Aero AT-3 |
Analysis |
Radar Transponders: Optional KT 67A Mode C transponder (AT-3 R100) |
Aero Vodochody L-159 |
Analysis |
LCD Displays: Dual LCD multi function displays (L-159T1); Distance Measuring Equipment: KDM 706A DME; Inertial Components & Systems: H-746G ring laser gyro INS wih embedded GPS (L-159T1); IFF Interrogators: AN/APX-100 IFF (L-159T1) |
Aeropro Eurofox |
Analysis |
Electronic Flight Instrument Systems: Optional avionics suite |
AIBOT aiEVTOL |
Analysis |
Fly-by-Wire Systems: |
Air Tractor AT-401B |
Analysis |
Radio Communications Equipment: KX 155 nav/com/glideslope (option) |
Air Tractor AT-502 |
Analysis |
Transceivers: Optional KX 155 nav/com/glideslope; Automatic Direction Finders: Optional KR 87 ADF |
Air Tractor AT-802 |
Analysis |
Transceivers: KX 155A nav/com; KY 99A or KY 196A transceivers; Radar Transponders: KT 76A transponder; Onboard Intercom Systems: KMA 24H audio control panel; GPS: KLX 135 GPS/com; KCS 55A compass; Automatic Direction Finders: KT 87 ADF |
Airbus A220 |
Analysis |
Auxiliary Power Units: 131-9C APU (A220); Flight Recorders: Information Recording System (IRS) (A220); Emergency Locator Transmitters: Emergency locator (A220) |
Airbus A320 |
Analysis |
Auxiliary Power Units: 131-9[A] series APU (A320ceo); Flight Management Systems: Pegasus flight management system (A320ceo); Inertial Components & Systems: Air data inertial reference system (A320ceo); Multi-Mode Receivers (MMR): IMMR Integrated Multi-Mode Receiver option |
Airbus A330 |
Analysis |
Auxiliary Power Units: 331-350 APU; Flight Management Systems: Flight management systems (A330-300); data management unit; Inertial Components & Systems: Air data inertial reference system; Multi-Mode Receivers (MMR): IMMR Integrated Multi-Mode Receiver option |
Airbus A350 |
Analysis |
Auxiliary Power Units: HGT1700 auxiliary power unit, installation kit & starter-generator (A350-900); Airborne Communication Systems: JetWave ka-band satellite connectivity system; Air Conditioning Equipment: Air management system; Flight Management Systems: (A350-900) |
Airbus A380 |
Analysis |
Engine Parts: Pneumatic system for Rolls-Royce Trent 900 Engine & Engine Alliance GP7200 Engine; Air Purification Systems: Cabin air Ozone Converter; Flight Management Systems: Next-generation Flight Management System; Inertial Components & Systems: Air data inertial reference system |
Airbus C295 |
Analysis |
Flight Recorders: Solid state CVR and solid state FDR (C295M); Inertial Components & Systems: Inertial Refernce System (CC-295); Terrain Awareness and Warning Systems: EGPWS (C295M); IFF Interrogators: IFF transponder (C295M) |
Airbus Helicopters AS565 Panther |
Analysis |
Terrain Awareness and Warning Systems: Mk XXII EGPWS (AS365N2) |
Airbus Helicopters H130 |
Analysis |
Radio Communications Equipment: KX 165A VHF/VOR/LOC/GS (EC130 B4); Horizontal Situation Indicator: KI 525 HSI (EC130 B4); GPS: KCS 55A gyro-compass (EC130 B4); Automatic Direction Finders: KR 87 ADF with KI 229 radio magnetic indicator (EC130 B4) |
Airbus Helicopters H145M/EC145 |
Analysis |
Automatic Flight Control Systems: SPZ-7100 dual digital AFCS (EC145); Radar/Radio Altimeters: KRA 405B radar altimeter; Distance Measuring Equipment: DMS 44A; VOR (Omnirange) Receivers: Twin VNS 41A VOR/ILS |
Airbus Helicopters H155 |
Analysis |
Terrain Awareness and Warning Systems: Mk XXII EGPWS (EC155B) |
Airbus Helicopters H175 |
Analysis |
Weather Mapping Radar: Primus 701 weather & search radar |
Airbus Helicopters H215/H225/AS332/AS532 |
Analysis |
Terrain Awareness and Warning Systems: Optional Mk XXII EGPWS (AS332L1) |
American Blimp Lightship A-170 |
Analysis |
Transceivers: Bendix/King Silver Crown range |
American Champion 7GCBC Citabria Explorer |
Analysis |
Transceivers: Optional KR 22 marker beacon receiver |
AMS Carat |
Analysis |
Radar Transponders: |
Antonov An-132 |
Analysis |
Electronic Flight Instrument Systems: Primus Epic 2.0 avionics |
ATR 42/72 |
Analysis |
Air Conditioning Equipment: (42-500); Automatic Flight Control Systems: DFZ 600 AFCS (42-500); Flight Management Systems: FMZ-800 (42-500); Weather Mapping Radar: P-660 weather radar (42-500); weather radar (72-600); Air Data Computers: AZ-800 ADC (42-500); air data computer (72-600); Attitude and Heading Reference Systems: AH-600 AHRS (42-500) |
BAE Systems Hawk 100 |
Analysis |
Attitude and Heading Reference Systems: Mk 1/Srs 50 |
Beechcraft Baron G58 |
Analysis |
Radar/Radio Altimeters: RDR 2000 VP colour weather radar |
Beechcraft Bonanza G36 |
Analysis |
GPS: KN 63 DME |
Beechcraft King Air 250 |
Analysis |
Terrain Awareness and Warning Systems: Mk VII EGPWS |
Beechcraft King Air 350 |
Analysis |
Terrain Awareness and Warning Systems: Mk VIII EGPWS TAWS |
Beechcraft T-6 |
Analysis |
Radar Transponders: MST 67A Mode S transponder; VOR (Omnirange) Receivers: Dual VNS-41 navigation systems for VOR, including VN-411B receivers; GPS: KLN 90 GPS |
Bell 407 |
Analysis |
Radio Communications Equipment: KX 155 & KX 165 nav/com, KY 196A VHF, KT 70 & KY 76A transponder; Automatic Direction Finders: KR 87 ADF; GPS: KLN 89B GPS, KCS 55A compass |
Bell 412EP |
Analysis |
Radar Transponders: KXP 750A transponder; Automatic Flight Control Systems: SPZ-7600 (412EP); Weather Mapping Radar: Primus 700 weather radar; Primus 660 (412EP); Radar/Radio Altimeters: Optional KRA 405B radar altimeter (412EP); Glide Slope Receivers: KGM 690 marker beacon/glideslope receiver; Automatic Direction Finders: KDF 800 ADF (412EP); Distance Measuring Equipment: KMD 700A DME; Distance Measuring Equipment: KDM 706A DME (412EP); Terrain Awareness and Warning Systems: Optional Mark XXI or XXII HTAWS EGPWS (412EP) |
Bell 429 |
Analysis |
Weather Mapping Radar: Optional Primus 660 weather radar (429WLG); Attitude and Heading Reference Systems: KSG-7200 air data attitude heading reference system; Radar/Radio Altimeters: Radar altimeter; Automatic Direction Finders: ADF (option); Terrain Awareness and Warning Systems: Enhanced ground proximity warning system |
Bell 525 Relentless |
Analysis |
Auxiliary Power Units: RE100BR APU; Air Conditioning Equipment: AC-5510 environmental control system |
Bell AH-1Z Viper |
Analysis |
Air Conditioning Equipment: Environmental control unit |
Bell Boeing V-22 Osprey |
Analysis |
Air Conditioning Equipment: Environmental control system (ECS); Electronic Flight Instrument Systems: Enhanced Standby Flight Instruments (ESFI); Weapons Countermeasures: IR emission suppressors |
Blackshape Bk160 Gabriel |
Analysis |
Angle of Attack Indicators: Bendix King (BK200 variant) |
Boeing 737 |
Analysis |
Bleed Air Systems: Bleed air valves; Bleed Air Systems: Electronic Bleed Air System (EBAS) (737 MAX); Radio Communications Equipment: Quantum Line communication/navigation radios; Airborne Communication Systems: SATCOM systems; Precoolers: Pre-cooler control valve; Flight Management Systems: Flight data acquisition & management system; Flight Recorders: Cockpit voice & data recorders; Cockpit Printers: Mark II communications management unit with cockpit printer; Flight Recorders: Honeywell Connected Recorder-25 (HCR-25) cockpit voice recorder (CVR) and flight data recorder (FDR); Air Data Computers: HF/voice/HF data link; Electronic Flight Instrument Systems: Flat-panel LCD displays (737-700; 737-800; 737-600; 737-900); Multi-Mode Receivers (MMR): IMMR Integrated Multi-Mode Receiver option; Emergency Locator Transmitters: ; Terrain Awareness and Warning Systems: EGPWS on BBJ variants |
Boeing 767 |
Analysis |
Air Conditioning Equipment: Dual air cycle air conditioning system; Flight Management Systems: Flight Management Computers (FMCS); Flight Management Systems: Dual digital flight control system, 3x triple control computers, FCS0700 flight control system; Flight Recorders: Honeywell Connected Recorder-25 (HCR-25) cockpit voice recorder (CVR) and flight data recorder (FDR); Electronic Flight Instrument Systems: EFIS-700 flight instrument system; Radar/Radio Altimeters: RMI-743 radio magnetic indicator and radio altimeter; Air Data Computers: Digital Air Data Computer (DADC); VOR (Omnirange) Receivers: VOR/ILS/marker beacon receiver; Inertial Components & Systems: Inertial Reference System (IRS); Automatic Direction Finders: ; Distance Measuring Equipment: |
Boeing 777 |
Analysis |
Auxiliary Power Units: 331-500 APU; Airborne Communication Systems: Satellite Communications (SATCOM) high speed digital voice & data communications; Avionics Management Systems: Airplane Information Management System (AIMS); Flight Recorders: Honeywell Connected Recorder-25 (HCR-25) cockpit voice recorder (CVR) and flight data recorder (FDR); LCD Displays: Flat panel multipurpose colour LCD cockpit display; Multi-Mode Receivers (MMR): IMMR Integrated Multi-Mode Receiver option |
Boeing 787 Dreamliner |
Analysis |
Engine Parts: Engine nacelle anti-ice flow regulator; Flight Management Systems: Flight management system; flight controls; Inertial Components & Systems: Navigation package including inertial reference system, air data system, multi-mode receiver |
Boeing AH-64 Apache |
Analysis |
Fly-by-Wire Systems: Secondary fly-by-wire controls (AH-64D); Auxiliary Power Units: GTP 36-155(BH) APU (AH-64D); Engine Parts: Integrated pneumatic system (AH-64D); Automatic Flight Control Systems: Digital Automatic Stabilisation Equipment (DASE) (AH-64D); Electronic Flight Instrument Systems: Aerial rocket control system; Electronic Flight Instrument Systems: All-raster symbology generator; Flat-panel colour multi-purpose displays (AH-64D); Radar/Radio Altimeters: AN/APN-209 radar altimeter (AH-64D); LCD Displays: Two mulitpurpose displays (MPDs) in each cockpit (AH-64D) |
Boeing CH-47 Chinook |
Analysis |
Radio Communications Equipment: AN/ARC-199 HF com radio (CH-47D); Radar/Radio Altimeters: AN/APN-209 radar altimeter (CH-47D); Electronic Flight Instrument Systems: All-raster symbology generator; Electronic Flight Instrument Systems: EFIS and Advanced Cockpit Management System (ACMS); GPS: AN/ASN-43 gyromagnetic compass (CH-47D); IFF Interrogators: AN/APX-100 IFF (CH-47D) |
Boeing F-15E Strike Eagle |
Analysis |
Auxiliary Power Units: APU; Radio Communications Equipment: AN/APX-101 IFF transponder; Air Conditioning Equipment: Air conditioning system; Air Data Computers: AN/ASK-6 air data computer; Attitude and Heading Reference Systems: AN/ASN-108 AHRS; GPS: RP-341/A remote map reader; Inertial Components & Systems: CN/1655A/ASN ring laser gyro INS |
Boeing F/A-18 Super Hornet |
Analysis |
Auxiliary Power Units: GTC36-200 APU |
Bombardier Challenger 300 series |
Analysis |
Auxiliary Power Units: 36-150BD APU; Inertial Components & Systems: Laseref inertial reference system (Challenger 350) |
Bombardier Challenger 650 |
Analysis |
Air Conditioning Equipment: Air conditioning system; Cabin Pressure Control Systems: ; Inertial Components & Systems: Laseref V inertial reference system |
Bombardier Global series |
Analysis |
Auxiliary Power Units: RE220 GX (Global Express); Airborne Communication Systems: JetWave ka-band satellite connectivity system |
Boom Overture |
Analysis |
Flight Management Systems: Honeywell Anthem integrated flight deck (Overture) |
Cessna 172 Skyhawk |
Analysis |
Radio Communications Equipment: KX 155A nav/com; Autopilots: KAP 140 two-axis autopilot; Automatic Direction Finders: Optional KR 87 ADF |
Cessna 182T Skylane |
Analysis |
Radio Communications Equipment: KX 155A nav/com; Autopilots: KAP 140 two-axis autopilot; Automatic Direction Finders: KR 87 ADF (Option) |
Cessna 206 Stationair |
Analysis |
Radio Communications Equipment: KX 155A nav/com; Autopilots: KAP 140 two-axis autopilot; Electronic Flight Instrument Systems: KMD 550 colour AMLCD Multi-Function Display (Option); Automatic Direction Finders: Optional KR 87 ADF |
Cessna 208 Caravan |
Analysis |
Radio Communications Equipment: KX 165 nav/com/glideslope; Autopilots: KFC 225 flight director/autopilot; Weather Mapping Radar: RDR-200 weather radar; Radar/Radio Altimeters: Optional KRA 405B radar altimeter (Caravan/Grand Caravan EX) |
Cessna Citation 560XL |
Analysis |
Auxiliary Power Units: RE100 APU (Citation XLS+/XLS Gen2); RE100 XL APU (Citation Ascend); Terrain Awareness and Warning Systems: Mark V EGPWS (Citation XLS+/XLS Gen2) |
Cessna Citation CJ4 |
Analysis |
Terrain Awareness and Warning Systems: Optional Mark VIII EGPWS |
Cessna Citation Latitude |
Analysis |
Radio Communications Equipment: HF radios; Air Conditioning Equipment: Environmental control system; Cabin Pressure Control Systems: Digital cabin pressure control & monitoring system; Inertial Components & Systems: LASEREF VI inertial reference navigation systems |
Cessna Citation Longitude |
Analysis |
Auxiliary Power Units: 36-150 APU; Radio Communications Equipment: HF radios; Air Conditioning Equipment: Environmental control system; Cabin Pressure Control Systems: Digital cabin pressure control & monitoring system; Inertial Components & Systems: LASEREF VI inertial reference navigation systems |
Cirrus SR20 |
Analysis |
Terrain Awareness and Warning Systems: KGP-560 EGPWS (GTS model) |
COMAC C909 |
Analysis |
Fly-by-Wire Systems: Fly-by-wire flight control system (ARJ21-700) |
COMAC C919 |
Analysis |
Fly-by-Wire Systems: Fly-by-wire flight control system (C919-200); Auxiliary Power Units: 131-9(C9C) APU derivative HGT750[C]; Starter Generators: Starter/generator system & installation kit; Air Data Computers: Air data system (C919-200); Inertial Components & Systems: LASEREF VI inertial reference system (C919-200) |
Custom Flight North Star Bushplane |
Analysis |
Radio Communications Equipment: KX-125 nav/com; Radar Transponders: KT-76A transponder |
Dassault 2000 series |
Analysis |
Auxiliary Power Units: 36-150 APU; GTCP36-150F2M APU (2000); Airborne Communication Systems: JetWave ka-band satellite connectivity system (2000); Enhanced Vision Systems (EVS): SmartView synthetic vision system (2000); LCD Displays: Four 358 mm LCDs (2000) |
Dassault 7X |
Analysis |
Bleed Air Systems: Bleed air system; Auxiliary Power Units: 36-150F2M APU & engine starting system; Radio Communications Equipment: MCS-7120 satellite communications system; Airborne Communication Systems: JetWave ka-band satellite connectivity system; Air Conditioning Equipment: Air management system; Avionics Management Systems: Primus Epic avionics system (in EASy flight deck) |
Dassault 8X |
Analysis |
Airborne Communication Systems: JetWave ka-band satellite connectivity system; Avionics Management Systems: Primus Epic System (for the EASy Flight Deck); Weather Mapping Radar: RDR-4000 weather radar |
Dassault 900LX |
Analysis |
Auxiliary Power Units: 36-150 APU; GTCP36-150 APU (900C); Airborne Communication Systems: JetWave ka-band satellite connectivity system (900C); Avionics Management Systems: Primus 2000 EFIS avionics suite (900C/EX); EASy II avionics suite (900C/EASy/LX); Flight Management Systems: FMZ-2000 (900EX); Weather Mapping Radar: Primus weather mapping radar (900EX); Inertial Components & Systems: Laseref III inertial reference system (900EX); Terrain Awareness and Warning Systems: EGPWS (900EX) |
Dassault Falcon 10X |
Analysis |
Auxiliary Power Units: HGT400 Auxiliary Power Unit (APU); Avionics Management Systems: Primus Epic avionics system; Enhanced Vision Systems (EVS): Enhanced SmartView synthetic vision system; Moving Maps: 2-D Airport Moving Maps and Cockpit Display of Traffic Information (CDTI-SURF) and 3D Airport Moving Maps (AMM); GPS: Next-Generation Integrated Navigation (NG INAV); Terrain Awareness and Warning Systems: Runway Overrun Awareness and Alerting System (ROASS) |
Diamond DA40 Diamond Star |
Analysis |
Autopilots: KAP 140 dual-axis autopilot; Automatic Direction Finders: KR 87 ADF |
Diamond DA42 Twin Star |
Analysis |
Autopilots: KAP 140 autopilot |
Dorna Pica 1 |
Analysis |
Radio Communications Equipment: KX 125 or KX 155 nav/com, AK350 encoder, 403M intercom; Radar Transponders: KT 76A transponder; Onboard Intercom Systems: KA 134 audio panel; GPS: KLN 35A GPS; Automatic Direction Finders: KR 87 with KI 227 ADF; VOR (Omnirange) Receivers: KI 209 VOR/LOC/Glidescope |
Dorna Pica 2 |
Analysis |
Radio Communications Equipment: KX 155, AK350 encoder; Radar Transponders: Optional KT 76 transponder; VOR (Omnirange) Receivers: KI 209 VOR/LOC/Glidescope |
Dornier 228 |
Analysis |
Weather Mapping Radar: Optional weather radar (228 NG) |
Dornier Seawings Seastar |
Analysis |
Electronic Flight Instrument Systems: Primus Epic 2.0 |
Electra.aero eSTOL |
Analysis |
Fly-by-Wire Systems: Compact fly-by-wire flight control computer (eSTOL) |
Embraer E-Jet 170/190 series |
Analysis |
Airborne Communication Systems: JetWave communications system, ka-band satellite connectivity system for the Lineage 1000E variant.; Avionics Management Systems: Primus Epic integrated avionics suite; Primus Epic 2 on E2 jets with SmartRunway, and SmartLanding advisory functions |
Embraer ERJ-145 series |
Analysis |
Radio Communications Equipment: Dual Primus II radios and radio management systems (); Avionics Management Systems: Primus 1000 (ERJ-145, Legacy 600); Primus Elite (Legacy 650); Weather Mapping Radar: Primus 1000 weather mapping radar (ERJ-145; ERJ-135; ERJ-140; ERJ-145XR; EMB-145 AEW&C; ); GPS: GPS (Legacy 600); Inertial Components & Systems: HF-746G inertial navigation and GPS (ERJ-145 AEW&C) |
Embraer Phenom |
Analysis |
Cabin Pressure Control Systems: Cabin pressure control & monitoring system |
Embraer Praetor 500/600 |
Analysis |
Auxiliary Power Units: 36-150 APU (Legacy 450/500); Air Conditioning Equipment: Air conditioning system (Legacy 500) |
Enstrom 280FX/F282F |
Analysis |
Radio Communications Equipment: KX 155A\165 nav/com; KY 196/197 comms (options); Horizontal Situation Indicator: KCS 55A compass system with KI 525 HSI (option); Moving Maps: Skyforce colour Skymap Model IIIC moving map (option); Electronic Flight Instrument Systems: KMD 150 MFD with GPS/moving map (option); Automatic Direction Finders: KR 87 digital ADF with KI 227 (option) |
Enstrom 480B |
Analysis |
Radio Communications Equipment: KX 155A/165A nav/com; KY 196A com (options); Electronic Flight Instrument Systems: KMD 150 MFD with GPS/moving map (option); Moving Maps: Skyforce Colour Skymap Model IIIC moving map (option); Horizontal Situation Indicator: Optional KCS 55A compass system with KI 525 HSI; Radar/Radio Altimeters: KRA 405B-15 dual antenna radar altimeter; Automatic Direction Finders: Optional KR 87 digital ADF with KI 227; VOR (Omnirange) Receivers: Optional KI 209 VOR/LOC indicator |
Eve eVTOL |
Analysis |
Heading Indicators: Supplying heading reference systems; Inertial Components & Systems: Supply inertial reference system; Magnetometers: |
Evektor VUT 100 Cobra |
Analysis |
Automatic Direction Finders: KR 87 ADF (option) |
Eviation Alice |
Analysis |
Enhanced Vision Systems (EVS): SmartView Synthetic Vision System |
Extra EA-500 |
Analysis |
Autopilots: KFC 225 flight director/autopilot; Electronic Flight Instrument Systems: EHSI ED 461 EFIS & EADI attitude indicator; Distance Measuring Equipment: |
FAdeA IA-63 Pampa |
Analysis |
Air Conditioning Equipment: Environmental control system |
Flying Whale LCA60T |
Analysis |
Starter Generators: 1-megawatt generator system |
Grob G 120 |
Analysis |
Onboard Intercom Systems: KMA 24H-70 audio control/intercom; Radio Communications Equipment: KY 196A VHF, KT 76C transponder; Electronic Flight Instrument Systems: KX 165A nav/com/glidescope; GPS: KLN 94 GPS, KCS 55A compass; Automatic Direction Finders: KR 87 ADF with KI 227 indicator |
Gulfstream G280 |
Analysis |
Air Conditioning Equipment: Environmental control system; Avionics Management Systems: PlaneView280 flight deck, developed in partnership with Gulfstream |
Gulfstream G500 |
Analysis |
Radio Communications Equipment: MCS-7120 high-speed data; Air Conditioning Equipment: Environmental control system; Avionics Management Systems: Primus Epic avionics, integrated with the Gulfstream Symmetry flight deck; Enhanced Vision Systems (EVS): SmartView synthetic vision system; Weather Mapping Radar: LSZ-860 lightning sensor (option); LCD Displays: 8 inch LCD touchscreen controllers; Moving Maps: 2D & 3D airport moving maps; Collision Avoidance Systems/TCAS: Cockpit display of ADS-B-equipped traffic |
Gulfstream G600 |
Analysis |
Radio Communications Equipment: MCS-7120 high-speed data; Air Conditioning Equipment: Environmental control system; Cabin Pressure Control Systems: ; Avionics Management Systems: Primus Epic avionics, integrated with the Gulfstream Symmetry flight deck; Enhanced Vision Systems (EVS): SmartView synthetic vision system; LCD Displays: 8 inch LCD touchscreen controllers; Moving Maps: 2D & 3D airport moving maps; Collision Avoidance Systems/TCAS: Cockpit display of ADS-B-equipped traffic |
Gulfstream G650 |
Analysis |
Auxiliary Power Units: RE220 APU; Inflight Entertainment: DBS satellite television system (option); Air Conditioning Equipment: Twin air conditioning packs; Avionics Management Systems: Primary & multifunction displays; guidance panel; standby multifunction controller; Avionics Management Systems: Gulfstream PlaneView II avionics system is based on Honeywell Primus Epic, includes Gulfstream EVS II (G650); Weather Mapping Radar: LSZ-860 lightning sensor (option); Enhanced Vision Systems (EVS): Synthetic Vision-Primary Flight Display (SV-PFD) ; Terrain Awareness and Warning Systems: Runway Awareness and Advisory System (RAAS) (G650; G650ER) |
Gulfstream G700 |
Analysis |
Flight Management Systems: Primus Epic avionics, integrated with the Gulfstream Symmetry flight deck (G800; G700) |
Hafei Z-9 |
Analysis |
Weather Mapping Radar: Optional Primus 660 weather radar (AC312C) |
HAL Chetak |
Analysis |
Weather Mapping Radar: Optional RDR-1400C weather radar (Chetak, coastguard variant) |
Harbin Y-12 |
Analysis |
Electronic Flight Instrument Systems: Four-screen Primus Apex suite; GPS: KLN 90 GPS (option) (Y-12 II) |
HB Flugtechnik HB 207 Alfa |
Analysis |
Transceivers: 760-channel KX 155 transceiver, KT 76A transponder & ELT (options); VOR (Omnirange) Receivers: KX 125 VOR with KI 208 indicator (option) |
Heart ES-30 |
Analysis |
Flight Management Systems: |
Hongdu JL-8/K-8 |
Analysis |
Air Conditioning Equipment: 51833 air conditioning and pressurisation system (K-8P); Radar/Radio Altimeters: Type 265 radio altimeter (K-8P); Attitude and Heading Reference Systems: HZX-4A AHRS (K-8P); Automatic Direction Finders: ADF 462 |
Indonesian Aerospace NC212i |
Analysis |
Flight Recorders: Optional solid-state CVR, and optional solid-state FDR (NC212i); Terrain Awareness and Warning Systems: Mk VIII EGPWS (NC212i) |
Issoire APM series |
Analysis |
Airborne Communication Systems: Optional KLX 135A comms (APM-20); optional KX 125A VHF/VOR (APM-20); Onboard Intercom Systems: Optional KA 134 intercom (APM-20); Radar Transponders: Optional KT 76A transponder (APM-20); GPS: Optional KMD 250 GPS (APM-20); VOR (Omnirange) Receivers: Optional KI 208 (APM-20) |
Jekta PHA-ZE 100 |
Analysis |
Airborne Communication Systems: ; Avionics Management Systems: ; Flight Management Systems: |
KAI T-50 Golden Eagle |
Analysis |
Radar/Radio Altimeters: HG-9550 radar altimeter; Electronic Flight Instrument Systems: Instrumentation displays including HSI, altitude indicator, electronic altimeter and Mach speed indicator |
Kamov Ka-226T |
Analysis |
Radio Communications Equipment: Bendix/King equipment options |
Kawasaki P-1 |
Analysis |
Air Conditioning Equipment: Environmental control system |
Leonardo AW101 |
Analysis |
Weather Mapping Radar: Weather radar (civil, AW101); RDR-1400 radar (CH-149) |
Leonardo AW139 |
Analysis |
Electronic Flight Instrument Systems: Primus Epic core system (AW139) |
Leonardo M-346 Master |
Analysis |
Air Conditioning Equipment: Enviromental control system; Inertial Components & Systems: Laser gyro INS with embedded GPS |
LET 410 |
Analysis |
Transceivers: KHF 1050 HF transceiver (410 UVP-E20); optional (410 NG); Onboard Intercom Systems: KMA 24H-70 intercom (410 UVP-E20); Radar/Radio Altimeters: KRA 406B radar altimeter; Automatic Direction Finders: KR 87 ADF; Distance Measuring Equipment: KDM 706A DME |
Lockheed Martin C-130J Hercules |
Analysis |
GPS: Dual GPS/INS; Collision Avoidance Systems/TCAS: Miltary version of TCAS |
Lockheed Martin F-16 Fighting Falcon |
Analysis |
Cockpit Video Displays: Multifunction displays (F-16C/D; F-16E/F; F-16I; F-16V Viper; F-21); Air Data Computers: Central air data computer (F-16C/D; F-16E/F; F-16I; F-16V Viper; F-21) |
Lockheed Martin F-35 Lightning II |
Analysis |
Electric Power Controllers: Thermal- and energy-management module |
Magnaghi Sky Arrow |
Analysis |
Radar Transponders: Optional KT-76A Mode C transponder (Sky Arrow 650/710); Radio Communications Equipment: KX-125 nav/com (Sky Arrow 650/710); Radio Communications Equipment: Optional KX-155 nav/com (Sky Arrow 650/710); VOR (Omnirange) Receivers: KI 204 VOR/LOC/Glidescope (Sky Arrow 650/710) |
NZAero 750XL-II SuperPAC |
Analysis |
Radar/Radio Altimeters: KRA 405B radar altimeter (750 XSTOL); Automatic Direction Finders: KR 87 with KI 227 ADF (750 XSTOL); GPS: KCS 55A compass (750 XSTOL) |
Orbis Avia SM-92TE Praga Alfa |
Analysis |
Automatic Direction Finders: KR 87 ADF (SM-92TE Praga Alfa) |
PAC Mushshak |
Analysis |
Radar Transponders: KT 76A/78A ATC transponder (Mushshak); Onboard Intercom Systems: KA 134 audio panel (Mushshak); Automatic Direction Finders: KR 87 ADF (Mushshak) |
Piaggio P.180 Avanti |
Analysis |
Cabin Pressure Control Systems: Cabin Pressure Control and Monitoring System (CPCMS) (Avanti EVO); Flight Management Systems: Epic control display (Avanti) |
Piasecki ARES |
Analysis |
Fly-by-Wire Systems: |
Pilatus PC-12 |
Analysis |
Bleed Air Systems: Engine bleed air system; Radio Communications Equipment: KTR 2280 radio, optional KHF 1050 HF radio; Radar Transponders: KXP 2290 Mode S transponder; Avionics Management Systems: Primus Apex avionics system; Flight Management Systems: Honeywell Anthem integrated flight deck; Enhanced Vision Systems (EVS): SmartView synthetic vision system; Electronic Flight Instrument Systems: Advanced Cockpit Environment (ACE) system (PC-12 NGX); Radar/Radio Altimeters: KRA 405 radar altimeter; Terrain Awareness and Warning Systems: EGPWS Mark VI |
Pilatus PC-24 |
Analysis |
Airborne Communication Systems: VHF Datalink with AFIS, ACARS Graphical Weather, basic and advanced satellite graphical weather (S-XM), FMS Takeoff and Landing Data (TOLD), Controller to Pilot Data Link Communications (CPDLC) over the FANS 1/A+ network, KMA-29A Bluetooth 3D audio panel with record and playback functions.; Avionics Management Systems: Primus Apex and Primus Epic avionics; Weather Mapping Radar: RDR-7000 solid state weather radar with predictive hail and lightning functions; Electronic Flight Instrument Systems: Pilatus advanced cockpit environment (ACE) with touch-screen avionics controller, SmartRunway and SmartLanding advisory functions; Inertial Components & Systems: Laseref inertial reference system; Terrain Awareness and Warning Systems: EGPWS |
Pilatus PC-7 MKII |
Analysis |
Radar/Radio Altimeters: KRA 405B radar altimeter; VOR (Omnirange) Receivers: KNR 634A VOR/glidescope/MKR |
Pilatus PC-9 M |
Analysis |
Radar/Radio Altimeters: KRA 405B radar altimeter |
PZL Mielec M28 Skytruck |
Analysis |
Radio Communications Equipment: KHF 1050 HF radio; Radar/Radio Altimeters: KRA 405B radar altimeter; Automatic Direction Finders: KDF 806 ADF; Terrain Awareness and Warning Systems: EGPWS Mk VI |
Robin Dauphin |
Analysis |
Radio Communications Equipment: Optional KX 155 NAV/COM (DR400/100/160A); VOR (Omnirange) Receivers: Optional KI 208 VOR/LOC indicator (DR400/100/160A) |
Robin President |
Analysis |
Radio Communications Equipment: Optional KX 155 nav/com (DR500/200i); Radar Transponders: Optional KT 76C transponder (DR500/200i); VOR (Omnirange) Receivers: Optional KI 208 VOR/LOC indicator (DR500/200i) |
Saab JAS 39 Gripen |
Analysis |
Radar/Radio Altimeters: ; Inertial Components & Systems: Inertial Navigation System |
SAC Y-8 |
Analysis |
Avionics Management Systems: Primus Epic avionics suite; Flight Recorders: ED-55 flight data recorder |
SAIC LE-500 Xiaoying |
Analysis |
Radar Transponders: KT 76C transponder |
SAIC Y-5 |
Analysis |
Radio Communications Equipment: KHF-950 HF com; GNC 300XL area nav/VHF com; KY 196 receiver (Y-5B); Onboard Intercom Systems: KMA 24 MBR/audio control panel (Y-5B); Automatic Direction Finders: KR -87 ADF (Y-5B) |
SEAMAX M-22 |
Analysis |
Radio Communications Equipment: Bendix/King KY 97 VHF radio with antenna, KT 76A transponder with encoder & antenna |
ShinMaywa US-2 |
Analysis |
Auxiliary Power Units: RE-220 APU |
Sikorsky S-70A Black Hawk |
Analysis |
Weather Mapping Radar: Weather radar in nose (UH-60J) |
Sukhoi SuperJet 100 (SSJ) |
Analysis |
Auxiliary Power Units: |
SyberJet SJ30 |
Analysis |
Electronic Flight Instrument Systems: Core avionics for SyberVision glass panel cockpit; EPIC Primus 2.0 (SJ130i). |
Tecnam P2006T |
Analysis |
Horizontal Situation Indicator: KCS 55A HSI (P2006T); Automatic Direction Finders: KR 87/KI 227 ADF (P2006T) |
Viking Twin Otter Series 400 |
Analysis |
Onboard Intercom Systems: KMA 29 audio panel (Twin Otter Series 400); Radar Transponders: Dual KXP 2290 Mode S EHS transponders (Twin Otter Series 400); Avionics Management Systems: Primus Apex avionics (Twin Otter Series 400/Guardian 400); Super-Lite integrated digital avionics (Twin Otter 400S Seaplane); Radar/Radio Altimeters: Optional KRA 405B radar altimeter (Twin Otter Series 400); Terrain Awareness and Warning Systems: Mk VI EGPWS (Twin Otter Series 400) |
Vulcanair A-Viator |
Analysis |
Electronic Flight Instrument Systems: KMD 850 MFD |
Vulcanair P68 |
Analysis |
Horizontal Situation Indicator: KCS 55A compass system with KI 525A HSI; Radar/Radio Altimeters: KR 87 ADF; VOR (Omnirange) Receivers: KI 209A VOR/LOC/GS/GPS indicator |
Warrior Ocean Seaplane |
Analysis |
Electronic Flight Instrument Systems: Apex 1000 standard |
XAC MA600 Modern Ark |
Analysis |
Radio Communications Equipment: BendixKing dual KTR 908 VHF, single KHF 950 HF & KXP 756 ATC transponder (MA60); Collision Avoidance Systems/TCAS: ACAS II collision avoidance system (MA60); Terrain Awareness and Warning Systems: MkVII GPWS (MA60) |