ_family
Small utility helicopter
on the Bo 108 included the first full-authority digital engine controls (FADEC) on a helicopter, a hingeless main rotor, and the adoption of a new transmission
Eurocopter_EC135
1990s Russian turbofan aircraft engine
treated exhaust duct for low noise Full-authority digital engine control (FADEC) Long service life based on on-condition maintenance Modular design for
Aviadvigatel_PS-90
2025 aviation accident in India
seconds after that. Each engine's full authority digital engine control (FADEC) then automatically attempted to restart them. About 9 seconds after the
Air_India_Flight_171
Network protocol for automation
in power generation, environmental and flight controls. TTP is used in FADEC and modular aerospace controls, and flight computers. In addition, TTP devices
Time-Triggered_Protocol
Electronic flight control system
commonly feature computerized Full-Authority Digital Engine Control systems (FADECs) that control their engines, air inlets, fuel storage and distribution system
Fly-by-wire
Franco–American turbofan aircraft engine
that provides information to the full authority digital engine controller (FADEC). In 1989, CFMI began work on a new, double-annular combustor. Instead of
CFM_International_CFM56
Small turbofan engine
turbine, a new full length bypass duct/exhaust mixer and a dual channel FADEC. FJ44-1C 1,500 lbf (6.7 kN) thrust, derated version of the FJ44-1A, SFC
Williams_FJ44
Turboprop engine model
ratio, variable stator vanes, cooled turbine blades, 3D printed parts and FADEC. After introducing the General Electric H80 in 2010 to improve the Walter
General_Electric_Catalyst
Aircraft Engines
Sukhoi Superjet 100. Snecma is in charge of the core engine, control system (FADEC), transmissions (accessory gearbox, transfer gearbox), overall engine integration
PowerJet_SaM146
Control system for gas turbine engines
hydromechanical fuel control. Full-authority digital engine control (FADEC): A gas turbine with FADEC uses a digital computer which uses the engine's operating conditions
Fuel_control_unit
Series of high-bypass turbofan aero engines
dual-channel full authority digital engine control (FADEC) system. It was certified in 1984 as the first civilian FADEC-controlled aviation engine. MTU Aero Engines
Pratt_&_Whitney_PW2000
1970s American aircraft piston engine
IOF-240 is similar to the IO-240-B except that it employs an Aerosance FADEC system to control the ignition and fuel injection systems. The engine was
Continental_O-240
American multi-role fighter aircraft
tanks; AN/APG-80 AESA radar, General Electric F110-GE-132A engine with FADEC controls; electronic warfare suite and infrared search and track (IRST)
General Dynamics F-16 Fighting Falcon
General_Dynamics_F-16_Fighting_Falcon
Military utility helicopter model by Boeing
maintenance at the operational level. The helicopter is propelled by two FADEC-controlled Pratt & Whitney Canada PT6 turboshaft engines, housed in separate
Boeing_MH-139_Grey_Wolf
Military medium-lift helicopter
cabin, which feature a dual-channel full authority digital engine control (FADEC) system. They can be fitted with an anti-icing system to enable the aircraft
Eurocopter_EC725
American low-bypass turbofan engine for the F-22 Raptor
thrust. The F119 has dual-redundant full authority digital engine control (FADEC), also referred to internally as Digital Electronic Engine Control (DEEC)
Pratt_&_Whitney_F119
American medium-size commercial utility helicopter
production; it was equipped with twin Turbomeca Arriel 2S1 engines with FADEC and a Honeywell EFIS suite. This version also incorporated active noise
Sikorsky_S-76
Indian national defence laboratory
invariably configured with a Full Authority Digital Engine Control (FADEC) system. The FADEC takes the input in terms of the thrust demand based on the current
Combat Aircraft Systems Development & Integration Centre
Combat_Aircraft_Systems_Development_&_Integration_Centre
Military turboprop engine
issue, resulting in a FADEC system consisting of over 275,000 lines of code, which was four times more complex than the FADEC software for the largest
Europrop_TP400
Light business jet
turbofans. With the same airframe, it has Pro Line 21 avionics package and FADEC engine control. It was certified in 2005. The GE Honda HF120 engine was
Cessna_CitationJet/M2
Italian light aircraft
equipped with a 170 hp Continental CD-170 Jet-A diesel engine, featuring FADEC (Full Authority Digital Engine Control), single-lever operation, and turbocharging
Tecnam_P2010
Medium utility helicopter
two 1,325 kW (1,775 shp) class, Full Authority Digital Engine Control (FADEC)-equipped Pratt & Whitney Canada PT6C-67E turboshaft engines, which provide
Airbus_Helicopters_H175
Light utility multipurpose helicopter
rotor (ducted fan), more powerful engines, FADEC, and enhanced avionics. The B model has a fully automated FADEC for engine control, which reduces the possibility
Eurocopter_UH-72_Lakota
High-thrust turbofan jet engine
Combustor Single annular Twin Annulus Premixing Swirler Control dual channel FADEC Compressor 1 fan, 3-stage LP, 11-stage HP Turbine 2-stage HP, 6-stage LP
General_Electric_GE9X
Multi-role helicopter family by Aérospatiale
Turbomeca Arriel turboshaft engines; on later variants, these are equipped with FADEC units, which provide additional functionality such as an automated start-up
Eurocopter_AS365_Dauphin
Chinese fighter turbofan engine
(27,000–31,000 lbf) thrust. It has full authority digital engine control (FADEC). The WS-10 is reverse engineered from the CFM56 with the experience gained
Shenyang_WS-10
Very light jet in Austria
been automated and are seamlessly performed by the FADEC system. For redundancy, the dual-channel FADEC system uses four independent electrical power sources
Diamond_D-Jet
Family of single engine turboprop aircraft
associated with managing the PT6A engine, it is not as capable as a full FADEC arrangement. The cockpit design of the TBM strives to be user-friendly and
SOCATA_TBM
Regional jet airliner family
6 kN). The engines are equipped with full authority digital engine control (FADEC). The fully redundant, computerized management system continuously optimizes
Embraer_E-Jet_family
Family of private twinjet aircraft manufactured by Gulfstream Aerospace
relocated aft. The Rolls-Royce Tay 611 engines are replaced by 611-8Cs with FADEC, redesigned thrust reversers, nacelles and pylons which increases range
Gulfstream_IV
American stealth air superiority fighter
dual-redundant Hamilton Standard full-authority digital engine control (FADEC) and maximum thrust in the 35,000 lbf (156 kN) class. The F-22's thrust-to-weight
Lockheed_Martin_F-22_Raptor
Franco-Italian Aircraft manufacturer
thermal de-icing to replace the current pneumatic boots, a single lever FADEC for both engine and propeller and an aerodynamic clean-up of the secondary
ATR_(aircraft_manufacturer)
Aircraft engine operating on the Diesel principle
common rail direct injection, turbocharger, 1:1.4138 reduction gearbox and FADEC producing 81 kW (109 hp) at takeoff at 3675 rpm and 66 kW (89 hp) continuously
Aircraft_diesel_engine
Aircraft engine
component improvements, including a full authority digital engine control (FADEC), that allowed maximum thrust to be achieved in a wider range of conditions
General_Electric_F110
string Propulsion controls, devices and fuel systems Autothrottle Drop tank FADEC Fuel tank Gascolator Inlet cone Intake ramp NACA cowling NACA duct Self-sealing
Dual_control_(aviation)
Turbofan aircraft engine family
The accessory gearbox is mounted at its bottom and two single channel FADEC units are mounted in the aircraft. It has fore and aft mounting provisions
Rolls-Royce_AE_3007
Russian fighter aircraft engine
MiG-35. The RD-33MK develops 7% higher thrust, is digitally controlled FADEC and smokeless unlike earlier RD-33 engines, has increased afterburner thrust
Klimov_RD-33
Canadian series of aircraft engines
needed] Hispano-Suiza Canada designed and manufactures the dual channel FADEC.[citation needed] PW610F PW615F PW617F Cessna Citation Mustang Eclipse 400
Pratt_&_Whitney_Canada_PW600
Nautical terms for direction
string Propulsion controls, devices and fuel systems Autothrottle Drop tank FADEC Fuel tank Gascolator Inlet cone Intake ramp NACA cowling NACA duct Self-sealing
Port_and_starboard
Flight instrument which displays the aircraft's orientation relative to Earth's horizon
string Propulsion controls, devices and fuel systems Autothrottle Drop tank FADEC Fuel tank Gascolator Inlet cone Intake ramp NACA cowling NACA duct Self-sealing
Attitude_indicator
Largest Civilian Rotorcraft Manufactured by Airbus Helicopters
engine control (FADEC) system for high reliability, a further backup system is present in the event of both FADEC systems failing. The FADEC system ensures
Eurocopter_EC225_Super_Puma
High-bypass turbofan aircraft engine
initially consisted of the hydromechanically controlled LF 507-1H and the FADEC-controlled LF 507-1F, both offering 7,000 lbf (31 kN) of thrust. Both variants
Lycoming_ALF_502
Engine where combustion is pulsed instead of continuous
Engine controls Autothrottle Full Authority Digital Engine/Electronics (FADEC) Thrust lever Thrust reversal Fuel and induction systems Flame holder Jet
Pulsejet
Austrian light aircraft
avgas-powered version of the DA50 was intended to be equipped with a single FADEC-equipped Continental TSIO-550-J powerplant with twin turbo chargers producing
Diamond_DA50
Network security measure
as: Controls of nuclear power plants; Computers used in aviation, such as FADECs, air traffic control systems, and avionics; Computerized medical equipment;
Air_gap_(networking)
the aircraft themselves and grew steadily in sophistication. The first FADEC (Full Authority Digital Engine Control) trials took place in 1968, with
Aviation_in_the_Digital_Age
Instrument used for navigation and orientation
string Propulsion controls, devices and fuel systems Autothrottle Drop tank FADEC Fuel tank Gascolator Inlet cone Intake ramp NACA cowling NACA duct Self-sealing
Compass
Shock-induced combustion ramjet engine
Engine controls Autothrottle Full Authority Digital Engine/Electronics (FADEC) Thrust lever Thrust reversal Fuel and induction systems Flame holder Jet
Shcramjet
Aircraft term
(which includes airplanes with constant-speed propellers and airplanes with FADEC which controls both the engine and propeller; turbojet and turbofan airplanes
Complex_airplane
Regional airliner prototype
crew alerting system (EICAS), and full authority digital engine control (FADEC), which are vulnerable to lightning and high-intensity radiated fields (HIRF)
Embraer/FMA_CBA_123_Vector
2026 French light helicopter
is equipped with a dual-channel full authority digital engine control (FADEC) system, the latter feature is intended to reduce the pilot's workload.
Guimbal_Cabri_G5
Passenger transport helicopter
engines which feature a dual-channel Full Authority Digital Engine Control (FADEC) system. The EC155 B1 features uprated 697 kW (935 shp) Arriel 2C2s. The
Eurocopter_EC155
Aerial service branch of the Chinese People's Liberation Army
engines, advanced aerospace materials, full authority digital engine control (FADEC), integrated avionics, missile technologies, and active electronically scanned
People's Liberation Army Air Force
People's_Liberation_Army_Air_Force
Turbofan jet engine developed in the 1960s
and LP turbines, and introduces Full Authority Digital Engine Control (FADEC).[citation needed] The Mk 951 was certified in 2005. F405-RR-402 - Upgrade
Rolls-Royce_Turbomeca_Adour
American kit helicopter
safety. In 1994, a fuel injection system with electronic ignition, and FADEC was added to the Exec 90, producing the Exec 162F. Unlike most U.S.-designed
RotorWay_Exec
authority digital engine control (FADEC) system prevents such a condition from occurring. In engines without FADEC, the flight crew has to monitor the
Hot_start
Belgian aircraft engine manufacturer
application. The new engine should have the following aims and objectives: FADEC, simple, robust, easy to maintain, low parts count, high power to weight
ULPower_Aero_Engines
Business jet aircraft
conditions, while normal cruise speed is Mach 0.76 436 kn (807 km/h) TAS. The FADEC-controlled 4,600 lbf (20 kN) PW305A turbofans have a 6,000 hour TBO, reserves
Learjet_60
Multinational engine manufacturer
Tiger delivery to Germany followed on 6 April 2005. The MTU390 itself is a FADEC-controlled turboshaft engine; each Tiger helicopter is powered by a pair
MTU_Turbomeca_Rolls-Royce
Family of South Korean jet aircraft
equipped with a GE F404 engine with Full Authority Digital Engine Control (FADEC) built under license by Samsung Techwin. Under the terms of the T-50/F404-102
KAI_T-50_Golden_Eagle
Single engine series of the Ecureuil light helicopter family
use of digital systems, such as the Garmin-built G500H avionics suite and FADEC engine control system. Prior to 2013, the type had been manufactured principally
Eurocopter_AS350_Écureuil
Business jet made by Bombardier Aviation
July 2019, after five years of service. Hot-section modifications and a FADEC push gave the Honeywell HTF7350 7.3% more takeoff thrust at 7,323 lbf (32
Bombardier_Challenger_300
Sino-Pakistani multirole fighter aircraft
lbf) thrust with afterburner) with Full Authority Digital Engine Control (FADEC) (previous engine: 1 x Klimov RD-93 afterburning turbofan (84.4 kN (18,974
CAC/PAC_JF-17_Thunder
Very light business jet
ISA+10 °C. These engines have dual full authority digital engine controls (FADEC). In the event of a single engine failure during takeoff, an automatic performance
Embraer_Phenom_100
Small business jet delivered by Cessna between 1989 and 2011
amounted to 65. It was certified by the FAA in December 2006. The Encore+ adds FADEC and Rockwell Collins Pro Line 21 avionics with a center MFD and both side
Cessna_Citation_V
French aerospace and defence company
and electrical harnesses for the LEAP engine, Rafale jets, Falcon 10X and FADEC, respectively. Additionally, Safran plans to establish a new subsidiary
Safran
Medium to transfer power in hydraulic machinery
string Propulsion controls, devices and fuel systems Autothrottle Drop tank FADEC Fuel tank Gascolator Inlet cone Intake ramp NACA cowling NACA duct Self-sealing
Hydraulic_fluid
High-bypass turbofan engine
low pressure: 5,650 RPM, high pressure: 14,950 RPM Control: Dual channel FADEC Comparable engines CFM International CFM56 Pratt & Whitney PW6000 Related
IAE_V2500
Turbofan engines in Canada
rated at 3,478 lbf (15.47 kN)/ Unveiled at the May 2023 EBACE show, the FADEC-controlled PW545D is developed for the Cessna 560XL Ascend variant, to be
Pratt_&_Whitney_Canada_PW500
Family of turbofan engines used by the Soviet military
temperatures. The AL-31FM2 has a new full authority digital engine control (FADEC) with a hydromechanical backup. Thrust was increased 9% across the envelope
Saturn_AL-31
Russian turbofan engine
in afterburner. The AL-51F-1 has full authority digital engine control (FADEC) to ensure its reliability in various operating conditions. Sukhoi Su-57M
Saturn_AL-51
Long-range, large business jet
thrust, a higher bypass ratio, and Full Authority Digital Engine Controls (FADEC). Operating ceiling increased from 45,000 to 51,000 ft (14,000 to 16,000 m)
Gulfstream_V
Jet engine
systems. The 1996 development of a 50W full authority digital engine control (FADEC) system, with a mechanical calculator as a seamless backup. A completely
Volvo_RM12
Aircraft cockpit with electronic displays
Engine controls Autothrottle Full Authority Digital Engine/Electronics (FADEC) Thrust lever Thrust reversal Fuel and induction systems Flame holder Jet
Glass_cockpit
Four cylinder piston aircraft engine
announced the 912 iS variant, a 75 kW (100 hp) version with fuel injection and FADEC, with ECUs supplied by Rockwell Collins. The version weighs 63 kg (139 lb)
Rotax_912
Entertainment available to aircraft passengers during a flight
string Propulsion controls, devices and fuel systems Autothrottle Drop tank FADEC Fuel tank Gascolator Inlet cone Intake ramp NACA cowling NACA duct Self-sealing
In-flight_entertainment
South Korean utility helicopter
common core, high-efficiency counter-rotating power turbine, and a new FADEC system. The exhausts of the engines are equipped with large infrared suppressors
KAI_KUH-1_Surion
1960s British turbofan aircraft engine
already present on the -535E4. These were the first versions to feature FADEC. This was later adopted by GE and Pratt & Whitney for their engines. The
Rolls-Royce_RB211
Military utility helicopter
turboshafts, which are equipped with full authority digital engine control (FADEC). The main missions of this version are transport of 8 to 10 fully equipped
Eurocopter_AS565_Panther
Medium-bypass turbofan aircraft engine
turbine blades, larger fan from the 650-15, structural by-pass duct and FADEC. All Tay engines use a 22-blade titanium fan, a 3-stage intermediate-pressure
Rolls-Royce_RB.183_Tay
Twin-engine light utility helicopter
AW139. The AW169 is powered by a pair of Pratt & Whitney Canada PW210A FADEC turboshaft engines, which drives the main rotor at variable speeds to reduce
AgustaWestland_AW169
Aircraft flight instrument
string Propulsion controls, devices and fuel systems Autothrottle Drop tank FADEC Fuel tank Gascolator Inlet cone Intake ramp NACA cowling NACA duct Self-sealing
Turn_and_slip_indicator
Small single-aisle airliner
by an electronic engine system (Full Authority Digital Engine Control — FADEC) developed by BAE Systems, offering improved controllability and optimization
Boeing_717
Civil 7-seat utility helicopter
HTS900 turboshaft engine, producing 970 shp (720 kW) and includes full FADEC controls. The cabin sat five passengers in club-seating configuration, in
Bell_407
Utility helicopter
is powered by two Pratt & Whitney Canada PW207D turboshaft engines with FADEC. Like the Bell 407, the 427 uses a four-blade main rotor system with a rigid
Bell_427
Family of turboshaft engines by Pratt & Whitney Canada
Lower fuel consumption, Dual Channel Full Authority Digital Engine Control (FADEC), Reduced environmental emissions and an Increase in power output ranging
Pratt_&_Whitney_Canada_PW200
Aircraft turbofan jet engine
is controlled with a dual channel Full Authority Digital Engine Control (FADEC) system. The PW307A is a new centre-line engine developed specifically for
Pratt_&_Whitney_Canada_PW300
2000s British turbofan aircraft engine
high-pressure compressor drum, as well as an upgrade to the engine control (FADEC) software. The EP2 package entered testing in May 2013 and was scheduled
Rolls-Royce_Trent_900
Gas turbine used to spin a shaft
Engine controls Autothrottle Full Authority Digital Engine/Electronics (FADEC) Thrust lever Thrust reversal Fuel and induction systems Flame holder Jet
Turboshaft
2010s Japanese turbofan aircraft engine
is a twin-spool axial-flow afterburning turbofan with a dual redundant FADEC, consisting of a 3-stage fan, a 6-stage high-pressure compressor, an annular
IHI_Corporation_XF9
Aircraft control surface that combines the functions of both flaps and ailerons
string Propulsion controls, devices and fuel systems Autothrottle Drop tank FADEC Fuel tank Gascolator Inlet cone Intake ramp NACA cowling NACA duct Self-sealing
Flaperon
System to limit ice on aircraft surfaces
string Propulsion controls, devices and fuel systems Autothrottle Drop tank FADEC Fuel tank Gascolator Inlet cone Intake ramp NACA cowling NACA duct Self-sealing
Ice_protection_system
Soviet turbofan engine
and new compressor sections. Several variants of the engine incorporate a FADEC. The Motor-Sich plant in Zaporozhie, where the assembly line for D-436 engines
Progress_D-436
FADEC
FADEC
FADEC
FADEC
Male
Hebrew
(עָכָר) Variant form of Hebrew Akan, AKAR means "one who troubles." In the bible, this is the name of an Israelite who stole forbidden items during the assault on Jericho, for which he was stoned to death.Â
Girl/Female
Hindu
Goddess of good wishes
Boy/Male
Tamil
Ever smiling
Boy/Male
Muslim
Slave of the giver
Female
Dutch
, everlasting, or, ever-living.
Boy/Male
Tamil
The Moon
Boy/Male
Bengali, Hindu, Indian, Tamil
Name of the Chola King; Soldier
Girl/Female
Indian, Sikh
Loyal
Male
Celtic
, (the Lord); Apollo, Jupiter.
Boy/Male
Indian, Sanskrit
Divine
FADEC
FADEC
FADEC
FADEC
FADEC