| Cessna |
525 Series |
SA00987CH |
Installation of AlliedSignal two tube EFIS-50 on co-pilot's panel with Honeywell FZ500 flight director. |
| Beechcraft |
King Air |
SA01347CH-D |
Installation of a Honeywell/AlliedSignal Mark VIII Enhanced Ground Proximity Warning System. |
| Cessna |
525 Series |
SA01394CH-D |
Installation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I). |
| Cessna |
Multiple |
SA01637CH |
Certification of Reduced Vertical Separation Minimum (RVSM) operational capability. |
| Cessna |
501 Series |
SA02076CH-D |
Installation of a Rockwell Collins IDS-3000 Integrated Display System. |
| Cessna |
Multiple |
SA02157CH-D |
Installation of a Collins TCAS 4000 Traffic Alert and Collision Avoidance System. |
| 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 . |
| Beechcraft |
King Air |
SA03140CH-D |
Installation of a removable tail cone and additional aft bulkhead mounting structure |
| Twin Commander |
690 |
SA1024SO |
Installation of AiResearch TPE331-5-252K engines replacing AiResearch TPE331-5-251K engines. |
| Beechcraft |
Bonanza |
SA1035WE |
Installation of Continental TSIO-520-D |
| Boeing |
B727 Series |
SA1353NM |
Installation of dual Delco Carousel IV AX or C-Six Inertial Navigation System. |
| Cessna |
550 Series |
SA1407GL |
Installation of the Collins Radio Group, FPA-80 Flight Profile Advisory System. |
| Dassault |
F 20 Series |
SA1537GL |
Installation of a Bendix/King TCAS II system with dual MST-67 Mode S transponders. |
| Cessna |
Multiple |
SA1608GL |
Installation of a band D model8909X cockpit voice recorder, P/N 89090-003211. (500 S/N 0214 AND UP) |
| Mitsubishi Heavy Industries, Ltd. |
MU-2 Series |
SA161GL |
Install Garrett AiResearch TPE331-6-252M engines. |
| Hawker |
800A |
SA1684GL |
Installation of a Fairchild solid state flight data recorder. |
| 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. |
| Gulfstream |
Multiple |
SA1848WE |
Installation of Custom Products Model 1875 jump seat on radio rack. |
| 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. |
| Mitsubishi Heavy Industries, Ltd. |
MU-2 Series |
SA291GL |
Installation of auxiliary fuel tank in aft baggage compartment. |
| Dornier |
228 |
SA329CH-D |
Installation of AlliedSignal Engines Models TPE331-10T-511D, TPE331-10GT-511D, TPE331-10GP-511D or TPE331-10P-511D. |
| Twin Commander |
681 |
SA337GL-D |
Installation of AiResearch TPE331-1-151-K engines. |
| Fairchild Aircraft Corporation |
SA226-T |
SA338GL-D |
Installation of continuous water alcohol injection system. |
| Gulfstream |
Multiple |
SA3399WE |
Installation of a single or dual Litton LTN-72R INS/RNAV navigation system. |
| Fairchild Aircraft Corporation |
SA226-T |
SA344GL-D |
Installation of Garrett TPE331-10UA-511G engines. |
| Fairchild Aircraft Corporation |
SA226-T |
SA345GL-D |
Installation of Garrett TPE 331-10UA-511G engines. |
| Hawker |
700A |
SA3690WE |
Installation of a Garrett/ AiResearch GTCP36-100 APU in the tail compartment. |
| Gulfstream |
GIV |
SA3750NM |
Replacement of Honeywell attitude heading reference system (AHRS) with Honeywell lasertrak inertial reference system (IRS). |
| Gulfstream |
Multiple |
SA4416NM |
Installation of oxygen system. |
| Gulfstream |
Multiple |
SA4421NM |
Installation of single or dual Global GNS-500A VLF/Omega navigation system and optional Global NDB-2 navigation data bank. |
| Beechcraft |
B100 |
SA455CH-D |
Installation of AlliedSignal Aerospace TPE331-10AV Engines and Hartzell HC-B4TN-5F/T10173AN(B, K)-12.5 Propellers |
| Gulfstream |
GIV |
SA5001NM |
Installation of heading and course select buttons. |
| Gulfstream |
Multiple |
SA5465NM |
Installation of Honeywell traffic alert and collision avoidance system. |
| Gulfstream |
Multiple |
SA5488NM |
Installation of Collins traffic alert and collision avoidance system. |
| Dassault |
F 20 Series |
SA57GL |
Installation of passenger couch. |
| 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. |
| Gulfstream |
Multiple |
SA655EA |
Installation of Collins flight directors. |
| Piper |
PA-23-250 |
SA688CE |
Installation of propeller unfeathering system. |
| Mitsubishi Heavy Industries, Ltd. |
MU-2 Series |
SA747CE |
Installation of AiResearch TPE331-1-151A engines. |
| 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) |
| Dassault |
F 20 Series |
SA970GL-D |
Modification of both pilot and copilot control wheels to accept a dual horizontal stabilizer control switch. |
| Dassault |
F 50 Series |
SA971GL-D |
Installation of a Howell N1 engine monitoring system. |
| 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. |
| British Aerospace |
Jetstream 31 |
SA978GL-D |
Relocation of the EGT compensating resistors. |
| Piper |
PA-23-250 |
SA978WE |
Installation of turbo supercharged Lycoming O-540-C4B5 engines. Approved for serial numbers 27-2505 and subsequent. |
| 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 |
SA980GL-D |
Installation of a P/N M45-170093-501 or M45-170093-502 Master Warning Panel. |
| 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 50 Series |
SA982GL-D |
Installation of a Bendix TCAS II system |
| Cessna |
650 series |
SA983GL-D |
Installation of a Bendix TCAS II system |
| Saab |
340 Series |
SA984GL-D |
Installation of a Bendix TCAS II system. |
| Dassault |
F 10 Series |
SA989GL-D |
Installation of a Bendix TCAS II system |
| Bell |
412 series |
SH767NE |
Installation of ACRO Manufactured and/or Overhauled Ejectors. |
| Sikorsky |
S-76 series |
SH804NE |
Installation of replacement exhaust ejectors. |
| 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 |
| 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 |
| Bell |
206 series |
SR00490SE |
Installation of replacement tail rotor pitch control tube assembly fairleads in tailboom. |
| Bell |
Huey series |
SR00767SE |
Fabrication of Helipro spar replacement system |
| 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 |
| Bell |
206 series |
SR01149SE |
Fabrication of Helipro Corporation International Alternate Drive Cover |
| Bell |
427 series |
SR01262NY |
Installation of a FSI Ultra Media II, III, or Wescam camera and isolation mount. |
| Sikorsky |
S-61 series |
SR01264SE |
Fabrication of Helipro replacement windshields |
| 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). |
| Bell |
430 series |
SR01450SE |
Installation of two (2) sliding windows (left and right side) in the passenger compartment. |
| Bell |
430 series |
SR01451SE |
Installation of Cineflex HD V 14 gyro stabilized camera in structural provisions for a nose-mounted camera. |
| 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 |
427 series |
SR01520NY |
Installation of bulkhead adapter assembly p/n 427-25-11-901-001. |
| Sikorsky |
S-76 series |
SR01520SE |
Installation of a Modularized Main DC Electrical Junction Box. |
| Bell |
427 series |
SR01666NY |
Installation of Helipro Sliding Windows. |
| 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 |
SR02326AK |
Installation of a single PFD SAGEM integrated cockpit display system with an Attitude and Heading Reference System (AHRS) |
| 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 |
| Sikorsky |
S-76 series |
SR02352AK |
Installation of an AXSYS FLIR Camera 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 |
SR02399AK |
Installation of dual Garmin GNS530W/430W system, including Helicopter Terrain Awareness and Warning System (HTAWS) functionality |
| 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 |
| 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 |
SR02455AK |
Installation of a Honeywell Enhanced Ground Proximity Warning System (EGPWS) |
| 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 |
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 |
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 |
| Airbus Helicopters |
AS332/EC225 series |
SR02473AK |
Installation of the L-3 Communications NGT-9000R/RD and NGT-9000/D ADS-B IN/OUT system |
| Bell |
412 series |
SR02473AK |
Installation of the L-3 Communications NGT-9000R/RD and NGT-9000/D ADS-B IN/OUT system |
| Leonardo Helicopters |
AW139 series |
SR02473AK |
Installation of the L-3 Communications NGT-9000R/RD and NGT-9000/D ADS-B IN/OUT system |
| Sikorsky |
S-76 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 |
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 |
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 |
| Airbus Helicopters |
AS350/AS355/EC130 series |
SR02492AK |
Installation of a Crash Resistant Fuel System (CRFS) |
| 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 |
| 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 |
SR09232RC |
Installation of a ground inverter. |
| Sikorsky |
S-61 series |
SR09233RC |
Installation of a Solid State Voltage Regulator |
| 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 |
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 |
SR09236RC |
Installation of a Modular Harness |
| 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 |
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. |
| Israel Aerospace |
Astra |
ST00056CH-D |
Installation of Universal Avionics Flight Management Systems for Primary Means in Oceanic and Remote Airspace. |
| Gulfstream |
GIV |
ST00253LA |
Requirements for the installation of the Honeywell Heads Up Display HUD 2020. |
| McDonnell Douglas |
DC-9 Series |
ST00257LA |
Installation of Honeywell SATCOM 'MCS-3000' system. |
| Gulfstream |
GIV |
ST00258LA |
Installation of Ground Proximity Warning System (GPWS) or Enhanced Ground Proximity Warning System (EGPWS). |
| 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 |
ST00455LA |
Installation of BF Goodrich "GH-3000" Electronic Standby Instrument System |
| Gulfstream |
Multiple |
ST00462CH-D |
Installation of aircraft cabin interior furnishings and cabinetry. |
| 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. |
| Hawker |
Multiple |
ST00539CH-D |
Installation of a dual Universal Avionics UNS-1D Flight Management System with GPS as a primary means of navigation. |
| 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. |
| Gulfstream |
Multiple |
ST00598CH |
Installation of an AlliedSignal GNS-XLS Flight Management System. |
| Israel Aerospace |
1124 Series |
ST00611CH |
Installation of an AlliedSignal GNS-XLS Flight Management System. |
| Cessna |
Multiple |
ST00618CH |
Installation of a Fairchild F1000 Digital Flight Data Recorder. |
| 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. |
| Gulfstream |
Multiple |
ST00651LA |
Installation of Dual Universal Avionics System UNS-1K flight management systems with Dual Integral Global Positioning System Sensors. |
| Dassault |
F 50 Series |
ST00652CH-D |
Installation of an AlliedSignal Avionics TCAS II, CAS 67A. |
| 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 900 Series |
ST00655CH-D |
Installation of a Collins Avionics 906-6 SATCOM Satellite Communications System. |
| Dassault |
F 50 Series |
ST00656CH-D |
Installation of a Collins Avionics AHS-85E, Dual (AHRS) Attitude Heading Reference 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. |
| Cessna |
650 series |
ST00668CH |
Installation of Dual AlliedSignal GNS-XLS Flight Management Systems. |
| Learjet |
35 Series |
ST00678CH |
Installation of AlliedSignal Mark VII ground proximity warning system with windshear advisories. |
| Gulfstream |
Multiple |
ST00681CH-D |
Installation of an AlliedSignal Avionics, TCAS II CAS67A, Traffic Alert and Collision Avoidance System. |
| 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 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. |
| 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. |
| Dassault |
F 900 Series |
ST00706CH-D |
Installation of a Third Crewmember Jumpseat. |
| Gulfstream |
Multiple |
ST00711LA |
Installation of Dual Honeywell SPI-501 Flight Director Systems. |
| Dassault |
F 20 Series |
ST00716CH |
Installation of AlliedSignal Traffic Alert and Collision Avoidance Systems (TCAS II). |
| Gulfstream |
Multiple |
ST00738LA |
Installation of Honeywell Dual AZ-800 Digital Air Data Computer (DADC). |
| Gulfstream |
Multiple |
ST00760CH |
Dual Universal UNS-1C Flight Management Systems a primary means of navigation for oceanic/remote operations. |
| 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 |
B727 Series |
ST00765CH |
Installation of an AlliedSignal CAS-67A TCAS II Traffic Alert and Collision Avoidance System. |
| 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 |
ST00775CH-D |
Installation of an AlliedSignal Avionics MK-V, enhanced ground proximity warning system. |
| Dassault |
F 20 Series |
ST00776CH-D |
Modification of the aircraft Fire Warning/Control Panel. |
| 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 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 20 Series |
ST00779CH-D |
Installation of an AlliedSignal Avionics MK-V Ground proximity warning system with windshear. |
| 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. |
| 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. |
| 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 900 Series |
ST00783CH-D |
Installation of aircraft cabin interior furnishings and cabinetry. |
| Hawker |
Multiple |
ST00784CH-D |
Installation of a Honeywell TCAS 2000 Traffic Alert and Collision Avoidance System with dual Mode S Transponders. |
| Gulfstream |
Multiple |
ST00788CH |
Installation of AlliedSignal Mark VII ground proximity warning system with windshear advisories. |
| Gulfstream |
Multiple |
ST00789CH |
Installation of a Fairchild F1000 Flight Data Recorder. |
| Learjet |
Lear 60 |
ST00796CH |
Installation of dual Universal UNS-1C flight management systems. |
| Bombardier |
Challenger Series |
ST00806CH |
Installation of a Collins TCAS-94 traffic alert and collision avoidance system (TCAS II). |
| 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 |
ST00809CH |
Installation of AlliedSignal Mark V enhanced ground proximity warning system with windshear advisories. |
| Gulfstream |
GI |
ST00813CH |
Installation of a Fairchild F1000 flight data recorder. |
| Dassault |
F 50 Series |
ST00824CH |
Installation of AlliedSignal Mark V enhanced ground proximity warning system with windshear advisories. |
| Dassault |
F 900 Series |
ST00831CH-D |
Installation of a Honeywell MCS-3000 Satcom, satellite communications system. |
| Dassault |
F 20 Series |
ST00833CH-D |
Installation of an AlliedSignal Avionics SSUFDR Flight Data Recorder System. |
| Hawker |
800 Series |
ST00837CH-D |
Installation of an AlliedSignal Avionics MK-VII, Enhanced Ground Proximity Warning System without display. |
| Sabreliner Corporation |
65 Series |
ST00844CH |
Installation of dual Universal UNS-1K Flight Management Systems. |
| Bombardier |
Challenger Series |
ST00848CH |
Installation of a Fairchild F1000 Flight Data Recorder. |
| Sabreliner Corporation |
65 Series |
ST00891CH |
Installation of Fairchild F-800 digital flight data recorder. |
| Cessna |
650 series |
ST00892CH |
Installation of an AlliedSignal Mark VII Ground Proximity Warning System or AlliedSignal Mark VII Enhanced Ground Proximity Warning System. |
| Dassault |
F 900EX |
ST00905CH-D |
Installation of an AlliedSignal Avionics Mark V enhanced ground proximity warning system with display. |
| Dassault |
F 20 Series |
ST00906CH-D |
Installation of Aircraft cabin interior, furnishings and cabinetry. |
| Learjet |
Multiple |
ST00907CH-D |
Installation of an AlliedSignal Avionics TCAS I CAS 66A Traffic and Collision Avoidance System. |
| Gulfstream |
GIV |
ST00908CH-D |
Installation of dual Honeywell RCZ852 Mode S Transponders and Honeywell TCAS 2000 System. |
| Bombardier |
Challenger Series |
ST00924CH |
Modification of a Honeywell EDZ-815/816 Electronic Flight Instrument System (EFIS). |
| Gulfstream |
Multiple |
ST00930CH |
Installation of an AlliedSignal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II). |
| Dassault |
F 20 Series |
ST00932CH-D |
Installation of an AlliedSignal Avionics MK-VII Enhanced Ground Proximity Warning System. |
| Gulfstream |
GIV |
ST00933CH-D |
Installation of an AlliedSignal MK-V Enhanced Ground Proximity Warning System. |
| Dassault |
F 10 Series |
ST00936CH-D |
Installation of an AlliedSignal Avionics CAS 67A traffic alert and collision avoidance system (TCAS II). |
| Dassault |
F 20 Series |
ST00937CH-D |
Installation of an AlliedSignal avionics MK-VII, enhanced ground proximity Warning System. |
| Dassault |
F 50 Series |
ST00938CH-D |
Installation of an AlliedSignal avionics MK-VII, enhanced ground proximity warning 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 900 Series |
ST00941CH-D |
Installation of AlliedSignal Avionics Mark V Enhanced Ground Proximity Warning System with display. |
| 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. |
| Hawker |
800 Series |
ST00943CH-D |
Installation of an AlliedSignal Avionics MK-VII, enhanced ground proximity warning system with display. |
| 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 |
ST00956CH |
Installation of Dual Universal Avionics UNS-1D Flight Management Systems for Primary Means in Oceanic and Remote Airspace. |
| Learjet |
35 Series |
ST00967CH |
Installation of an AlliedSignal CAS-67A Traffic alert and collision avoidance system (TCAS II). |
| 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). |
| 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. |
| Dassault |
F 20 Series |
ST00993CH |
Installation of a Fairchild F-1000 flight data recorder system. |
| Dassault |
F 20 Series |
ST00994CH |
Installation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System. |
| Israel Aerospace |
1124 Series |
ST00996CH |
Installation of AlliedSignal CAS-66A traffic alert and collision avoidance system (TCAS I). |
| Dassault |
F 20 Series |
ST01001CH-D |
Installation of a single Universal Avionics UNS-1K Flight Management System with Bendix/King EFS-10. |
| 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. |
| Gulfstream |
Multiple |
ST01004CH-D |
Installation of an Airshow Direct TV System. |
| Dassault |
F 10 Series |
ST01006CH-D |
Installation of an AlliedSignal Engines TFE731-2C Turbofan Engine. |
| Hawker |
800 Series |
ST01009CH |
Installation of an AlliedSignal CAS-67A traffic alert and collision avoidance system (TCAS II). |
| 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. |
| 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. |
| Gulfstream |
Multiple |
ST01037CH |
Installation of dual Universal UNS-1M Flight Management Systems. |
| Hawker |
800 Series |
ST01043CH |
Installation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System. |
| Dassault |
F 50 Series |
ST01047CH-D |
Certification of Reduced Vertical Separation Minimums (RVSM) operational capability. |
| Dassault |
F 50 Series |
ST01048CH-D |
Installation of an AlliedSignal Avionics MK-VII Enhanced Ground Proximity Warning System. |
| Dassault |
F 20 Series |
ST01049CH-D |
Installation of an AIRSAT 1 IRIDIUM Satellite Communication System. |
| Gulfstream |
Multiple |
ST01050CH-D |
Installation of a dual universal avionics UNS-1C flight management system with GPS as primary navigation. |
| Learjet |
55 Series |
ST01051CH-D |
Installation of an AlliedSignal Inc TFE731-3C/3CR Turbofan engine(s). |
| 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. |
| Hawker |
Multiple |
ST01053CH-D |
Installation of an ARTEX 110-406 NAV Emergency Locator Transmitter. |
| Dassault |
F 20 Series |
ST01054CH-D |
Installation of an ARTEX 110-406 NAV Emergency Locator Transmitter. |
| Dassault |
F 20 Series |
ST01055CH-D |
Installation of a Universal Avionics TT-5000 series Aero-I Airborne Satellite Telecommunications 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. |
| 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 |
ST01093CH-D |
Installation of a Honeywell TCAS 2000 traffic alert and collision avoidance system (TCAS II) in aircraft equipped with Honeywell primus 2000 Radios. |
| 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. |
| Lockheed |
Jetstar |
ST01095CH-D |
Installation of an Allied Signal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II). |
| Learjet |
55 Series |
ST01097CH-D |
Installation of an Allied Signal CAS-67A traffic alert and collision avoidance system (TCAS II). |
| Cessna |
560 series |
ST01098CH-D |
Installation of an AlliedSignal CAS-66A traffic alert and collision avoidance system (TCAS I). |
| Dassault |
F 20 Series |
ST01127CH-D |
Installation of provisions for the future installation of Universal Avionics flat Panel Electronic Engine Indicators. |
| Hawker |
800 Series |
ST01128CH-D |
Installation of an AlliedSignal Avionics MK-VII, enhanced ground proximity warning system. |
| Hawker |
Multiple |
ST01130CH-D |
Installation of provisions for the future upgrade to existing EFIS and WNAV display capabilities. |
| 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. |
| 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. |
| Hawker |
Multiple |
ST01136CH-D |
Installation of a Senior Flexonics Inc. Signal conditioner Unit. |
| Bombardier |
Challenger Series |
ST01140CH-D |
Installation of a Universal Avionics TT-5000 Series Aero I Airborne Satellite Telecommunications System. |
| Bombardier |
Challenger Series |
ST01141CH-D |
Installation of a Honeywell TCAS 2000 Traffic Alert and Collision Avoidance System (TCAS II). |
| Bombardier |
Challenger Series |
ST01142CH-D |
Installation of an AlliedSignal Mark VII 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. |
| Israel Aerospace |
1124 Series |
ST01144CH-D |
Installation of an AlliedSignal Mark VI or Mark VIII Enhanced Ground Proximity Warning System. |
| 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. |
| 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. |
| Cessna |
550 Series |
ST01147CH-D |
Installation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System (without Windshear). |
| Boeing |
B747 Series |
ST01148CH-D |
Installation of a Litton Aero Products LTN-2001 GPS sensor. |
| Beechcraft |
1900 Series |
ST01149CH-D |
Installation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I). |
| Dassault |
F 50 Series |
ST01193CH-D |
Installation of an AlliedSignal Global Airborne Flight Information System (AFIS) Satlink System |
| Dassault |
F 50 Series |
ST01194CH-D |
Installation of an ARTEX 110-406 NAV Emergency Locator Transmitter (ELT) system. |
| Dassault |
F 50 Series |
ST01195CH-D |
Installation of a Rockwell Collins HF-9000 High Frequency Communication System. |
| Dassault |
F 50 Series |
ST01197CH-D |
Installation of a MagnaStar C-2000 Digital Airborne Telephone System. |
| Dassault |
F 50 Series |
ST01199CH-D |
Installation of a Smith's Industries Integrated Standby Instrument System (ISIS). |
| Dassault |
F 900 Series |
ST01202CH-D |
Installation of a dual Honeywell FMZ-2000 Flight Management System. |
| Boeing |
B747 Series |
ST01222CH-D |
Installation of a Universal Avionics TT-5000 Series Aero I Airborne Satellite Telecommunications System. |
| 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 |
ST01224CH-D |
Installation of a Honeywell/AlliedSignal Mark VIII Enhanced Ground Proximity Warning System. |
| Dassault |
F 50 Series |
ST01225CH-D |
Installation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System with Terrain Video Display. |
| Bombardier |
Challenger Series |
ST01226CH-D |
Installation of an AlliedSignal CAS-67A traffic alert and collision avoidance system (TCAS II)incorporating MOPS Change 7. |
| Cessna |
550 Series |
ST01227CH-D |
Installation of a Honeywell SPZ-500 Flight Director System for the copilot. |
| Gulfstream |
Multiple |
ST01228CH-D |
Installation of Honeywell/AlliedSignal Mark VIII enhanced ground proximity warning system. |
| 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. |
| Hawker |
Multiple |
ST01231CH-D |
Installation of a Collins FCS-80 flight director system installed as a second system for use by copilot. |
| Dassault |
F 50 Series |
ST01256CH-D |
Installation of Collins TCAS 94 Traffic and Collision Avoidance System (TCAS II) with MOPS Change 7. |
| Dassault |
F 900 Series |
ST01257CH-D |
Installation of a Universal Avionics TT-3000 Aero-M Airborne Satellite Telecommunications System. |
| Dassault |
F 900 Series |
ST01258CH-D |
Installation of an Airshow Genesys Network System. |
| Learjet |
31 Series |
ST01259CH-D |
Installation of an AlliedSignal Mark VII Enhanced Ground Proximity Warning System. |
| Dassault |
F 50 Series |
ST01260CH-D |
Installation of an AlliedSignal MK-V Enhanced Ground Proximity Warning System (EGPWS). |
| Dassault |
F 20 Series |
ST01262CH-D |
Certification of Reduced Vertical Separation Minimums (RVSM) operational capability. |
| Dassault |
F 50 Series |
ST01263CH-D |
Installation of an AlliedSignal CAS-67A Traffic and Collision Avoidance System (TCAS II). |
| 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 |
ST01296CH-D |
Installation of AlliedSignal Mark VII Enhanced Ground Proximity Warning System with windshear advisories and video display of terrain. |
| Hawker |
800 Series |
ST01297CH-D |
Installation of a Honeywell/AlliedSignal Mark V Enhanced Ground Proximity Warning System. |
| Bombardier |
Challenger Series |
ST01298CH-D |
Installation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS II). |
| Gulfstream |
Multiple |
ST01299CH-D |
Installation of a Universal Avionics Terrain Awareness Warning System TAWS. |
| Dassault |
F 10 Series |
ST01301CH-D |
Installation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I). |
| Cessna |
550 Series |
ST01303CH-D |
Installation of a pedestal modification. |
| Cessna |
560 series |
ST01304CH-D |
Installation of a Honeywell AlliedSignal Mark V 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 |
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 900 Series |
ST01313CH-D |
Installation of an AlliedSignal Airborne Flight Information System (AFIS). |
| Dassault |
F 20 Series |
ST01314CH-D |
Installation of provisions for future installation of Universal Avionics Terrain Avoidance Warning System (TAWS). |
| 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 |
ST01319CH-D |
Installation of Dual Davtron Cockpit clocks. |
| Hawker |
Multiple |
ST01324LA |
Installation of Garrett Aviation auxiliary electrical hydraulic system. |
| Cessna |
650 series |
ST01342CH-D |
Installation of a Honeywell/AlliedSignal Mark VIII Enhanced Ground Proximity Warning System. |
| 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 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 |
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 20 Series |
ST01351CH-D |
Installation of Dual Universal UNS-1K Flight Management System. |
| 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 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 10 Series |
ST01361CH-D |
Installation of a Rockwell Collins ADC-80K. |
| 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 |
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 |
ST01363CH-D |
Installation of a Securaplane XL245-A emergency battery. |
| Dassault |
F 20 Series |
ST01364CH-D |
Installation of Safe Flight 1501 Series Angle of Attack System. |
| Gulfstream |
Multiple |
ST01387CH-D |
Installation of dual Universal Avionics UNS-1K flight management systems. |
| 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. |
| Hawker |
700 Series |
ST01390CH-D |
Installation of a Honeywell/AlliedSignal Mark VIII Enhanced Ground Proximity Warning 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. |
| McDonnell Douglas |
DC3 |
ST01395CH-D |
Installation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I). |
| Dassault |
F 20 Series |
ST01400CH |
Installation of Universal Avionics Systems Model 640 flat panel electronic engine and systems instrument display system. |
| 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 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 50 Series |
ST01426CH-D |
Installation of Universal Avionics Multi-Function Display (MFD). |
| Dassault |
F 20 Series |
ST01427CH-D |
Installation of Honeywell MK-V Enhanced Ground Proximity Warning System (EGPWS). |
| Hawker |
800 Series |
ST01439CH-D |
Installation of AirCell Air/Ground Telephone 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. |
| Boeing |
B727 Series |
ST01446CH-D |
Installation of Honeywell MK-VII Enhanced Ground Proximity Warning System (EGPWS). |
| 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. |
| Dassault |
F 10 Series |
ST01448CH-D |
Installation of Universal Avionics EFI-550 Flat Panel Electronic Flight Instruments. |
| Gulfstream |
Multiple |
ST01459CH-D |
Installation of Honeywell YG1779 Inertial Reference Systems. |
| 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. |
| 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 |
Multiple |
ST01551CH-D |
Installation of a Honeywell/AlliedSignal Mark VIII Enhanced Ground Proximity Warning System. |
| Dassault |
F 50 Series |
ST01556CH-D |
Installation of Dual Universal Avionics UNS-1D/1D+ GPS Flight Management Systems. |
| 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 |
ST01574CH-D |
Installation of a Rockwell Collins TCAS 4000 Traffic and Collision Avoidance System. |
| 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 |
ST01576CH-D |
Installation of a Collins Pro Line 21 Continuum Retrofit Integrated Avionics System. |
| Dassault |
F 50 Series |
ST01578CH-D |
Installation of a Collins Pro Line 21 Continuum Retrofit Integrated Avionics System. |
| Dassault |
F 20 Series |
ST01579CH-D |
Installation of a Honeywell MK-VIII Enhanced Ground Proximity Warning System (EGPWS). |
| 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). |
| Gulfstream |
Multiple |
ST01635CH |
Certification of Reduced Vertical Separation Minimum (RVSM) operational capability. |
| Cessna |
Multiple |
ST01636CH |
Certification of Reduced Vertical Separation Minimum (RVSM) operational capability. |
| Learjet |
Multiple |
ST01662CH-D |
Installation of a Honeywell Mark VIII Enhanced Ground Proximity Warning System, EGPWS with video display of terrain |
| Dassault |
F 10 Series |
ST01723CH |
Certification of Reduced Vertical Separation Minimum (RVSM) operational capability. |
| Dassault |
F 900 Series |
ST01757CH-D |
Installation of a cabin interior and in-flight entertainment system. |
| Gulfstream |
Multiple |
ST01793CH-D |
Installation of a Universal Avionics Multi-Function Display MFD-640. |
| Dassault |
F 10 Series |
ST01806CH |
Certification of Reduced Vertical Separation Minimum (RVSM) operational capability. |
| Dassault |
F 50 Series |
ST01849CH-D |
Installation of a Cabin Interior and In-Flight Entertainment System. |
| Israel Aerospace |
Astra |
ST01854CH-D |
Installation of an Innovative Solutions & Support (IS&S) Air Data Display Unit and Standby Altimeter. |
| Dassault |
Multiple |
ST01933CH-D |
Installation of Honeywell Runway Awareness and Advisory System (RAAS). |
| Dassault |
Multiple |
ST01933CH-D |
Installation of Honeywell Runway Awareness and Advisory System (RAAS). |
| Gulfstream |
Multiple |
ST01990CH |
Installation of a Honeywell AZ-960 Air Data System with Honeywell BA-250 (pilot) altimeters. |
| Dassault |
F 50 Series |
ST01991CH |
Installation of an L3 Communications (Fairchild) Model F1000 Flight Data Recorder (FDR) system. |
| 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. |
| Lockheed |
Jetstar |
ST02038CH-D |
Installation of Honeywell N1 Digital Electronic Engine Controls (DEEC) |
| Dassault |
F 50 Series |
ST02059CH-D |
Modification of engine cowling to install a Sight Glass. |
| Israel Aerospace |
1124 Series |
ST02150CH-D |
Installation of a Honeywell CAS-67A Traffic and Collision Avoidance System (TCAS II) |
| Israel Aerospace |
Astra |
ST02163CH-D |
Installation of a Honeywell Mark VIII Enhanced Ground Proximity Warning System. |
| Dassault |
F 20 Series |
ST02167CH-D |
Installation of a Rockwell Collins IDS-3000 Integrated Display System. |
| Hawker |
800 Series |
ST02452CH-D |
Installation of a Collins IFIS-5000 Integrated Flight Information System. |
| Bombardier |
Challenger Series |
ST02602CH-D |
Installation of a Chelton HGA-7000 High Gain Antenna. |
| Embraer |
EMB-135LR |
ST02656CH-D |
Reconfiguration of the cabin seating arrangement. |
| 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 |
ST02756CH-D |
Installation of an in flight entertainment (IFE) system |
| Embraer |
Multiple |
ST02803CH-D |
Installation of a Honeywell KHF-1050 HF System |
| Dassault |
F 50 Series |
ST02817CH-D |
Installation of Interior Cabin Arrangement to include Single or Dual Aft Divans |
| Dassault |
Multiple |
ST02824CH-D |
Installation of Cabin Emergency LED Lights |
| Dassault |
Multiple |
ST02837CH-D |
Installation of a Honeywell DU-875 display. |
| Embraer |
Multiple |
ST02882CH-D |
Installation of a Honeywell Flight Management System (FMS #2). |
| Gulfstream |
GIV |
ST02911CH-D |
Installation of an Interior Reconfiguration. |
| Dassault |
F 50 Series |
ST02912CH-D |
Installation of an Interior Refurbishment and a Pocket Door. |
| Gulfstream |
GV |
ST02922CH-D |
Installation of an Aircell Axxess Iridium Phone System with a True North Express WiFi System. |
| Dassault |
Multiple |
ST02960CH-D |
Installation of Hutchinson Aerospace Enhanced Thermal and Acoustic Insulation System (TAIS). |
| Boeing |
B757 Series |
ST03018CH-D |
Installation of Gogo ATG-5000 |
| Gulfstream |
Multiple |
ST03033CH-D |
Installation of a True North Simphone System with Optional Swift Broadband, Handsets and Inmarsat Filter. |
| Gulfstream |
GV |
ST03038CH-D |
Reconfiguration of a Cabin Floorplan Arrangement. |
| Dassault |
Multiple |
ST03064CH-D |
Upgrade of the Honeywell MK V EGPWS to include the Runway Safety Package. |
| Dassault |
F 900EX |
ST03068CH-D |
Reconfiguration of Cabin Floor Plan Arrangement |
| Dassault |
Multiple |
ST03079CH-D |
Installation of a Jump Seat |
| Dassault |
F 20 Series |
ST03113CH-D |
Installation of a Left Hand Divan |
| Embraer |
Multiple |
ST03158CH-D |
Installation of a Reconfiguration of a Cabin Floorplan |
| Hawker |
Multiple |
ST03185CH-D |
Activation of a TrueNorth Avionics, Inc. Simphone WiFi System |
| Embraer |
E170 Series |
ST03225CH |
Installation of a Portable ELT and Modification of Interior Placards |
| Bombardier |
Global Express |
ST03234CH |
Reconfiguration of Cabin Floorplan Arrangement |
| Dassault |
F 20 Series |
ST03246CH |
Upgrade of Rockwell Collins Electronic Flight Instrument System (EFIS-85) for GPS Scaling |
| Boeing |
B737 Series |
ST03267CH |
Activation of a Satcom Direct Wi-Fi System |
| Bombardier |
Global Express |
ST03274CH |
Activation of an 802.11 a/b/g/n WiFi System |
| Bombardier |
Multiple |
ST03274CH |
Activation of a WiFi System |
| Bombardier |
Global Express |
ST03293CH |
Upgrade of the Honeywell MK V EGPWS to include the Runway Safety Package |
| Dassault |
F 50 Series |
ST03344CH |
Installation of an Airshow 500 Passenger Flight Information System |
| Dassault |
Multiple |
ST03350CH |
WI-FI Activation |
| Dassault |
Multiple |
ST03431CH |
Upgrade of TCAS to Software V7.1 |
| Bombardier |
Challenger Series |
ST04033CH |
Upgrade of TCAS to Software V7.1 |
| Dassault |
Multiple |
ST04072CH |
Installation of an L-3 Avionics Systems GH-3900 Electric Standby Instrument System (ESIS) |
| Airbus |
A319- model 115 |
ST04118CH |
Installation of a CTT Humidification System |
| Dassault |
Multiple |
ST04140CH |
Installation of a Honeywell JetWave System |
| Gulfstream |
GIV |
ST04162CH |
Installation of a Honeywell JetWave System with associated Ka-Band Radome |
| Dassault |
Falcon 7X |
ST04170CH |
Activation of a WiFi System |
| Gulfstream |
GV |
ST04236CH |
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 |
ST04276CH |
Installation of a Honeywell JetWave System with associated Ka-Band Radome |
| Bombardier |
Multiple |
ST04281CH |
Installation of a Satcom Direct Router System |
| Gulfstream |
Multiple |
ST04283CH |
Activation of a WiFi System |
| Bombardier |
Multiple |
ST04293CH |
Installation of a Honeywell JetWave System |
| Dassault |
Falcon 2000 |
ST04305CH |
Installation of an L3 Avionics Systems GH-3900 Electronic Standby Instrument System |
| Dassault |
Multiple |
ST04305CH |
Installation of an L-3 Avionics Systems GH-3900 Electronic Standby Instrument System |
| Embraer |
Multiple |
ST04316CH |
Installation of a Smartsky System |
| Dassault |
Multiple |
ST09017CH-T |
Installation of an L-3 Avionics Systems GH-3900 Electronic Standby Instrument System |
| Dassault |
F 20 Series |
ST1445CH-D |
Installation of Honeywell N1 Digital Electronic Engine Control (DEEC) |
| Cessna |
550 Series |
ST183CH |
Installation of a Fairchild model F800 digital flight data recorder. |
| Cessna |
650 series |
ST242CH |
Installation of Sundstrand Mark VI Ground Proximity Warning System. |
| Dassault |
F 20 Series |
ST274CH |
Installation of a Bendix/King CAS67TCAS II system with dual MST-67 Mode S transponders. |
| Dassault |
F 20 Series |
ST274CH-D |
Installation of a Honeywell CAS 67 TCAS II System. |
| Hawker |
800A |
ST285CH |
Installation of Sundstrand Mark VI ground proximity warning system. |
| 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 |
Multiple |
ST300CH |
Installation of a Sundstrand Mark VI GPWS. |
| Cessna |
Multiple |
ST301CH |
Installation of an AlliedSignal CAS-67A TCAS II system. |
| Gulfstream |
Multiple |
ST317CH |
Installation of Bendix/King CAS-66A traffic alert and collision avoidance system (TCAS I). |
| Dassault |
F 50 Series |
ST334CH-D |
Installation of an AlliedSignal avionics MK-V, Enhanced Ground Proximity Warning System. |
| Cessna |
560 series |
ST336CH-D |
Installation of an AlliedSignal Avionics Mark VII Ground Proximity Warning System with Windshear. |
| Dassault |
F 900 Series |
ST337CH-D |
Installation of a Bendix/King model CAS 67A Traffic Collision Avoidance System (TCAS II). |
| Dassault |
F 50 Series |
ST345CH-D |
Installation of an AlliedSignal Avionics MK-V Enhanced Ground Proximity Warning System. |
| Hawker |
Multiple |
ST348CH-D |
Installation of a Sundstrand Mark VI Ground Proximity Warning System. |
| Hawker |
Multiple |
ST349CH-D |
Installation of APU Access Panels. |
| Dassault |
Multiple |
ST4048CH |
Upgrade of TCAS V7.0 Software to V7.1 and DIU Installation |
| 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 900EX |
ST4049CH |
Upgrade of TCAS V7.0 Software to V7.1 |
| Dassault |
Multiple |
ST4049CH |
Upgrade of TCAS V7.0 Software to V7.1 |
| Dassault |
F 50 Series |
ST461CH-D |
Installation of Rockwell Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS II). |
| Gulfstream |
Multiple |
ST462CH-D |
Installation of aircraft cabin interior furnishings and cabinetry. |
| Bombardier |
Challenger Series |
ST471CH |
Installation of an Allied Signal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II). |
| Dassault |
F 20 Series |
ST491CH |
Installation of an AlliedSignal CAS-66A Traffic Alert and Collision Avoidance System (TCAS I). |
| Hawker |
700A |
ST501CH |
Installation of AlliedSignal CAS-67A traffic alert and collision avoidance system (TCAS II). |
| Dassault |
F 20 Series |
ST540CH-D |
Installation of a Universal Avionics Systems Corp. Dual UNS-1D Flight Management System. |
| Cessna |
650 series |
ST541CH-D |
Installation of an AlliedSignal Avionics MK-VII, enhanced ground proximity warning system. |
| Dassault |
F 50 Series |
ST542CH-D |
Installation of an AlliedSignal Avionics MK-V Enhanced Ground Proximity Warning System. |
| Hawker |
Multiple |
ST546CH-D |
Installation of an AlliedSignal Avionics, Dual GNS-XLS, Flight Management System with GPS as a primary means of navigation |
| Dassault |
F 50 Series |
ST547CH-D |
Installation of Honeywell LASEREF Inertial Reference Systems. |
| Cessna |
650 series |
ST568CH-D |
Installation of a Dual Universal Avionics UNS-1B, Flight Management System with GPS as a primary means of navigation. |
| Hawker |
Multiple |
ST569CH-D |
Installation of a Dual Universal Avionics UNS-1D, Flight Management System with GPS as a primary means of navigation. |
| Lockheed |
Jetstar |
ST56CH-D |
Installation of a Bendix TCAS II system. (1329 series Modified by STC SA2326SW) |
| Hawker |
Multiple |
ST574CH-D |
Installation of a Dual Honeywell NZ-2000, Flight Management System, with GPS as a primary means of navigation. |
| Learjet |
31 Series |
ST576CH-D |
Installation of an AlliedSignal Avionics, Bendix/King CAS 67A TCAS II Traffic Collision Avoidance System. |
| Dassault |
F 50 Series |
ST583CH |
Installation of AlliedSignal CAS-67A Traffic Alert and Collision Avoidance System (TCAS II). |
| Gulfstream |
Multiple |
ST598CH |
Installation of an AlliedSignal GNS-XLS Flight Management System. |
| Hawker |
Multiple |
ST71CH-D |
Installation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System with Collins TDR-94D Mode S Transponders. |
| Gulfstream |
Multiple |
ST75CH |
Installation of Sundstrand Mark VI ground proximity warning 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 |
Falcon 7X |
ST04546CH |
Installation of an Aviation Clean Air (ACA) system |
| Gulfstream |
GV-SP |
ST04539CH |
Reconfigure of Cabin Floor Plan |
| Dassault |
Falcon 2000 |
ST04532CH |
Installation of an Aviation Clean Air (ACA) system |
| Bombardier |
Challenger 300 / 350 |
ST04508CH |
Installation of KuSat-2000 Tail mounted SATCOM |
| Textron |
650 Series |
ST04503CH |
Upgrade Dual FMZ-2000 / NZ 6.1 with WAAS-LPV |
| Bombardier |
Global / Express |
ST04488CH |
Installation of a Honeywell MCS-7120 SATCOM |
| Gulfstream |
G-IV, GV |
ST04432CH |
Upgrade of a Honeywell LASERREF Inertial Reference System |
| Bombardier |
Challenger Series |
ST04400CH |
Upgrade of Existing Cobham Aviator 700 Inmarsat to Aviator 700D System |
| Gulfstream |
GIV-X |
ST04478CH |
Installation of KuSat-2000 Tail mounted SATCOM |
| Gulfstream |
GV, GV-SP |
ST04277CH |
Installation of Ontonomy Camera System |
