Elliott Aviation Technical Products
Holds 57 approved modifications, most of them for the Beechcraft B200 King Air B200. FAA spelling: Elliott Aviation Technical Products.
Approved modifications 57 · newest first
Beechcraft B200 King Air B200 12Beechcraft B300 King Air 350 11Beechcraft 300 King Air 300 10Beechcraft 400 Beechjet 10Cessna 550 Citation II 9Cessna S550 8Dassault FALCON 10 8Cessna 560 Citation V, Ultra, Encore and Excel 7Cessna 551 6Beechcraft C90 King Air C90 4Beechcraft 65 3Beechcraft E-90 King Air E90 3
2014-09-07ST03375CH · For aircraft equipped with the Honeywell SPZ-8000 avionics including dual FMZ-2000 Flight Management Systems,... · BAe.125 Series 800A, BAe.125 Series 800B, Hawker 800
2014-01-13SA03289CH · Installation of the Mid-Continent MD302 Electronic Standby Indicator · 200, 200C, 300
2011-01-06SA01352CH · Installation of a Rockwell Collins TCAS 4000 Traffic Alert and Collision Avoidance System (TCAS II) in accordance... · 200, 200C, 200CT
2009-12-18ST02784CH · Installation of a Honeywell Digital Flight Data Recorder (DFDR) · 400, 400A
2009-12-07ST02783CH · Installation of an Artex C406-2 Emergency Locator Transmitter (ELT) · 400
2009-10-13ST02760CH · Installation of a single Universal Avionics Systems Corporation UNS-1Lw Flight Management System and an LP/LPV Monitor · Falcon 10
2009-09-16ST02745CH · Installation of Universal Avionics Systems Corporation Dual UNS-1Espw Flight Management System · 650
2009-08-20SA01640CH · Installation of Universal Avionics Systems Corporation Electronic Flight Instruments Displays (EFI-550). · 200, 200C, 200CT
2009-08-20ST02194CH · Installation of a Universal Avionics Systems Corp. (UASC) EFI-890R Electronic Flight Instrument System (EFIS) and... · Falcon 10
2008-10-27ST02643CH · Installation of modified baggage compartment · TBM 700
2008-07-01ST02588CH · Installation of AirMed Medical Base Assembly · 400A
2008-03-14ST02547CH · Installation of a Universal Avionics Systems Corporation UL-701 UniLink System · Falcon 10
2008-03-14ST02548CH · Installation of an International Communications Group ICS-120 Iridium Satellite Telephone System · Falcon 10
2008-01-10ST02271CH · Installation of a Universal Avionics EFI-890R Electronic Flight Instrument System (EFIS) · 501, 551
2007-05-30ST02431CH · Installation of a Universal Avionics Application Server Unit (ASU). · Falcon 10
2007-04-16ST02407CH · Installation of a Universal Avionics Application Server Unit (ASU). · 501, 551
2006-10-12ST01666CH · Installation of Collins Traffic Alert and Collision Avoidance TCAS 4000 system. · Falcon 10
2006-10-12ST00875WI · Installation of a Universal Avionics System Corporation Terrain Awareness Warning System (TAWS) · Falcon 10
2006-03-22SA02264CH · Installation of Air Data Systems · 300, 300LW, B200
2005-05-03ST01456CH · Installation of a Honeywell Mark VII Enhanced Ground Proximity Warning System (EGPWS). · 550, S550, 560
2005-04-21ST02133CH · Limited to installation on Raytheon model HS.125 series 600A, serial number 256045 ONLY. Non-group aircraft... · HS.125 Series 600A
2005-04-05ST00983CH · Installation of AlliedSignal Enhanced Ground Proximity Warning System. · 400A
2004-11-18ST02074CH · Installation of Innovative Solutions & Support (IS&S) dual Air Data Display Units (ADDU) and single Analog Interface... · BH.125 Series 600A, HS.125 Series 600A, HS.125...
2004-10-14ST02063CH · Modification of executive interior. Limited to installation on model HS.125 Series 700A, serial number 257019 ONLY. · HS.125 Series 700A
2004-08-12ST02019CH · Installation of Universal Avionics Systems Corporation Terrain Awareness Warning System (TAWS) with optional MFD-640... · 550, 560, S550
2004-08-12ST02018CH · Installation of dual Rockwell Collins AHS-1000S Attitude Heading System. · 550, 560, S550
2004-08-12ST02017CH · Installation of a 2-tube or 4-tube Universal Avionics Systems Corporation (UASC) EFI-550 electric flight instrument... · 550, 560, S550
2004-07-20ST02007CH · Certification for Reduced Vertical Separation Minimum (RVSM) operational capability and installation of Honeywell... · MU-300, MU-300-10
2004-05-12ST385CH · Installation of Bendix/King CAS-67A traffic alert and collision avoidance system(TCAS) II. · MU-300, 400, MU-300-10
2004-05-12ST01486CH · Installation of a Honeywell Mark VI/VIII Enhanced Ground Proximity Warning System (EGPWS). · MU-300, 400, MU-300-10
2003-12-18ST01922CH · Installation of the Innovative Solutions & Support (IS&S) Air Data Display Unit (ADDU) with the IS&S Analog... · Falcon 10
2003-12-05SA01914CH · Installation of dual Rockwell Collins AHS-1000S Attitude Heading System. · 200, 200C, 200CT
2003-03-20SA1619GL · Installation of a Bendix TCAS II system comprised of the following P/N's: TPA-81A, TCAS processor; KFS-578A, TCAS... · 650
2002-12-20ST01748CH · Installation of a Universal Terrain Avoidance and Warning System (TAWS). · 35, 35A (C-21A), 36
2002-12-20ST01749CH · Installation of a 4-tube Universal Avionics Electronics Flight Instrumentation System (EFI-550). · 35, 35A (C-21A), 36
2002-12-18ST01744CH · Installation of a Honeywell Enhanced Ground Proximity Warning System (EGPWS) with an optional Rockwell Colins... · HS.125 Series 700A
2002-05-15SA01216CH · Installation of AlliedSignal MK-VI enhanced ground proximity warning system. · B300, 200 (A100-1 (U-21J)), B200C
2002-03-19SA01629CH · Installation of Sound Management System. · 200CT, B200T, B200C
2001-10-24ST468CH · Installation of Honeywell CAS-67A or Collins TCAS 4000 traffic alert and collision avoidance (TCAS II system. · 560, S550, 550
2001-07-03SA01416CH · Installation of a Honeywell Mark VI/VIII Enhanced Ground Proximity Warning System (EGPWS) · C90A, E90, 65-90
2001-06-25SA01480CH · Installation of Bendix/King EFS 50 electronic flight instrument system. · 300 Series, 200 (A100-1 (U-21J)), 200C
1999-08-16ST00931CH · Installation of AlliedSignal Enhanced Ground Proximity Warning System. · 400
1999-06-24SA01071CH · Installation of AlliedSignal MK VII Enhanced Ground Proximity Warning System (EGPWS). · 65-90, E90, C90A
1998-07-23SA00921CH · Installation of Allied Signal Enhanced Ground Proximity Warning System (EGPWS). · B200T, B200C, 300LW
1998-06-15ST404CH · Installation of a Collins TCAS-94 traffic alert and collision avoidance system(TCAS) II. · 400A, 400
1998-04-24SA115CH · Installation of a Bendix/King TCAS I system. · B300, 200 (A100-1 (U-21J)), B200
1997-01-10ST00614CH · Installation of AlliedSignal CAS 66A traffic alert and collision avoidance system (TCAS I). · 560, S550, 550
1996-12-20SA00596CH · Installation of Elliott Aviation Sound Management system. · 690A, 695A, 695
1995-12-12ST469CH · Installation of an AlliedSignal Mark VI ground proximity warning system. · 560, 550, S550
1995-08-21SA398CH · Installation of a Bendix/King TCAS II System. · B200C, 200T, B300
1995-07-20ST390CH · Installation of a Sundstrand Mark VI Ground Proximity Warning System. · 400A
1995-07-14ST386CH · Installation of a Sundstrand Mark VI Ground Proximity Warning System. · 400
1995-05-18ST354CH · Installation of Flight Visions FV-2000 advanced heads-up display. · 550, S550, 551
1994-12-08SA271CH · Installation of a Sundstrand Mark VI Ground Proximity Warning System. · B300C, 200CT, 200T
1994-11-02SA00237WI · Installation of a Bendix/King EFIS-4 0electronic flight instrument system · C90, 65 (L-23F), A65
1994-09-27SA257CH · Increases the cruise interstage turbine temperature (ITT) limit to 695 degrees centrigrade. (C90 WITH PRATT &... · C90
1991-07-12SA1628GL · Installation of Bendix TCAS II system comprised of the following P/N's: TPA-81A, TCAS processor; KFS-578A, TCAS... · 550
Source: FAA Dynamic Regulatory System (type certificate data sheets, supplemental type certificates, technical standard order authorisations). An organisation's name is as the FAA spelled it on each record; related spellings are separate pages.