Manufacturer | Model | STC No. |
Airbus
|
A319- model 115
|
ST04118CH
| Installation of a CTT Humidification System |
Airbus Helicopters
|
AS332/EC225 series
|
SR02393AK
| Installation of a SkyTrac ISAT Model 100 or Model 200, Flight Following Satellite Communication System |
Airbus Helicopters
|
AS332/EC225 series
|
SR02398AK
| Installation of an Astronics Luminescent Systems Inc. Helicopter Emergency Egress Lighting System |
Airbus Helicopters
|
AS332/EC225 series
|
SR02405AK
| Installation of Night Vision Goggle (NVG) Compatible Lighting System |
Airbus Helicopters
|
AS332/EC225 series
|
SR02415AK
| Installation of cockpit voice and data recorder system |
Airbus Helicopters
|
AS332/EC225 series
|
SR02399AK
| Installation of dual Garmin GNS530W/430W system, including Helicopter Terrain Awareness and Warning System (HTAWS) functionality |
Airbus Helicopters
|
AS332/EC225 series
|
SR02473AK
| Installation of the L-3 Communications NGT-9000R/RD and NGT-9000/D ADS-B IN/OUT system |
Airbus Helicopters
|
AS350/AS355/EC130 series
|
SR02338AK
| Installation of an Intelligent Automation Corporation, Model 1134 Helicopter Monitor System |
Airbus Helicopters
|
AS350/AS355/EC130 series
|
SR02341AK
| Installation of a SAGEM integrated cockpit display system and Crossbow attitude and heading reference system |
Airbus Helicopters
|
AS350/AS355/EC130 series
|
SR02478AK
| Installation of the L-3 Aviation Products Lynx multilink surveillance system model NGT-9000() part number 9029000-20000 or Garmin GTX-345 ADS-B transponder part number 011-03302-40 |
Airbus Helicopters
|
AS350/AS355/EC130 series
|
SR02492AK
| Installation of a Crash Resistant Fuel System (CRFS) |
Airbus Helicopters
|
EC120 series
|
SR02478AK
| Installation of the L-3 Aviation Products Lynx multilink surveillance system model NGT-9000() part number 9029000-20000 or Garmin GTX-345 ADS-B transponder part number 011-03302-40 |
Airbus Helicopters
|
EC135 series
|
SR02478AK
| Installation of the L-3 Aviation Products Lynx multilink surveillance system model NGT-9000() part number 9029000-20000 or Garmin GTX-345 ADS-B transponder part number 011-03302-40 |
Beechcraft
|
1900 Series
|
ST01149CH-D
| Installation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I). |
Beechcraft
|
B100
|
SA455CH-D
| Installation of AlliedSignal Aerospace TPE331-10AV Engines and Hartzell HC-B4TN-5F/T10173AN(B, K)-12.5 Propellers |
Beechcraft
|
Bonanza
|
SA1035WE
| Installation of Continental TSIO-520-D |
Beechcraft
|
King Air
|
SA01347CH-D
| Installation of a Honeywell/AlliedSignal Mark VIII Enhanced Ground Proximity Warning System. |
Beechcraft
|
King Air
|
SA03140CH-D
| Installation of a removable tail cone and additional aft bulkhead mounting structure |
Bell
|
206 series
|
SR02326AK
| Installation of a single PFD SAGEM integrated cockpit display system with an Attitude and Heading Reference System (AHRS) |
Bell
|
206 series
|
SR01149SE
| Fabrication of Helipro Corporation International Alternate Drive Cover |
Bell
|
206 series
|
SR02292AK
| Installation of a SAGEM Avionics Integrated Cockpit Display System (ICDS) with a Crossbow Attitude and Heading Reference System (AHRS) in accordance with Vector Aerospace Helicopter Services USA Inc. "Master Drawing List", HP 206-34-33-101, revision G, dated February 28, 2011, or later FAA approved revision. |
Bell
|
206 series
|
SR00490SE
| Installation of replacement tail rotor pitch control tube assembly fairleads in tailboom. |
Bell
|
212 series
|
SR02512AK
| Installation of a Dual Universal Avionics EFI-890H PFD, Garmin GTN-750 NAV/COM/GPS/HTAWS/ADS-B and Rockwell Collins AHC-1000 AHRS System |
Bell
|
412 series
|
SR02473AK
| Installation of the L-3 Communications NGT-9000R/RD and NGT-9000/D ADS-B IN/OUT system |
Bell
|
412 series
|
SH767NE
| Installation of ACRO Manufactured and/or Overhauled Ejectors. |
Bell
|
427 series
|
SR01520NY
| Installation of bulkhead adapter assembly p/n 427-25-11-901-001. |
Bell
|
427 series
|
SR01262NY
| Installation of a FSI Ultra Media II, III, or Wescam camera and isolation mount. |
Bell
|
427 series
|
SR01666NY
| Installation of Helipro Sliding Windows. |
Bell
|
430 series
|
SR01451SE
| Installation of Cineflex HD V 14 gyro stabilized camera in structural provisions for a nose-mounted camera. |
Bell
|
430 series
|
SR01450SE
| Installation of two (2) sliding windows (left and right side) in the passenger compartment. |
Bell
|
430 series
|
SR01452SE
| Installation of structural provisions for four antenna pods, two on the underside of the fuselage and one each on the tips of the rotorcraft wings. |
Bell
|
Huey series
|
SR00267SE
| Fabrication and Installation of a Bell Model 212 vertical tail fin and rotor, 42deg and 90deg gearboxes, and 212 push rod anti-torque control system |
Bell
|
Huey series
|
SR00767SE
| Fabrication of Helipro spar replacement system |
Boeing
|
B727 Series
|
ST01446CH-D
| Installation of Honeywell MK-VII Enhanced Ground Proximity Warning System (EGPWS). |
Boeing
|
B727 Series
|
ST00765CH
| Installation of an AlliedSignal CAS-67A TCAS II Traffic Alert and Collision Avoidance System. |
Boeing
|
B727 Series
|
SA1353NM
| Installation of dual Delco Carousel IV AX or C-Six Inertial Navigation System. |
Boeing
|
B727 Series
|
ST00764CH
| Installation of dual Universal Avionics UNS-1D or Universal Avionics UNS-1F Flight Management Systems with optional Universal MFD-640 |
Boeing
|
B737 Series
|
ST00978CH
| Installation of a Fairchild F-1000 flight data recorder system. |
Boeing
|
B737 Series
|
ST00979CH
| Installation of dual Universal UNS-1C flight management systems. |
Boeing
|
B737 Series
|
ST00981CH
| Installation of an AlliedSignal CAS-67A traffic alert and collision avoidance system (TCAS II). |
Boeing
|
B737 Series
|
ST02756CH-D
| Installation of an in flight entertainment (IFE) system |
Boeing
|
B737 Series
|
ST02753CH-D
| Installation of an Aircell High Speed Internet (AHSI) system and an optional Aircell Cabin Telecommunications Router (CTR) |
Boeing
|
B737 Series
|
ST03267CH
| Activation of a Satcom Direct Wi-Fi System |
Boeing
|
B747 Series
|
ST01148CH-D
| Installation of a Litton Aero Products LTN-2001 GPS sensor. |
Boeing
|
B747 Series
|
ST01222CH-D
| Installation of a Universal Avionics TT-5000 Series Aero I Airborne Satellite Telecommunications System. |
Boeing
|
B757 Series
|
ST03018CH-D
| Installation of Gogo ATG-5000 |
Bombardier
|
Challenger Series
|
ST00808CH
| Installation of dual Honeywell FMZ-2000 flight management systems with dual GNSSU GPS sensors as a primary means of navigation. |
Bombardier
|
Challenger Series
|
ST00924CH
| Modification of a Honeywell EDZ-815/816 Electronic Flight Instrument System (EFIS). |
Bombardier
|
Challenger Series
|
ST00848CH
| Installation of a Fairchild F1000 Flight Data Recorder. |
Bombardier
|
Challenger Series
|
ST01142CH-D
| Installation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System. |
Bombardier
|
Challenger Series
|
ST01226CH-D
| Installation of an AlliedSignal CAS-67A traffic alert and collision avoidance system (TCAS II)incorporating MOPS Change 7. |
Bombardier
|
Challenger Series
|
ST00806CH
| Installation of a Collins TCAS-94 traffic alert and collision avoidance system (TCAS II). |
Bombardier
|
Challenger Series
|
ST01141CH-D
| Installation of a Honeywell TCAS 2000 Traffic Alert and Collision Avoidance System (TCAS II). |
Bombardier
|
Challenger Series
|
ST01140CH-D
| Installation of a Universal Avionics TT-5000 Series Aero I Airborne Satellite Telecommunications System. |
Bombardier
|
Challenger Series
|
ST00809CH
| Installation of AlliedSignal Mark V enhanced ground proximity warning system with windshear advisories. |
Bombardier
|
Challenger Series
|
ST02602CH-D
| Installation of a Chelton HGA-7000 High Gain Antenna. |
Bombardier
|
Challenger Series
|
ST01298CH-D
| Installation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS II). |
Bombardier
|
Challenger Series
|
ST471CH
| Installation of an Allied Signal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II). |
Bombardier
|
Challenger Series
|
ST04033CH
| Upgrade of TCAS to Software V7.1 |
Bombardier
|
Global Express
|
ST03234CH
| Reconfiguration of Cabin Floorplan Arrangement |
Bombardier
|
Global Express
|
ST03293CH
| Upgrade of the Honeywell MK V EGPWS to include the Runway Safety Package |
Bombardier
|
Global Express
|
ST03274CH
| Activation of an 802.11 a/b/g/n WiFi System |
Bombardier
|
Multiple
|
ST03274CH
| Activation of a WiFi System |
Bombardier
|
Multiple
|
ST04276CH
| Installation of a Honeywell JetWave System with associated Ka-Band Radome |
Bombardier
|
Multiple
|
ST04276CH
| Installation of a Honeywell JetWave System with associated Ka-Band Radome |
Bombardier
|
Multiple
|
ST04281CH
| Installation of a Satcom Direct Router System |
Bombardier
|
Multiple
|
ST04293CH
| Installation of a Honeywell JetWave System |
British Aerospace
|
Jetstream 31
|
SA978GL-D
| Relocation of the EGT compensating resistors. |
Cessna
|
208B
|
SA03393CH
| Installation of a Pratt and Whitney Canada PT6A-140 Engine |
Cessna
|
501 Series
|
SA02076CH-D
| Installation of a Rockwell Collins IDS-3000 Integrated Display System. |
Cessna
|
525 Series
|
SA01394CH-D
| Installation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I). |
Cessna
|
525 Series
|
SA00987CH
| Installation of AlliedSignal two tube EFIS-50 on co-pilot's panel with Honeywell FZ500 flight director. |
Cessna
|
550 Series
|
SA1407GL
| Installation of the Collins Radio Group, FPA-80 Flight Profile Advisory System. |
Cessna
|
550 Series
|
ST183CH
| Installation of a Fairchild model F800 digital flight data recorder. |
Cessna
|
550 Series
|
ST01147CH-D
| Installation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System (without Windshear). |
Cessna
|
550 Series
|
ST01227CH-D
| Installation of a Honeywell SPZ-500 Flight Director System for the copilot. |
Cessna
|
550 Series
|
ST01303CH-D
| Installation of a pedestal modification. |
Cessna
|
560 series
|
ST01090CH-D
| Installation of a Honeywell TCAS 2000 traffic alert and collision avoidance system (TCAS II) in aircraft equipped with Honeywell Primus 2000 radios. |
Cessna
|
560 series
|
ST01092CH-D
| Installation of an AlliedSignal Mark VII enhanced ground proximity warning system. |
Cessna
|
560 series
|
ST01098CH-D
| Installation of an AlliedSignal CAS-66A traffic alert and collision avoidance system (TCAS I). |
Cessna
|
560 series
|
ST01223CH-D
| Installation of an Allied Signal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I) integrated to the Honeywell Primus 1000 EFIS. |
Cessna
|
560 series
|
ST01304CH-D
| Installation of a Honeywell AlliedSignal Mark V Enhanced Ground Proximity Warning System. |
Cessna
|
560 series
|
ST01093CH-D
| Installation of a Honeywell TCAS 2000 traffic alert and collision avoidance system (TCAS II) in aircraft equipped with Honeywell primus 2000 Radios. |
Cessna
|
560 series
|
ST01224CH-D
| Installation of a Honeywell/AlliedSignal Mark VIII Enhanced Ground Proximity Warning System. |
Cessna
|
560 series
|
ST336CH-D
| Installation of an AlliedSignal Avionics Mark VII Ground Proximity Warning System with Windshear. |
Cessna
|
650 series
|
SA983GL-D
| Installation of a Bendix TCAS II system |
Cessna
|
650 series
|
ST242CH
| Installation of Sundstrand Mark VI Ground Proximity Warning System. |
Cessna
|
650 series
|
ST541CH-D
| Installation of an AlliedSignal Avionics MK-VII, enhanced ground proximity warning system. |
Cessna
|
650 series
|
ST00705CH-D
| Installation of a Dual AlliedSignal Avionics GNS-X C129 with GNS-XLS CDU Flight Management System with GPS as a primary means of navigation. |
Cessna
|
650 series
|
ST568CH-D
| Installation of a Dual Universal Avionics UNS-1B, Flight Management System with GPS as a primary means of navigation. |
Cessna
|
650 series
|
ST297CH-D
| Installation of a Bendix/King CAS 67A TCAS II system with dual Bendix/King MST-67A Mode S Transponders. |
Cessna
|
650 series
|
ST00668CH
| Installation of Dual AlliedSignal GNS-XLS Flight Management Systems. |
Cessna
|
650 series
|
ST01342CH-D
| Installation of a Honeywell/AlliedSignal Mark VIII Enhanced Ground Proximity Warning System. |
Cessna
|
650 series
|
ST01440CH-D
| Installation of an AirCell Air/Ground Telephone System. |
Cessna
|
650 series
|
ST01443CH-D
| Installation of ARTEX Emergency Locator Transmitter (ELT) 110-406. |
Cessna
|
650 series
|
ST01466CH-D
| Installation of Universal Terrain Awareness Warning System (TAWS). |
Cessna
|
650 series
|
ST01549CH-D
| Installation of Dual Universal Avionics UNS-1F/1D+ GPS Flight Management Systems. |
Cessna
|
650 series
|
ST01145CH-D
| Installation of AlliedSignal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II) with MOPS 6.04A or MOPS 7. |
Cessna
|
650 series
|
ST00892CH
| Installation of an AlliedSignal Mark VII Ground Proximity Warning System or AlliedSignal Mark VII Enhanced Ground Proximity Warning System. |
Cessna
|
Multiple
|
SA1608GL
| Installation of a band D model8909X cockpit voice recorder, P/N 89090-003211. (500 S/N 0214 AND UP) |
Cessna
|
Multiple
|
SA1738GL
| Install cockpit center pedestal extensions, options A, B or C. |
Cessna
|
Multiple
|
SA1739GL
| Install cockpit center pedestal extensions, options A, B or C. |
Cessna
|
Multiple
|
ST300CH
| Installation of a Sundstrand Mark VI GPWS. |
Cessna
|
Multiple
|
ST00618CH
| Installation of a Fairchild F1000 Digital Flight Data Recorder. |
Cessna
|
Multiple
|
ST01551CH-D
| Installation of a Honeywell/AlliedSignal Mark VIII Enhanced Ground Proximity Warning System. |
Cessna
|
Multiple
|
ST301CH
| Installation of an AlliedSignal CAS-67A TCAS II system. |
Cessna
|
Multiple
|
SA02157CH-D
| Installation of a Collins TCAS 4000 Traffic Alert and Collision Avoidance System. |
Cessna
|
Multiple
|
SA01637CH
| Certification of Reduced Vertical Separation Minimum (RVSM) operational capability. |
Cessna
|
Multiple
|
ST01636CH
| Certification of Reduced Vertical Separation Minimum (RVSM) operational capability. |
Dassault
|
F 10 Series
|
SA989GL-D
| Installation of a Bendix TCAS II system |
Dassault
|
F 10 Series
|
ST00939CH-D
| Installation of an AlliedSignal Avionics MK-VII, Enhanced Ground Proximity Warning System. |
Dassault
|
F 10 Series
|
ST00940CH-D
| Installation of a Model 3479 erda Divan. |
Dassault
|
F 10 Series
|
ST00936CH-D
| Installation of an AlliedSignal Avionics CAS 67A traffic alert and collision avoidance system (TCAS II). |
Dassault
|
F 10 Series
|
ST01418CH-D
| Installation of Universal Avionics Terrain Awareness and Warning System (TAWS). |
Dassault
|
F 10 Series
|
ST01419CH-D
| Installation of Universal Avionics Multi-Function Display (MFD). |
Dassault
|
F 10 Series
|
ST01301CH-D
| Installation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I). |
Dassault
|
F 10 Series
|
ST01361CH-D
| Installation of a Rockwell Collins ADC-80K. |
Dassault
|
F 10 Series
|
ST01723CH
| Certification of Reduced Vertical Separation Minimum (RVSM) operational capability. |
Dassault
|
F 10 Series
|
ST01448CH-D
| Installation of Universal Avionics EFI-550 Flat Panel Electronic Flight Instruments. |
Dassault
|
F 10 Series
|
ST01806CH
| Certification of Reduced Vertical Separation Minimum (RVSM) operational capability. |
Dassault
|
F 10 Series
|
ST01006CH-D
| Installation of an AlliedSignal Engines TFE731-2C Turbofan Engine. |
Dassault
|
F 20 Series
|
SA57GL
| Installation of passenger couch. |
Dassault
|
F 20 Series
|
SA970GL-D
| Modification of both pilot and copilot control wheels to accept a dual horizontal stabilizer control switch. |
Dassault
|
F 20 Series
|
SA972GL-D
| Relocation of three computer emergency batteries (two optional installations). |
Dassault
|
F 20 Series
|
SA973GL-D
| Modification and relocation of the intake and exhaust for the solar auxiliary power unit, Model T62T39A. |
Dassault
|
F 20 Series
|
SA974GL-D
| Installation of cabin interior panels consisting of the headliner, window panels and sidewalls. |
Dassault
|
F 20 Series
|
SA977GL-D
| Relocation of the exhaust outlet for the microturbo Saphir auxiliary power unit. |
Dassault
|
F 20 Series
|
SA1537GL
| Installation of a Bendix/King TCAS II system with dual MST-67 Mode S transponders. |
Dassault
|
F 20 Series
|
ST540CH-D
| Installation of a Universal Avionics Systems Corp. Dual UNS-1D Flight Management System. |
Dassault
|
F 20 Series
|
ST00716CH
| Installation of AlliedSignal Traffic Alert and Collision Avoidance Systems (TCAS II). |
Dassault
|
F 20 Series
|
ST00697CH-D
| Installation of a Dual Universal Avionics UNS-1D, FMS, with GPS as a primary means of navigation. |
Dassault
|
F 20 Series
|
ST00700CH-D
| Installation of an electrically operated cabin air flood duct. |
Dassault
|
F 20 Series
|
ST00776CH-D
| Modification of the aircraft Fire Warning/Control Panel. |
Dassault
|
F 20 Series
|
ST00779CH-D
| Installation of an AlliedSignal Avionics MK-V Ground proximity warning system with windshear. |
Dassault
|
F 20 Series
|
ST00833CH-D
| Installation of an AlliedSignal Avionics SSUFDR Flight Data Recorder System. |
Dassault
|
F 20 Series
|
ST00654CH-D
| Installation of an AlliedSignal Avionics Dual GNS-XLS, FMS, with GPS as a primary means of navigation |
Dassault
|
F 20 Series
|
ST00993CH
| Installation of a Fairchild F-1000 flight data recorder system. |
Dassault
|
F 20 Series
|
ST00780CH-D
| Installation of a Dual AlliedSignal Avionics GNS-X C129 with GNS-XLS CDU Flight Management System with GPS as a primary means of navigation. |
Dassault
|
F 20 Series
|
ST01001CH-D
| Installation of a single Universal Avionics UNS-1K Flight Management System with Bendix/King EFS-10. |
Dassault
|
F 20 Series
|
ST01049CH-D
| Installation of an AIRSAT 1 IRIDIUM Satellite Communication System. |
Dassault
|
F 20 Series
|
ST94CH-D
| Installation of a Collins TCAS-94 traffic and collision avoidance system TCAS II with dual Collins TDR-94D mode 'S' transponders. |
Dassault
|
F 20 Series
|
ST00906CH-D
| Installation of Aircraft cabin interior, furnishings and cabinetry. |
Dassault
|
F 20 Series
|
ST00774CH-D
| Installation of a Dual Universal Avionics UNS-1D, Flight Management System with GPS as a primary means of navigation. |
Dassault
|
F 20 Series
|
ST01055CH-D
| Installation of a Universal Avionics TT-5000 series Aero-I Airborne Satellite Telecommunications system. |
Dassault
|
F 20 Series
|
ST00942CH-D
| Removal of existing wing located magnetic fuel indicators P/N L98A201 or P/N L98A202 and the installation of blank out plates. |
Dassault
|
F 20 Series
|
ST01054CH-D
| Installation of an ARTEX 110-406 NAV Emergency Locator Transmitter. |
Dassault
|
F 20 Series
|
ST491CH
| Installation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I). |
Dassault
|
F 20 Series
|
ST274CH
| Installation of a Bendix/King CAS67TCAS II system with dual MST-67 Mode S transponders. |
Dassault
|
F 20 Series
|
ST00932CH-D
| Installation of an AlliedSignal Avionics MK-VII Enhanced Ground Proximity Warning System. |
Dassault
|
F 20 Series
|
ST01315CH-D
| Standard Alterations required for installation of Collins Proline IV Avionics Suite. Requires concurrent installation of Collins Proline IV Avionics Suite per STC ST00600WI-D. |
Dassault
|
F 20 Series
|
ST01317CH-D
| Installation of Collins TCAS-4000 Traffic and Collision Avoidance System (TCAS II). |
Dassault
|
F 20 Series
|
ST01318CH-D
| Installation of a Terra Jet Call Selective Calling System (SELCAL). |
Dassault
|
F 20 Series
|
ST01356CH-D
| Installation of Universal Avionics CVR-30B cockpit voice recorder (CVR) system. |
Dassault
|
F 20 Series
|
ST01357CH-D
| Installation of BFGoodrich WX-1000E stormscope Series II system |
Dassault
|
F 20 Series
|
ST01351CH-D
| Installation of Dual Universal UNS-1K Flight Management System. |
Dassault
|
F 20 Series
|
ST01400CH
| Installation of Universal Avionics Systems Model 640 flat panel electronic engine and systems instrument display system. |
Dassault
|
F 20 Series
|
ST01364CH-D
| Installation of Safe Flight 1501 Series Angle of Attack System. |
Dassault
|
F 20 Series
|
ST01427CH-D
| Installation of Honeywell MK-V Enhanced Ground Proximity Warning System (EGPWS). |
Dassault
|
F 20 Series
|
ST01319CH-D
| Installation of Dual Davtron Cockpit clocks. |
Dassault
|
F 20 Series
|
ST00782CH-D
| Installation of a Dual Honeywell Avionics FMZ-2000, flight management system with GPS as a primary means of navigation. |
Dassault
|
F 20 Series
|
ST01052CH-D
| Installation of an AlliedSignal Avionics CAS 67A traffic alert and collision avoidance system (TCAS II) with Rockwell Collins TDR-94D mode s transponders. |
Dassault
|
F 20 Series
|
ST01420CH-D
| Installation of Standard Alterations Required for Installation of Collins EFIS-85B(12), EFIS-85C(14)/APS-85 Avionics. STC SA2157CE must be installed previously or concurrently. |
Dassault
|
F 20 Series
|
ST01363CH-D
| Installation of a Securaplane XL245-A emergency battery. |
Dassault
|
F 20 Series
|
ST01362CH-D
| Installation of a Dual Universal Avionics UNS-1K Flight Management System with GPS as a primary means of navigation. |
Dassault
|
F 20 Series
|
ST00775CH-D
| Installation of an AlliedSignal Avionics MK-V, enhanced ground proximity warning system. |
Dassault
|
F 20 Series
|
ST00777CH-D
| Modification of the aircraft inverter system, reducing the inverter system from three (3) inverters to two (2) inverters. |
Dassault
|
F 20 Series
|
ST01127CH-D
| Installation of provisions for the future installation of Universal Avionics flat Panel Electronic Engine Indicators. |
Dassault
|
F 20 Series
|
ST01580CH-D
| Installation of Universal Avionics Terrain Awareness and Warning System (TAWS) with Video Display on an optional Universal Avionics Multi-Function Display (MFD). |
Dassault
|
F 20 Series
|
ST01575CH-D
| Installation of ARTEX 110-406 NAV Emergency Locator Transmitter with an ELT/NAV Interface Unit. |
Dassault
|
F 20 Series
|
ST01579CH-D
| Installation of a Honeywell MK-VIII Enhanced Ground Proximity Warning System (EGPWS). |
Dassault
|
F 20 Series
|
ST01314CH-D
| Installation of provisions for future installation of Universal Avionics Terrain Avoidance Warning System (TAWS). |
Dassault
|
F 20 Series
|
SA980GL-D
| Installation of a P/N M45-170093-501 or M45-170093-502 Master Warning Panel. |
Dassault
|
F 20 Series
|
ST02020CH-D
| Installation of a Rockwell Collins Copilot's ADC-80K Air Data computer, ALI-80A Altimeter with FCS-80/85 Interface and Standby Pneumatic Altimeter. |
Dassault
|
F 20 Series
|
ST02030CH-D
| Installation of a dual Innovative Solutions and Support (IS&S) altimetry system. |
Dassault
|
F 20 Series
|
ST274CH-D
| Installation of a Honeywell CAS 67 TCAS II System. |
Dassault
|
F 20 Series
|
ST02167CH-D
| Installation of a Rockwell Collins IDS-3000 Integrated Display System. |
Dassault
|
F 20 Series
|
ST01262CH-D
| Certification of Reduced Vertical Separation Minimums (RVSM) operational capability. |
Dassault
|
F 20 Series
|
ST01362CH-D
| Installation of a Dual Universal Avionics UNS-1K Flight Management System with GPS as a primary means of navigation. |
Dassault
|
F 20 Series
|
ST00994CH
| Installation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System. |
Dassault
|
F 20 Series
|
ST1445CH-D
| Installation of Honeywell N1 Digital Electronic Engine Control (DEEC) |
Dassault
|
F 20 Series
|
SA979GL-D
| Installation of a Class C baggage compartment in aft equipment bay between fuselage Stations 34 and 42. |
Dassault
|
F 20 Series
|
ST00937CH-D
| Installation of an AlliedSignal avionics MK-VII, enhanced ground proximity Warning System. |
Dassault
|
F 20 Series
|
ST01576CH-D
| Installation of a Collins Pro Line 21 Continuum Retrofit Integrated Avionics System. |
Dassault
|
F 20 Series
|
ST03113CH-D
| Installation of a Left Hand Divan |
Dassault
|
F 20 Series
|
ST03246CH
| Upgrade of Rockwell Collins Electronic Flight Instrument System (EFIS-85) for GPS Scaling |
Dassault
|
F 50 Series
|
SA971GL-D
| Installation of a Howell N1 engine monitoring system. |
Dassault
|
F 50 Series
|
ST00656CH-D
| Installation of a Collins Avionics AHS-85E, Dual (AHRS) Attitude Heading Reference System. |
Dassault
|
F 50 Series
|
ST01048CH-D
| Installation of an AlliedSignal Avionics MK-VII Enhanced Ground Proximity Warning System. |
Dassault
|
F 50 Series
|
ST345CH-D
| Installation of an AlliedSignal Avionics MK-V Enhanced Ground Proximity Warning System. |
Dassault
|
F 50 Series
|
ST01143CH-D
| Installation of a Collins TCAS-94 traffic alert and collision avoidance system (TCAS II) with MOPS Change 7. previously equipped with STC SA1762GL. |
Dassault
|
F 50 Series
|
ST01002CH-D
| Installation of a Standby Battery System to provide power to the FMS's during periods of low aircraft bus voltage. |
Dassault
|
F 50 Series
|
ST01194CH-D
| Installation of an ARTEX 110-406 NAV Emergency Locator Transmitter (ELT) system. |
Dassault
|
F 50 Series
|
ST461CH-D
| Installation of Rockwell Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS II). |
Dassault
|
F 50 Series
|
ST542CH-D
| Installation of an AlliedSignal Avionics MK-V Enhanced Ground Proximity Warning System. |
Dassault
|
F 50 Series
|
ST01199CH-D
| Installation of a Smith's Industries Integrated Standby Instrument System (ISIS). |
Dassault
|
F 50 Series
|
ST583CH
| Installation of AlliedSignal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II). |
Dassault
|
F 50 Series
|
ST01225CH-D
| Installation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System with Terrain Video Display. |
Dassault
|
F 50 Series
|
ST01256CH-D
| Installation of Collins TCAS 94 Traffic and Collision Avoidance System (TCAS II) with MOPS Change 7. |
Dassault
|
F 50 Series
|
ST01197CH-D
| Installation of a MagnaStar C-2000 Digital Airborne Telephone System. |
Dassault
|
F 50 Series
|
ST01260CH-D
| Installation of an AlliedSignal MK-V Enhanced Ground Proximity Warning System (EGPWS). |
Dassault
|
F 50 Series
|
ST01263CH-D
| Installation of an AlliedSignal CAS-67A Traffic and Collision Avoidance System (TCAS II). |
Dassault
|
F 50 Series
|
ST01312CH-D
| Upgrade of Honeywell Traffic and Collision Avoidance System (TCAS II) to include MOPS Change 7. Requires previous installation of STC SA8218SW-D. |
Dassault
|
F 50 Series
|
ST00938CH-D
| Installation of an AlliedSignal avionics MK-VII, enhanced ground proximity warning system. |
Dassault
|
F 50 Series
|
ST01311CH-D
| Installation of a three (3) Universal Avionics Flight Management Systems consisting of two UNS-1C's and one UNS-1K. |
Dassault
|
F 50 Series
|
SA982GL-D
| Installation of a Bendix TCAS II system |
Dassault
|
F 50 Series
|
ST01195CH-D
| Installation of a Rockwell Collins HF-9000 High Frequency Communication System. |
Dassault
|
F 50 Series
|
ST01359CH-D
| Installation of a dual Collins AHS-3000 or AHS-3000A Attitude Heading Reference System (AHRS). |
Dassault
|
F 50 Series
|
ST01360CH-D
| Installation of Universal Avionics Terrain Awareness and Warning System (TAWS) |
Dassault
|
F 50 Series
|
ST01426CH-D
| Installation of Universal Avionics Multi-Function Display (MFD). |
Dassault
|
F 50 Series
|
ST01463CH-D
| Installation of a Rockwell Collins FDS-2000 Flight Display System. |
Dassault
|
F 50 Series
|
ST01464CH-D
| Installation of a Litton LTN-92 Inertial Navigation System. |
Dassault
|
F 50 Series
|
ST01465CH-D
| Installation of AlliedSignal Mark VIII Enhanced Ground Proximity Warning System with video display of terrain. |
Dassault
|
F 50 Series
|
ST01573CH-D
| Installation of Standard Alterations required for Installation Collins Proline IV Avionics Suite. Must have STC ST00231WI-D installed. |
Dassault
|
F 50 Series
|
ST00652CH-D
| Installation of an AlliedSignal Avionics TCAS II, CAS 67A. |
Dassault
|
F 50 Series
|
ST01348CH-D
| Installation of an AlliedSignal CAS-81A Traffic Alert and Collision Avoidance System (TCAS II) with MOPS change 7. Installation of ST201CH required. |
Dassault
|
F 50 Series
|
ST01349CH-D
| Installation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS II) with MOPS Change 7. STC ST00591WI must be installed. |
Dassault
|
F 50 Series
|
ST01556CH-D
| Installation of Dual Universal Avionics UNS-1D/1D+ GPS Flight Management Systems. |
Dassault
|
F 50 Series
|
ST01574CH-D
| Installation of a Rockwell Collins TCAS 4000 Traffic and Collision Avoidance System. |
Dassault
|
F 50 Series
|
ST547CH-D
| Installation of Honeywell LASEREF Inertial Reference Systems. |
Dassault
|
F 50 Series
|
ST01849CH-D
| Installation of a Cabin Interior and In-Flight Entertainment System. |
Dassault
|
F 50 Series
|
ST02059CH-D
| Modification of engine cowling to install a Sight Glass. |
Dassault
|
F 50 Series
|
ST00683CH-D
| Installation of a Universal Avionics UNS-1C, Dual (FMS) Flight Management System with GPS as a primary means of navigation. |
Dassault
|
F 50 Series
|
ST334CH-D
| Installation of an AlliedSignal avionics MK-V, Enhanced Ground Proximity Warning System. |
Dassault
|
F 50 Series
|
ST01022CH
| Installation of dual Universal UNS-1C Flight Management System per Notice N8110.60, GPS as a Primary Means of Navigation for Oceanic/Remote Operations. |
Dassault
|
F 50 Series
|
ST00778CH-D
| Installation of a Dual Universal Avionics UNS-1K Flight Management System with GPS as a primary means of navigation |
Dassault
|
F 50 Series
|
ST00824CH
| Installation of AlliedSignal Mark V enhanced ground proximity warning system with windshear advisories. |
Dassault
|
F 50 Series
|
ST01350CH-D
| Installation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS II) with MOPS Change 7. Installation of factory Mod M2104 or M2305 required. |
Dassault
|
F 50 Series
|
ST01047CH-D
| Certification of Reduced Vertical Separation Minimums (RVSM) operational capability. |
Dassault
|
F 50 Series
|
ST01991CH
| Installation of an L3 Communications (Fairchild) Model F1000 Flight Data Recorder (FDR) system. |
Dassault
|
F 50 Series
|
ST02912CH-D
| Installation of an Interior Refurbishment and a Pocket Door. |
Dassault
|
F 50 Series
|
ST01578CH-D
| Installation of a Collins Pro Line 21 Continuum Retrofit Integrated Avionics System. |
Dassault
|
F 50 Series
|
ST01193CH-D
| Installation of an AlliedSignal Global Airborne Flight Information System (AFIS) Satlink System |
Dassault
|
F 50 Series
|
ST02817CH-D
| Installation of Interior Cabin Arrangement to include Single or Dual Aft Divans |
Dassault
|
F 50 Series
|
ST03344CH
| Installation of an Airshow 500 Passenger Flight Information System |
Dassault
|
F 50 Series
|
ST4049CH
| Upgrade of TCAS V7.0 Software to V7.1 |
Dassault
|
F 900 Series
|
ST4049CH
| Upgrade of TCAS V7.0 Software to V7.1 |
Dassault
|
F 900 Series
|
ST337CH-D
| Installation of a Bendix/King model CAS 67A Traffic Collision Avoidance System (TCAS II). |
Dassault
|
F 900 Series
|
ST00831CH-D
| Installation of a Honeywell MCS-3000 Satcom, satellite communications system. |
Dassault
|
F 900 Series
|
ST00783CH-D
| Installation of aircraft cabin interior furnishings and cabinetry. |
Dassault
|
F 900 Series
|
ST01202CH-D
| Installation of a dual Honeywell FMZ-2000 Flight Management System. |
Dassault
|
F 900 Series
|
ST01258CH-D
| Installation of an Airshow Genesys Network System. |
Dassault
|
F 900 Series
|
ST00941CH-D
| Installation of AlliedSignal Avionics Mark V Enhanced Ground Proximity Warning System with display. |
Dassault
|
F 900 Series
|
ST01313CH-D
| Installation of an AlliedSignal Airborne Flight Information System (AFIS). |
Dassault
|
F 900 Series
|
ST00706CH-D
| Installation of a Third Crewmember Jumpseat. |
Dassault
|
F 900 Series
|
ST01345CH-D
| Installation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS II) with MOPS Change 7. Installation of STC SA7310SW-D required. |
Dassault
|
F 900 Series
|
ST00655CH-D
| Installation of a Collins Avionics 906-6 SATCOM Satellite Communications System. |
Dassault
|
F 900 Series
|
ST01757CH-D
| Installation of a cabin interior and in-flight entertainment system. |
Dassault
|
F 900 Series
|
SA981GL-D
| Installation of a Bendix/King (AlliedSignal Avionics) CAS 81A Traffic and Collision Avoidance System (TCAS II) and two MST 67A Mode S Transponders. |
Dassault
|
F 900 Series
|
ST01257CH-D
| Installation of a Universal Avionics TT-3000 Aero-M Airborne Satellite Telecommunications System. |
Dassault
|
F 900EX
|
ST00905CH-D
| Installation of an AlliedSignal Avionics Mark V enhanced ground proximity warning system with display. |
Dassault
|
F 900EX
|
ST03068CH-D
| Reconfiguration of Cabin Floor Plan Arrangement |
Dassault
|
F 900EX
|
ST4049CH
| Upgrade of TCAS V7.0 Software to V7.1 |
Dassault
|
Falcon 2000
|
ST04305CH
| Installation of an L3 Avionics Systems GH-3900 Electronic Standby Instrument System |
Dassault
|
Falcon 7X
|
ST04170CH
| Activation of a WiFi System |
Dassault
|
Multiple
|
ST04072CH
| Installation of an L-3 Avionics Systems GH-3900 Electric Standby Instrument System (ESIS) |
Dassault
|
Multiple
|
ST04140CH
| Installation of a Honeywell JetWave System |
Dassault
|
Multiple
|
ST04305CH
| Installation of an L-3 Avionics Systems GH-3900 Electronic Standby Instrument System |
Dassault
|
Multiple
|
ST02824CH-D
| Installation of Cabin Emergency LED Lights |
Dassault
|
Multiple
|
ST01933CH-D
| Installation of Honeywell Runway Awareness and Advisory System (RAAS). |
Dassault
|
Multiple
|
ST02837CH-D
| Installation of a Honeywell DU-875 display. |
Dassault
|
Multiple
|
ST02960CH-D
| Installation of Hutchinson Aerospace Enhanced Thermal and Acoustic Insulation System (TAIS). |
Dassault
|
Multiple
|
ST03064CH-D
| Upgrade of the Honeywell MK V EGPWS to include the Runway Safety Package. |
Dassault
|
Multiple
|
ST03079CH-D
| Installation of a Jump Seat |
Dassault
|
Multiple
|
ST03350CH
| WI-FI Activation |
Dassault
|
Multiple
|
ST03431CH
| Upgrade of TCAS to Software V7.1 |
Dassault
|
Multiple
|
ST4049CH
| Upgrade of TCAS V7.0 Software to V7.1 |
Dassault
|
Multiple
|
ST4048CH
| Upgrade of TCAS V7.0 Software to V7.1 and DIU Installation |
Dassault
|
Multiple
|
ST01933CH-D
| Installation of Honeywell Runway Awareness and Advisory System (RAAS). |
Dassault
|
Multiple
|
ST09017CH-T
| Installation of an L-3 Avionics Systems GH-3900 Electronic Standby Instrument System |
Dornier
|
228
|
SA329CH-D
| Installation of AlliedSignal Engines Models TPE331-10T-511D, TPE331-10GT-511D, TPE331-10GP-511D or TPE331-10P-511D. |
Embraer
|
E170 Series
|
ST03225CH
| Installation of a Portable ELT and Modification of Interior Placards |
Embraer
|
EMB-135LR
|
ST02656CH-D
| Reconfiguration of the cabin seating arrangement. |
Embraer
|
Multiple
|
ST02803CH-D
| Installation of a Honeywell KHF-1050 HF System |
Embraer
|
Multiple
|
ST02882CH-D
| Installation of a Honeywell Flight Management System (FMS #2). |
Embraer
|
Multiple
|
ST03158CH-D
| Installation of a Reconfiguration of a Cabin Floorplan |
Embraer
|
Multiple
|
ST04316CH
| Installation of a Smartsky System |
Fairchild Aircraft Corporation
|
SA226-T
|
SA338GL-D
| Installation of continuous water alcohol injection system. |
Fairchild Aircraft Corporation
|
SA226-T
|
SA344GL-D
| Installation of Garrett TPE331-10UA-511G engines. |
Fairchild Aircraft Corporation
|
SA226-T
|
SA254GL
| Installation of emergency/ continuous water-alcohol injection system. |
Fairchild Aircraft Corporation
|
SA226-T
|
SA279GL
| Installation of emergency/ continuous water-alcohol injection system. |
Fairchild Aircraft Corporation
|
SA226-T
|
SA345GL-D
| Installation of Garrett TPE 331-10UA-511G engines. |
Gulfstream
|
GI
|
ST00813CH
| Installation of a Fairchild F1000 flight data recorder. |
Gulfstream
|
GIV
|
SA5001NM
| Installation of heading and course select buttons. |
Gulfstream
|
GIV
|
ST00253LA
| Requirements for the installation of the Honeywell Heads Up Display HUD 2020. |
Gulfstream
|
GIV
|
ST00258LA
| Installation of Ground Proximity Warning System (GPWS) or Enhanced Ground Proximity Warning System (EGPWS). |
Gulfstream
|
GIV
|
ST00908CH-D
| Installation of dual Honeywell RCZ852 Mode S Transponders and Honeywell TCAS 2000 System. |
Gulfstream
|
GIV
|
ST01088CH-D
| Upgrade Honeywell SPZ-8000 Electronic Flight Information System for video compatibility with Enhanced Ground Proximity Warning Systems. |
Gulfstream
|
GIV
|
ST01089CH-D
| Installation of an AlliedSignal Mark V Enhanced Ground Proximity Warning System. |
Gulfstream
|
GIV
|
ST00933CH-D
| Installation of an AlliedSignal MK-V Enhanced Ground Proximity Warning System. |
Gulfstream
|
GIV
|
ST01389CH-D
| Installation of a Honeywell/L3 Communications Traffic Alert and Avoidance System (TCAS II) with MOPS Change 7. Previously equipped with STC SA3033SO. |
Gulfstream
|
GIV
|
ST00453LA
| Installation of Honeywell 'Primus 880' High Power Doppler turbulence detector weather radar. |
Gulfstream
|
GIV
|
ST00454LA
| Installation of Honeywell 'MCS-3000' Satcom and Magnavox 'C-2000' Magnastar phone systems. |
Gulfstream
|
GIV
|
ST02911CH-D
| Installation of an Interior Reconfiguration. |
Gulfstream
|
GIV
|
SA3750NM
| Replacement of Honeywell attitude heading reference system (AHRS) with Honeywell lasertrak inertial reference system (IRS). |
Gulfstream
|
GIV
|
ST00455LA
| Installation of BF Goodrich "GH-3000" Electronic Standby Instrument System |
Gulfstream
|
GIV
|
ST04162CH
| Installation of a Honeywell JetWave System with associated Ka-Band Radome |
Gulfstream
|
GV
|
ST04236CH
| Installation of a Honeywell JetWave System with associated Ka-Band Radome |
Gulfstream
|
GV
|
ST02922CH-D
| Installation of an Aircell Axxess Iridium Phone System with a True North Express WiFi System. |
Gulfstream
|
GV
|
ST03038CH-D
| Reconfiguration of a Cabin Floorplan Arrangement. |
Gulfstream
|
Multiple
|
ST75CH
| Installation of Sundstrand Mark VI ground proximity warning system. |
Gulfstream
|
Multiple
|
SA5465NM
| Installation of Honeywell traffic alert and collision avoidance system. |
Gulfstream
|
Multiple
|
SA5488NM
| Installation of Collins traffic alert and collision avoidance system. |
Gulfstream
|
Multiple
|
ST317CH
| Installation of Bendix/King CAS-66A traffic alert and collision avoidance system (TCAS I). |
Gulfstream
|
Multiple
|
ST598CH
| Installation of an AlliedSignal GNS-XLS Flight Management System. |
Gulfstream
|
Multiple
|
ST00681CH-D
| Installation of an AlliedSignal Avionics, TCAS II CAS67A, Traffic Alert and Collision Avoidance System. |
Gulfstream
|
Multiple
|
ST00760CH
| Dual Universal UNS-1C Flight Management Systems a primary means of navigation for oceanic/remote operations. |
Gulfstream
|
Multiple
|
ST00789CH
| Installation of a Fairchild F1000 Flight Data Recorder. |
Gulfstream
|
Multiple
|
ST00711LA
| Installation of Dual Honeywell SPI-501 Flight Director Systems. |
Gulfstream
|
Multiple
|
ST01037CH
| Installation of dual Universal UNS-1M Flight Management Systems. |
Gulfstream
|
Multiple
|
ST01050CH-D
| Installation of a dual universal avionics UNS-1C flight management system with GPS as primary navigation. |
Gulfstream
|
Multiple
|
ST01094CH-D
| Installed a Universal UNS-1B+ and a Universal UNS-1C flight management systems as primary means of navigation for oceanic and remote airspace. |
Gulfstream
|
Multiple
|
ST00930CH
| Installation of an AlliedSignal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II). |
Gulfstream
|
Multiple
|
ST01004CH-D
| Installation of an Airshow Direct TV System. |
Gulfstream
|
Multiple
|
ST462CH-D
| Installation of aircraft cabin interior furnishings and cabinetry. |
Gulfstream
|
Multiple
|
ST01229CH-D
| Installation of dual Universal Avionics UNS-1C Flight Management Systems plus a single Universal Avionics UNS-1K Flight Management System. |
Gulfstream
|
Multiple
|
ST01230CH-D
| Installation of dual Honeywell YG1779 Inertial Reference Systems. |
Gulfstream
|
Multiple
|
ST00462CH-D
| Installation of aircraft cabin interior furnishings and cabinetry. |
Gulfstream
|
Multiple
|
ST00598CH
| Installation of an AlliedSignal GNS-XLS Flight Management System. |
Gulfstream
|
Multiple
|
ST01296CH-D
| Installation of AlliedSignal Mark VII Enhanced Ground Proximity Warning System with windshear advisories and video display of terrain. |
Gulfstream
|
Multiple
|
ST01295CH-D
| Installation of an AlliedSignal CAS-81 Traffic Alert and Collision Avoidance Systems (TCAS II) incorporating MOPS Change 7. Previously equipped with STC ST5529NM. |
Gulfstream
|
Multiple
|
ST01228CH-D
| Installation of Honeywell/AlliedSignal Mark VIII enhanced ground proximity warning system. |
Gulfstream
|
Multiple
|
ST01387CH-D
| Installation of dual Universal Avionics UNS-1K flight management systems. |
Gulfstream
|
Multiple
|
ST01459CH-D
| Installation of Honeywell YG1779 Inertial Reference Systems. |
Gulfstream
|
Multiple
|
ST00788CH
| Installation of AlliedSignal Mark VII ground proximity warning system with windshear advisories. |
Gulfstream
|
Multiple
|
ST01132CH-D
| Installation of a dual Honeywell FMZ-2000 Flight Management System. |
Gulfstream
|
Multiple
|
ST01133CH-D
| Installation of an AlliedSignal MK-V Enhanced Ground Proximity Warning System (EGPWS). |
Gulfstream
|
Multiple
|
ST01135CH-D
| Installation of a Honeywell TCAS 2000 Traffic Alert and Collision Avoidance System. |
Gulfstream
|
Multiple
|
ST01793CH-D
| Installation of a Universal Avionics Multi-Function Display MFD-640. |
Gulfstream
|
Multiple
|
SA4421NM
| Installation of single or dual Global GNS-500A VLF/Omega navigation system and optional Global NDB-2 navigation data bank. |
Gulfstream
|
Multiple
|
SA1848WE
| Installation of Custom Products Model 1875 jump seat on radio rack. |
Gulfstream
|
Multiple
|
SA3399WE
| Installation of a single or dual Litton LTN-72R INS/RNAV navigation system. |
Gulfstream
|
Multiple
|
ST00651LA
| Installation of Dual Universal Avionics System UNS-1K flight management systems with Dual Integral Global Positioning System Sensors. |
Gulfstream
|
Multiple
|
ST00738LA
| Installation of Honeywell Dual AZ-800 Digital Air Data Computer (DADC). |
Gulfstream
|
Multiple
|
ST01299CH-D
| Installation of a Universal Avionics Terrain Awareness Warning System TAWS. |
Gulfstream
|
Multiple
|
ST01990CH
| Installation of a Honeywell AZ-960 Air Data System with Honeywell BA-250 (pilot) altimeters. |
Gulfstream
|
Multiple
|
SA655EA
| Installation of Collins flight directors. |
Gulfstream
|
Multiple
|
ST01635CH
| Certification of Reduced Vertical Separation Minimum (RVSM) operational capability. |
Gulfstream
|
Multiple
|
SA4416NM
| Installation of oxygen system. |
Gulfstream
|
Multiple
|
ST01447CH-D
| Installation of a Honeywell EPIC Control Display System for Retrofit (CDS-R) with optional Advanced File and Graphics Server (AFGS-L) with XM Weather Receiver. |
Gulfstream
|
Multiple
|
ST03033CH-D
| Installation of a True North Simphone System with Optional Swift Broadband, Handsets and Inmarsat Filter. |
Gulfstream
|
Multiple
|
ST04283CH
| Activation of a WiFi System |
Hawker
|
700 Series
|
ST01390CH-D
| Installation of a Honeywell/AlliedSignal Mark VIII Enhanced Ground Proximity Warning System. |
Hawker
|
700A
|
ST501CH
| Installation of AlliedSignal CAS-67A traffic alert and collision avoidance system (TCAS II). |
Hawker
|
700A
|
SA3690WE
| Installation of a Garrett/ AiResearch GTCP36-100 APU in the tail compartment. |
Hawker
|
700A
|
ST00561CH
| Installation of AlliedSignal Mark VII Ground Proximity/Windshear Warning System. |
Hawker
|
700A
|
ST00562CH
| Installation of an AlliedSignal GNS-XLS Flight Management System. |
Hawker
|
800 Series
|
ST00837CH-D
| Installation of an AlliedSignal Avionics MK-VII, Enhanced Ground Proximity Warning System without display. |
Hawker
|
800 Series
|
ST01043CH
| Installation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System. |
Hawker
|
800 Series
|
ST01131CH-D
| Installation of a Honeywell GNS Sensor Unit and GPS Antenna to complete a dual Honeywell FMZ-2000 Flight Management System and GPS as primary means of navigation. |
Hawker
|
800 Series
|
ST01146CH-D
| Installation of an Collins TCAS 94 Traffic Alert and Collision Avoidance System (TCAS II) integrated to the Collins EFIS 86 and incorporating MOPS Change 7. |
Hawker
|
800 Series
|
ST01009CH
| Installation of an AlliedSignal CAS-67A traffic alert and collision avoidance system (TCAS II). |
Hawker
|
800 Series
|
ST01297CH-D
| Installation of a Honeywell/AlliedSignal Mark V Enhanced Ground Proximity Warning System. |
Hawker
|
800 Series
|
ST01128CH-D
| Installation of an AlliedSignal Avionics MK-VII, enhanced ground proximity warning system. |
Hawker
|
800 Series
|
ST02452CH-D
| Installation of a Collins IFIS-5000 Integrated Flight Information System. |
Hawker
|
800 Series
|
ST01439CH-D
| Installation of AirCell Air/Ground Telephone System. |
Hawker
|
800 Series
|
ST00943CH-D
| Installation of an AlliedSignal Avionics MK-VII, enhanced ground proximity warning system with display. |
Hawker
|
800A
|
SA1684GL
| Installation of a Fairchild solid state flight data recorder. |
Hawker
|
800A
|
ST285CH
| Installation of Sundstrand Mark VI ground proximity warning system. |
Hawker
|
Multiple
|
ST569CH-D
| Installation of a Dual Universal Avionics UNS-1D, Flight Management System with GPS as a primary means of navigation. |
Hawker
|
Multiple
|
ST71CH-D
| Installation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System with Collins TDR-94D Mode S Transponders. |
Hawker
|
Multiple
|
ST348CH-D
| Installation of a Sundstrand Mark VI Ground Proximity Warning System. |
Hawker
|
Multiple
|
ST01130CH-D
| Installation of provisions for the future upgrade to existing EFIS and WNAV display capabilities. |
Hawker
|
Multiple
|
ST01053CH-D
| Installation of an ARTEX 110-406 NAV Emergency Locator Transmitter. |
Hawker
|
Multiple
|
ST01136CH-D
| Installation of a Senior Flexonics Inc. Signal conditioner Unit. |
Hawker
|
Multiple
|
ST574CH-D
| Installation of a Dual Honeywell NZ-2000, Flight Management System, with GPS as a primary means of navigation. |
Hawker
|
Multiple
|
ST00781CH-D
| Installation of AlliedSignal Avionics TCAS II, CAS 67A, Traffic Alert and Collision Avoidance System with dual MST-67A Mode S transponders. |
Hawker
|
Multiple
|
ST00784CH-D
| Installation of a Honeywell TCAS 2000 Traffic Alert and Collision Avoidance System with dual Mode S Transponders. |
Hawker
|
Multiple
|
ST01231CH-D
| Installation of a Collins FCS-80 flight director system installed as a second system for use by copilot. |
Hawker
|
Multiple
|
ST01324LA
| Installation of Garrett Aviation auxiliary electrical hydraulic system. |
Hawker
|
Multiple
|
ST01393CH-D
| Installation of a Honeywell/L3 Communications Traffic Alert and Collision Avoidance System (TCAS II) with MOPS Change 7. Previously equipped with STC ST09023SC. |
Hawker
|
Multiple
|
ST00539CH-D
| Installation of a dual Universal Avionics UNS-1D Flight Management System with GPS as a primary means of navigation. |
Hawker
|
Multiple
|
ST349CH-D
| Installation of APU Access Panels. |
Hawker
|
Multiple
|
ST546CH-D
| Installation of an AlliedSignal Avionics, Dual GNS-XLS, Flight Management System with GPS as a primary means of navigation |
Hawker
|
Multiple
|
ST03185CH-D
| Activation of a TrueNorth Avionics, Inc. Simphone WiFi System |
Israel Aerospace
|
1124 Series
|
ST00611CH
| Installation of an AlliedSignal GNS-XLS Flight Management System. |
Israel Aerospace
|
1124 Series
|
ST01144CH-D
| Installation of an AlliedSignal Mark VI or Mark VIII Enhanced Ground Proximity Warning System. |
Israel Aerospace
|
1124 Series
|
ST02150CH-D
| Installation of a Honeywell CAS-67A Traffic and Collision Avoidance System (TCAS II) |
Israel Aerospace
|
1124 Series
|
ST00996CH
| Installation of AlliedSignal CAS-66A traffic alert and collision avoidance system (TCAS I). |
Israel Aerospace
|
Astra
|
ST00990CH
| Installation of dual Allied Signal GNS-XLS Flight Management Systems per notice N8110.60 GPS as a Primary means of Navigation for Oceanic/Remote Operations. |
Israel Aerospace
|
Astra
|
ST01021CH
| Installation of dual Universal UNS-1C Flight Management Systems per Notice N8110.60, GPS as a Primary Means of Navigation for Oceanic/Remote Operations. |
Israel Aerospace
|
Astra
|
ST00955CH
| Installation of an AlliedSignal Mark VII Enhanced ground proximity warning system including optional windshear and optional video terrain display. |
Israel Aerospace
|
Astra
|
ST01854CH-D
| Installation of an Innovative Solutions & Support (IS&S) Air Data Display Unit and Standby Altimeter. |
Israel Aerospace
|
Astra
|
ST00956CH
| Installation of Dual Universal Avionics UNS-1D Flight Management Systems for Primary Means in Oceanic and Remote Airspace. |
Israel Aerospace
|
Astra
|
ST00056CH-D
| Installation of Universal Avionics Flight Management Systems for Primary Means in Oceanic and Remote Airspace. |
Israel Aerospace
|
Astra
|
ST02163CH-D
| Installation of a Honeywell Mark VIII Enhanced Ground Proximity Warning System. |
Learjet
|
31 Series
|
ST576CH-D
| Installation of an AlliedSignal Avionics, Bendix/King CAS 67A TCAS II Traffic Collision Avoidance System. |
Learjet
|
31 Series
|
ST01259CH-D
| Installation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System. |
Learjet
|
35 Series
|
ST00967CH
| Installation of an AlliedSignal CAS-67A Traffic alert and collision avoidance system (TCAS II). |
Learjet
|
35 Series
|
ST00678CH
| Installation of AlliedSignal Mark VII ground proximity warning system with windshear advisories. |
Learjet
|
55 Series
|
ST01051CH-D
| Installation of an AlliedSignal Inc TFE731-3C/3CR Turbofan engine(s). |
Learjet
|
55 Series
|
ST01097CH-D
| Installation of an Allied Signal CAS-67A traffic alert and collision avoidance system (TCAS II). |
Learjet
|
Lear 60
|
ST00796CH
| Installation of dual Universal UNS-1C flight management systems. |
Learjet
|
Multiple
|
ST00907CH-D
| Installation of an AlliedSignal Avionics TCAS I CAS 66A Traffic and Collision Avoidance System. |
Learjet
|
Multiple
|
ST01662CH-D
| Installation of a Honeywell Mark VIII Enhanced Ground Proximity Warning System, EGPWS with video display of terrain |
Leonardo Helicopters
|
AW139 series
|
SR02473AK
| Installation of the L-3 Communications NGT-9000R/RD and NGT-9000/D ADS-B IN/OUT system |
Lockheed
|
Jetstar
|
ST56CH-D
| Installation of a Bendix TCAS II system. (1329 series Modified by STC SA2326SW) |
Lockheed
|
Jetstar
|
ST02038CH-D
| Installation of Honeywell N1 Digital Electronic Engine Controls (DEEC) |
Lockheed
|
Jetstar
|
ST01095CH-D
| Installation of an Allied Signal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II). |
McDonnell Douglas
|
DC-9 Series
|
ST00257LA
| Installation of Honeywell SATCOM 'MCS-3000' system. |
McDonnell Douglas
|
DC-9 Series
|
ST00465LA
| Installation of Collins TCAS-94 with dual Collins Mode S Transponders. |
McDonnell Douglas
|
DC-9 Series
|
ST00466LA
| Installation of Allied Signal Enhanced Ground Proximity Warning System. |
McDonnell Douglas
|
DC-9 Series
|
ST00641LA
| Installation of a right side cockpit window emergency exit access panel to allow opening of the exit from outside the aircraft. |
McDonnell Douglas
|
DC3
|
ST01395CH-D
| Installation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I). |
Mitsubishi Heavy Industries, Ltd.
|
MU-2 Series
|
SA747CE
| Installation of AiResearch TPE331-1-151A engines. |
Mitsubishi Heavy Industries, Ltd.
|
MU-2 Series
|
SA291GL
| Installation of auxiliary fuel tank in aft baggage compartment. |
Mitsubishi Heavy Industries, Ltd.
|
MU-2 Series
|
SA161GL
| Install Garrett AiResearch TPE331-6-252M engines. |
Mitsubishi Heavy Industries, Ltd.
|
MU-2 Series
|
SA60GL
| Installation of two 25-gallon auxiliary fuel tanks in nose section of main landing gear wheel fairings. |
Piper
|
PA-23-250
|
SA688CE
| Installation of propeller unfeathering system. |
Piper
|
PA-23-250
|
SA852WE
| Turbo supercharged Lycoming O-540-A1B5, -A1D5, or -A3D5 engines (S/N's 27-1 thru 27-2504). |
Piper
|
PA-23-250
|
SA909WE
| Installation of turbo supercharged Lycoming IO-540-J4A5 engines. (PA-E23-250 SN 27-2505 and up) |
Piper
|
PA-23-250
|
SA978WE
| Installation of turbo supercharged Lycoming O-540-C4B5 engines. Approved for serial numbers 27-2505 and subsequent. |
Saab
|
340 Series
|
SA984GL-D
| Installation of a Bendix TCAS II system. |
Sabreliner Corporation
|
65 Series
|
ST00667CH
| Installation of Dual AlliedSignal GNS-XLS flight management systems as primary means of navigation for oceanic and remote airspace. |
Sabreliner Corporation
|
65 Series
|
ST00844CH
| Installation of dual Universal UNS-1K Flight Management Systems. |
Sabreliner Corporation
|
65 Series
|
ST00891CH
| Installation of Fairchild F-800 digital flight data recorder. |
Sikorsky
|
S-61 series
|
SR09233RC
| Installation of a Solid State Voltage Regulator |
Sikorsky
|
S-61 series
|
SR09232RC
| Installation of a ground inverter. |
Sikorsky
|
S-61 series
|
SR09236RC
| Installation of a Modular Harness |
Sikorsky
|
S-61 series
|
SR00283SE
| Removal of a 50 inch section from the forward fuselage between stations 110 and 160 and reinstallation of forward cabin with associated fabricated parts. |
Sikorsky
|
S-61 series
|
SR00427SE
| Fabrication and installation of a Helipro Model H9661N01-01, -03, -05, -07, -51, -53, -55, -57, -59 or -61 logging utility system |
Sikorsky
|
S-61 series
|
SR09231RC
| Installation of Smiths Industries Cockpit Voice Recorder in accordance with Master Drawing List ACRO 61-23-00-103, Rev NC, dated April 6, 1999, or later FAA approved revision. |
Sikorsky
|
S-61 series
|
SR09235RC
| Installation of Litton T5PTIT Indicators in accordance with Master Drawing List ACRO 61-77-20-101, Rev. NC dated April 06, 1999, or later FAA approved revision. |
Sikorsky
|
S-61 series
|
SR09238RC
| Installation of NAV/COM avionics package in accordance with Master Drawing List ACRO 61-23-00-101, Rev. B, dated February 21, 2000, or later FAA approved revision. |
Sikorsky
|
S-61 series
|
SA02279AK
| Installation of dual Rockwell Collins FDS 2000 flight displays, dual AHS 3000 attitude and heading reference systems, dual Garmin GNS 530 navigation systems and supporting avionics equipment . |
Sikorsky
|
S-61 series
|
SR09237RC
| Installation of SFENA 904 Standby Attitude Indicator in accordance with Master Drawing List ACRO 61-34-00-101, Rev. NC dated January 28, 1999, or later FAA approved revision. |
Sikorsky
|
S-61 series
|
SR09234RC
| Installation of Navigation Switching and GPS System in accordance with Master Drawing List ACRO 61-34-00-103, Rev A dated February 21, 2000, or later FAA approved revision |
Sikorsky
|
S-61 series
|
SR01264SE
| Fabrication of Helipro replacement windshields |
Sikorsky
|
S-61 series
|
SR00814SE
| Fabrication of reinforcement kit - aft fuselage station 493. For model S61A, applies to S/N 61094. For model S61NM, applies to S/N 66454 |
Sikorsky
|
S-76 series
|
SR02352AK
| Installation of an AXSYS FLIR Camera System |
Sikorsky
|
S-76 series
|
SR02449AK
| Installation of High Intensity Strobe Light (HISL) System |
Sikorsky
|
S-76 series
|
SR02454AK
| Installation of GARMIN GPS 400W System(s); Option #2 - Pilot, Option #1 - Copilot, and Option #3 - Pilot and Copilot |
Sikorsky
|
S-76 series
|
SR02456AK
| Installation of a D1000C Iridium Satcom Blue Sky System |
Sikorsky
|
S-76 series
|
SR02457AK
| Installation of an ACH1000 Advanced Control System Head for an Iridium Satcom Blue Sky System |
Sikorsky
|
S-76 series
|
SR02460AK
| Installation of a Sagem Auxiliary Flight Data Acquisition & Management Unit (AFDAMU) & Fairchild Cockpit Voice & Data Recorder (CVDR) system |
Sikorsky
|
S-76 series
|
SR02461AK
| Installation of a Bendix/King KTA 970 TCAS 1 traffic collision avoidance system |
Sikorsky
|
S-76 series
|
SR02462AK
| Installation of a Garmin GPS 400 system |
Sikorsky
|
S-76 series
|
SR02455AK
| Installation of a Honeywell Enhanced Ground Proximity Warning System (EGPWS) |
Sikorsky
|
S-76 series
|
SR02458AK
| Installation of an LSI Helicopter Emergency Egress Lighting (HEEL) System |
Sikorsky
|
S-76 series
|
SR02459AK
| Installation of a Honeywell Multifunction Radar Display (MFRD) |
Sikorsky
|
S-76 series
|
SR02473AK
| Installation of the L-3 Communications NGT-9000R/RD and NGT-9000/D ADS-B IN/OUT system |
Sikorsky
|
S-76 series
|
SR01520SE
| Installation of a Modularized Main DC Electrical Junction Box. |
Sikorsky
|
S-76 series
|
SR01367SE
| Installation of Rockwell Collins Four Tube FDS 2000 Electronic Flight Instrument System (EFIS) and Rockwell Collins AHC 3000 Attitude Heading Reference System (AHRS). |
Sikorsky
|
S-76 series
|
SH804NE
| Installation of replacement exhaust ejectors. |
Twin Commander
|
681
|
SA337GL-D
| Installation of AiResearch TPE331-1-151-K engines. |
Twin Commander
|
690
|
SA1024SO
| Installation of AiResearch TPE331-5-252K engines replacing AiResearch TPE331-5-251K engines. |