Named product lines from the aerospace manufacturing supply chain — who makes them, and the aircraft programs they fly on. Listings grow as suppliers confirm their catalogues.
541 products · page 9 of 11
Flight Display System (SV-HDX Series) available as 7"/10" touchscreen PFD (SV-HDX800/1100) for type certified aircraft and 12" PFD option for exper…
8300 kgf thrust, twin-shaft, turbojet engine, modified RD-33 with lower engine box and increased length
160 N thrust, micro gas turbine, turbojet engine with automatic starting capability for high speed UAS
HUD for fixed-wing aircraft.
HUD for fixed-wing aircraft.
Mach 5-12, green hydrogen-powered, reusable, ceramic matrix composite, 3D-printed, scramjet engine
Family of military UAS turbojet engines, developed by Kratos' subsidiary Technical Directions Inc., with multi-fuel capability and modular exhaust …
Low-bypass engine, intended for civilian jet airliners but also used in various military applications
Single-screen EFIS system, with split-screen capability to display map, HSI, and EMS on PFD, or button to switch between screens. Features optional…
Auxiliary Power Units that provide electric and pneumatic power for business jets whilst in-flight/on-ground, and with updated FADEC offering in-fl…
230 hp, four-cylinder, turbocharged, compression ignition, piston diesel engine
50 hp, 2-stroke, electric ignition & starter piston engine, originally designed for trikes.
Includes T407-GE-400, T408-GE-400 (GE38-1B), GE38-3, and contra-rotating UDF GE38-B5
Helicopter engine, previously Lycoming T53
Formerly Lycoming; company designation LTC-4, for helicopters
Small gas turbine, used mainly as a helicopter auxiliary power unit (APU), ground power generator, turboprop engine or helicopter turboshaft engine
Free-turbine turboshaft engines orignially designed for (often military) helicopters
Military variants of CT7 engines
South Korean variant of T700 turboshaft engine, developed by Hanwha Aerospace and GE, made under license by Hanwha.
Japanese T700-201C2, manufactured by IHI, military turboshaft engine
GE Aviation's T700-GE-701D engines' designation when made in Turkey
Military turboshaft engines, designed by LHTEC - a joint venture between Rolls Royce and Honeywell
3000 shp, dual-spool, turboshaft engine developed for the United States Army's Improved Turbine Engine Program
Gas turbine Auxiliary Power Unit capable of providing pneumatic and electrical power (20-40 kVA).
New generation Auxiliary Power Unit with electronic control, provides pneumatic and electrical power (60 kVA) for main engine starting, on-board po…
New generation Auxiliary Power Unit with electronic control, provides pneumatic and electrical power for main engine starting, on-board power, and …
125 hp, four-cylinder, four-stroke, piston diesel engine, diesel variant of the CD-135 (Centurion 1.7) family
98-115 hp, two-cylinder, four-stroke, air-cooled, piston engine with spur gear and centrifugal clutch
Turkish built LHTEC CST800 engines
Military turbofan engine with 35,000 lbf thrust and low fuel consumption, developed in partnership with TRMOTOR. In development.
First indigenous turbofan engine with 6,000 lbf thrust, includes 10,000 lbf after-burning variant TEI-TF10000
440 hp, eight-cylinder, direct-injection, piston diesel engine
1200 lbf thrust, axial and diagonal single-stage fan-compressor, rotor driven, two-stage turbine, direct flux annular combustion chamber, turbofan …
300 lbf thrust, diagonal single-stage fan-compressor, rotor driven, two-stage turbine, direct flux annular combustion chamber, turbofan engine
700 lbf thrust, axial and diagonal single-stage fan-compressor, rotor driven, two-stage turbine, direct flux annular combustion chamber, turbofan e…
Geared turbofan engines for business jets
55-90 kW power, turbogenerator, hybrid-electric engines
Integrated Electronic Standby Instrument with LED backlighting, LCD screen, and enhanced graphics/symbology in 3-ATI unit; for airliner, helicopter…
1627 kw peak power, direct drive, turn-key integrated, ultra-high efficiency, all-electric jet engine with 600 km range
The Wright Propulsion System includes a 2 MW motor, Wright inverters, and thermal management system
29 hp, single-cylinder, two-stroke, air-cooled piston engine series
36 hp, single-cylinder, liquid-cooled, piston engine series with reduced and compact design and electronic/battery ignition