# Gates Lear Jet 36A - Type: Aircraft model (FAA registry) - Registry code: 5170603 - Manufacturer (registry): GATES LEAR JET - Model: 36A - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 10 - Weight class: 12,500 to 19,999 lb - Cruise speed: 400 mph - Certification: Type certificated - Data sheet: [TCDS A10CE](https://openairdocs.org/tcds/A10CE) (OpenAirDocs) - Holder: Learjet Inc. - Registered aircraft: 21 - Page: https://openairdocs.org/model/gates-lear-jet-36a Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2022-05-01](https://openairdocs.org/ad/2022-05-01): Spoilers · Learjet 35, 35A (C-21A), 36 and 5 more. Effective Mar 9, 2022 - [AD 2018-19-04](https://openairdocs.org/ad/2018-19-04): TE Flap Control System · Learjet 28, 29, 31 and 9 more. Effective Oct 23, 2018 - [AD 2017-04-15](https://openairdocs.org/ad/2017-04-15): Flight controls · Learjet 36A. Effective Apr 4, 2017 - [AD 2007-17-17](https://openairdocs.org/ad/2007-17-17): Unsealed gaps on the pylon side of the engine firewall · Learjet 31, 31A, 35 and 7 more. Effective Oct 2, 2007 - [AD 2007-04-18](https://openairdocs.org/ad/2007-04-18): Left- and right-hand standby fuel pump switches · Learjet 23, 24, 24A and 25 more. Effective Mar 23, 2007 - [AD 2004-03-08](https://openairdocs.org/ad/2004-03-08): Drag Angles of Fuselage and Engine Pylons · Learjet 31, 31A, 35 and 3 more. Effective Mar 15, 2004 - [AD 2001-07-11](https://openairdocs.org/ad/2001-07-11): Main Landing Gear Tires · Learjet 23, 24, 24A and 25 more. Effective May 1, 2001 - [AD 2000-24-19](https://openairdocs.org/ad/2000-24-19): Flightcrew Oxygen Masks · Learjet 35, 35A (C-21A), 36 and 1 more. Effective Jan 4, 2001 - [AD 95-19-04 R1 RES](https://openairdocs.org/ad/95-19-04-R1-RES): Omega Navigation System · Learjet 35, 35A (C-21A), 36 and 4 more. Effective Mar 27, 2000 - [AD 96-19-13](https://openairdocs.org/ad/96-19-13): Operating Mach Limit · Learjet 35, 35A (C-21A), 36 and 1 more. Effective Oct 22, 1996 - [AD 95-22-01](https://openairdocs.org/ad/95-22-01): Fluorescent Lighting System · Aerospace Lighting Fluorescent lighting systems, A310-203, A310-204 and 74 more. Effective Dec 4, 1995 - [AD 95-20-03](https://openairdocs.org/ad/95-20-03): Airplane Flight Manual (AFM) - Altitude Limitations · Learjet 24, 24A, 24B and 24 more. Effective Nov 2, 1995 - [AD 92-19-12](https://openairdocs.org/ad/92-19-12): Oxygen Plumbing & Map Light Wires · Learjet 23, 24, 24A and 22 more. Effective Nov 17, 1992 - [AD 91-03-08](https://openairdocs.org/ad/91-03-08): Fluorescent Lighting Systems · Learjet 31, 35, 35A (C-21A) and 5 more. Effective Feb 12, 1991 - [AD 89-12-01](https://openairdocs.org/ad/89-12-01): Drag Chute Riser · Learjet 24, 24A, 24B and 22 more. Effective Jul 3, 1989 - [AD 86-05-05 R1](https://openairdocs.org/ad/86-05-05-R1): Battery Vent System · Learjet 23, 24, 24A and 20 more. Effective Jan 19, 1988 - [AD 87-04-06](https://openairdocs.org/ad/87-04-06): Autopilot/Flight Director · Learjet 35, 35A (C-21A), 36 and 4 more. Effective Mar 9, 1987 - [AD 87-02-06](https://openairdocs.org/ad/87-02-06): Engine Mounts · Learjet 35, 35A (C-21A), 36 and 4 more. Effective Feb 6, 1987 - [AD 86-22-05](https://openairdocs.org/ad/86-22-05): Flap Sector Mounting Brackets Inspection · Learjet 23, 24, 24A and 23 more. Effective Nov 10, 1986 - [AD 82-01-05 R2](https://openairdocs.org/ad/82-01-05-R2): Stall Warning Accelerometer Unit · Learjet 23, 24, 24A and 16 more. Effective Apr 10, 1986 - [AD 85-16-04](https://openairdocs.org/ad/85-16-04): Aileron · Raisbeck Mark IV performance system (STC SA766NW). Effective Sep 6, 1985 - [AD 80-19-11 R1](https://openairdocs.org/ad/80-19-11-R1): Automatic Flight Control and Stall Warning Systems · Learjet 23, 24, 24A and 20 more. Effective May 20, 1985 - [AD 84-19-06](https://openairdocs.org/ad/84-19-06): Tab Control System · Learjet 24, 24A, 24B and 22 more. Effective Oct 22, 1984 - [AD 79-08-01 R1](https://openairdocs.org/ad/79-08-01-R1): Thrust Reversers · Learjet 35, 35A (C-21A), 36 and 1 more. Effective Apr 19, 1982 - [AD 81-13-07](https://openairdocs.org/ad/81-13-07): Change to AFM Fuel Starvation · Learjet 23, 24, 24A and 20 more. Effective Jun 25, 1981 - [AD 80-19-09 R1](https://openairdocs.org/ad/80-19-09-R1): Jet Pumps · Learjet 23, 24, 24A and 20 more. Effective Dec 11, 1980 - [AD 80-17-11](https://openairdocs.org/ad/80-17-11): Airspeed Warning Placard · Learjet 35, 35A (C-21A), 36 and 1 more. Effective Aug 28, 1980 - [AD 80-07-09](https://openairdocs.org/ad/80-07-09): Cabin Main Entrance Upper Door · Learjet 23, 24, 24A and 20 more. Effective May 1, 1980 - [AD 80-06-02](https://openairdocs.org/ad/80-06-02): Electrical System · Learjet 35, 35A (C-21A), 36 and 1 more. Effective Mar 24, 1980 - [AD 78-16-03](https://openairdocs.org/ad/78-16-03): Refrigeration Condenser Fan · Learjet 23, 24, 24A and 18 more. Effective Aug 17, 1978 Historical (superseded or no longer in force): - [AD 95-19-04](https://openairdocs.org/ad/95-19-04) (historical): Omega Navigation System · Learjet 35, 35A (C-21A), 36 and 4 more. Effective Oct 12, 1995 ## Information bulletins (advisory) (4) - [SAIB 2026-07](https://openairdocs.org/saib/2026-07): MAIN LANDING GEAR ATTACH SECTION, Trunnion Pins. Issued Mar 19, 2026 - [SAIB NM-16-24](https://openairdocs.org/saib/NM-16-24): Fuselage: Main Plate/Skin. Issued Sep 15, 2016 - [SAIB NM-13-38](https://openairdocs.org/saib/NM-13-38): Flight Controls Control Column Section. Issued Jun 24, 2013 - [SAIB NM-11-48](https://openairdocs.org/saib/NM-11-48): Ice and Rain Protection: Wing Transverse Duct Assembly. Issued Aug 22, 2011 ## Registered aircraft (21) - [N116MA](https://openairdocs.org/aircraft/N116MA): [Fsa Aerospace Inc Trustee](https://openairdocs.org/faa-owner/FSA%20AEROSPACE%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1977, S/N 029 - [N132LJ](https://openairdocs.org/aircraft/N132LJ): [Aery Aviation LLC](https://openairdocs.org/faa-owner/AERY%20AVIATION%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1977, S/N 032 - [N136DH](https://openairdocs.org/aircraft/N136DH): [Csc Delaware Trust Co Trustee](https://openairdocs.org/faa-owner/CSC%20DELAWARE%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1977, S/N 036 - [N160GC](https://openairdocs.org/aircraft/N160GC): [C2d LLC](https://openairdocs.org/faa-owner/C2D%20LLC), [Cartersville, GA](https://openairdocs.org/faa-place/GA/Cartersville), S/N 36A-030 - [N16FN](https://openairdocs.org/aircraft/N16FN): [Gh Equipment LLC](https://openairdocs.org/faa-owner/GH%20EQUIPMENT%20LLC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), built 1976, S/N 027 - [N17A](https://openairdocs.org/aircraft/N17A): [Valiair Limited Co Trustee](https://openairdocs.org/faa-owner/VALIAIR%20LIMITED%20CO%20TRUSTEE), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper), built 1980, S/N 046 - [N18FN](https://openairdocs.org/aircraft/N18FN): [Gh Equipment LLC](https://openairdocs.org/faa-owner/GH%20EQUIPMENT%20LLC), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), built 1974, S/N 037 - [N20GJ](https://openairdocs.org/aircraft/N20GJ): [Global Jetcare Inc](https://openairdocs.org/faa-owner/GLOBAL%20JETCARE%20INC), [Brooksville, FL](https://openairdocs.org/faa-place/FL/Brooksville), S/N 026 - [N302EW](https://openairdocs.org/aircraft/N302EW): [Aery Aviation LLC](https://openairdocs.org/faa-owner/AERY%20AVIATION%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1976, S/N 024 - [N31GJ](https://openairdocs.org/aircraft/N31GJ): [Global Jetcare Inc](https://openairdocs.org/faa-owner/GLOBAL%20JETCARE%20INC), [Brooksville, FL](https://openairdocs.org/faa-place/FL/Brooksville), built 1976, S/N 022 - [N32PA](https://openairdocs.org/aircraft/N32PA): [Phoenix Air Group Inc](https://openairdocs.org/faa-owner/PHOENIX%20AIR%20GROUP%20INC), [Cartersville, GA](https://openairdocs.org/faa-place/GA/Cartersville), built 1976, S/N 025 - [N363PJ](https://openairdocs.org/aircraft/N363PJ): [Premier Jets Inc](https://openairdocs.org/faa-owner/PREMIER%20JETS%20INC), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1977, S/N 038 - [N41GJ](https://openairdocs.org/aircraft/N41GJ): [Global Jetcare Inc](https://openairdocs.org/faa-owner/GLOBAL%20JETCARE%20INC), [Brooksville, FL](https://openairdocs.org/faa-place/FL/Brooksville), built 1984, S/N 055 - [N51GJ](https://openairdocs.org/aircraft/N51GJ): [Global Jetcare Inc](https://openairdocs.org/faa-owner/GLOBAL%20JETCARE%20INC), [Brooksville, FL](https://openairdocs.org/faa-place/FL/Brooksville), built 1976, S/N 018 - [N527PA](https://openairdocs.org/aircraft/N527PA): [Phoenix Air Group Inc](https://openairdocs.org/faa-owner/PHOENIX%20AIR%20GROUP%20INC), [Cartersville, GA](https://openairdocs.org/faa-place/GA/Cartersville), built 1976, S/N 019 - [N545PA](https://openairdocs.org/aircraft/N545PA): [Phoenix Air Group Inc](https://openairdocs.org/faa-owner/PHOENIX%20AIR%20GROUP%20INC), [Cartersville, GA](https://openairdocs.org/faa-place/GA/Cartersville), S/N 36A-028 - [N56PA](https://openairdocs.org/aircraft/N56PA): [Phoenix Air Group Inc](https://openairdocs.org/faa-owner/PHOENIX%20AIR%20GROUP%20INC), [Cartesville, GA](https://openairdocs.org/faa-place/GA/Cartesville), built 1976, S/N 023 - [N62PG](https://openairdocs.org/aircraft/N62PG): [Phoenix Air Group Inc](https://openairdocs.org/faa-owner/PHOENIX%20AIR%20GROUP%20INC), [Cartersville, GA](https://openairdocs.org/faa-place/GA/Cartersville), built 1977, S/N 031 - [N71CK](https://openairdocs.org/aircraft/N71CK): [Kalitta Charters LLC](https://openairdocs.org/faa-owner/KALITTA%20CHARTERS%20LLC), [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti), built 1977, S/N 035 - [N81GJ](https://openairdocs.org/aircraft/N81GJ): [Global Jetcare Inc](https://openairdocs.org/faa-owner/GLOBAL%20JETCARE%20INC), [Brooksville, FL](https://openairdocs.org/faa-place/FL/Brooksville), built 1981, S/N 047 - [N99RS](https://openairdocs.org/aircraft/N99RS): [Casmos LLC](https://openairdocs.org/faa-owner/CASMOS%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 039 ## NTSB investigations (6) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB WPR23FA185](https://openairdocs.org/ntsb/WPR23FA185), May 10, 2023: Gates Lear Jet 36A (N56PA), San Clemente Island, CA, destroyed, 3 fatal. Probable cause: The pilots’ loss of airplane control following a catastrophic fire that started on the left side of the aft equipment bay (tail cone). The fire likely initiated from a leak from the left fuel motive… - [NTSB ENG07IA030](https://openairdocs.org/ntsb/ENG07IA030), Jun 4, 2007: Learjet 36 (N136DH), Bismarck, ND, incident, minor damage. Probable cause: A total loss of engine power during takeoff due to the right engine sustaining a fractured fan blade after the ingestion of a mallard duck. Some liberated fan blade fragments were uncontained,… - [NTSB NYC07LA087](https://openairdocs.org/ntsb/NYC07LA087), Mar 26, 2007: Gates Learjet 36A (N527PA), Newport News, VA, substantial damage. Probable cause: The failure of the landing gear tires due to foreign object damage (FOD) on the runway. Contributing to the accident was the failure of the drag chute. - [NTSB SEA03LA010](https://openairdocs.org/ntsb/SEA03LA010), Dec 3, 2002: Learjet 36A (N546PA), Astoria, OR, destroyed. Probable cause: Collision with an elk during the takeoff roll. Factors include dark night VFR conditions. - [NTSB CHI97WA039](https://openairdocs.org/ntsb/CHI97WA039), Dec 6, 1996: Learjet 36 (N14TX), Stephenville, Ireland, destroyed, 2 fatal - [NTSB FTW88MA047](https://openairdocs.org/ntsb/FTW88MA047), Jan 8, 1988: Gates Learjet 36A (N79SF), Monroe, LA, destroyed, 2 fatal ## FAA accident and incident reports (15) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20230510005119A](https://openairdocs.org/incident/20230510005119A), May 10, 2023: Gates Lear Jet 36A (N56PA), CA, Destroyed, 3 fatal. Lead of a flight two aircraft, collaborative effort for u.s navy training. The two aircraft took off from n.a.s pt mugu and joined up at 15,000 feet then… - [Incident 20230315002779I](https://openairdocs.org/incident/20230315002779I), Mar 15, 2023: Gates Lear Jet 36A (N41GJ), Houston, TX, Minor damage. Aircraft departed bangor, me kbgr enroute to khou Houston hobby on 135 medevac flight. During takeoff roll, crew noticed “bump”, left anti-skid lights right… - [Incident 20200207019439I](https://openairdocs.org/incident/20200207019439I), Feb 7, 2020: Gates Lear Jet 36A (N363PJ), Hillsboro, OR, Minor damage. Minor damage on the underside of the right wing fuel tip tank. Damage included scraping parallel to longitudinal axis of aircraft. Unknown how or when damage… - [Incident 20131219025049I](https://openairdocs.org/incident/20131219025049I), Dec 19, 2013: Gates Lear Jet 36A (N82GG), No damage. The aircraft was repositioning from oakland, CA to manila, philippines. The aircraft departed marjuro after a fuel stop at approximately 0900 on dec 19, 2013.… - [Incident 20090915018409I](https://openairdocs.org/incident/20090915018409I), Sep 15, 2009: Lear 36A (N62PG), Lake Charles, LA, Minor damage. Pilot statement is that copilot was flying and landed with a "crab" and failed to straighten out prior to touchdown. The aircraft was landing runway 15 and… - [Accident 20070326003499A](https://openairdocs.org/incident/20070326003499A), Mar 26, 2007: Lear 36A (N527PA), Newport News, VA, Substantial damage. (-23) March 26, 2007 lr JET-36A, N527PA was operated by phoenix air group as flight 327. At approximately 0725 EDT N527PA departed Newport News/Williamsburg… - [Incident 20051119032529I](https://openairdocs.org/incident/20051119032529I), Nov 19, 2005: Lear 36A (N527PA), Newport News, VA. (-23) The aircraft returned to the Newport News, Virginia, airport (phf) from a target tow mission for the military and initiated an approach to land on rwy 7.… - [Incident 20050228003269I](https://openairdocs.org/incident/20050228003269I), Feb 28, 2005: Lear 36A (N136DH), Lincolnton, NC. (-23) Aircraft landed on wet/slushy runway late at night. Aircraft went off end of runway 300 feet. Fixed base operator was closed. Last runway report… - [Accident 20021203033119A](https://openairdocs.org/incident/20021203033119A), Dec 3, 2002: Lear 36A (N546PA), Astoria, OR, Destroyed. (-23) On Tuesday dec 3, 2002 at 0612 am, Lear jet N546PA departed Astoria, OR airport on an IFR flight under part 91. The airport was VFR with a 3500 foot… - [Incident 20000703034109I](https://openairdocs.org/incident/20000703034109I), Jul 3, 2000: Lear 36A (N432JW), San Francisco, CA. (-23)Occurence happened during descent. Pilots heard a loud rumbling noise, which they though was airframe noise,then the #1 engine low engine-oil pressure… - [Incident 20000130000059I](https://openairdocs.org/incident/20000130000059I), Jan 30, 2000: Lear 36A (N32AJ), Reno, NV. (-23) The pilot reported: on 01/03/2000, at approx, 0345Z, I departed rno airport. Takeoff and initial climbout were normal. While climbing through approx,… - [Accident 19961206042479A](https://openairdocs.org/incident/19961206042479A), Dec 6, 1996: Lear 36A (N14TX), Stephenville, Destroyed, 2 fatal. (.19) On December 6, 1996, at about 0430 eastern standard time (EST), a Learjet 36, N14TX, registered to chrysler aviation, inc., of van nuys, California, ,… - [Incident 19920518018599I](https://openairdocs.org/incident/19920518018599I), May 18, 1992: Lear 36A (N71CK), Albany, NY. Fuel imbalance en route. Diverted and landed. Added fuel to left tank. Pilot blamed left standby pump. - [Accident 19880108000359A](https://openairdocs.org/incident/19880108000359A), Jan 8, 1988: Lear 36A (N79SF), Monroe, LA, Destroyed, 2 fatal. Collided with terrain on a ILS night approach. High speed and high descent rate. Had nose up and wing down atitude. - [Incident 19880103006329I](https://openairdocs.org/incident/19880103006329I), Jan 3, 1988: Lear 36A (N79SF), Honolulu, HI. Total fuel exhaustion due to headwinds. Executed dead stick landing on runway. Flight was non stop from California. ## Service difficulty reports (49) As reported by operators and repair stations, by the model named in the report. - [SDR CMWA2020060300001](https://openairdocs.org/sdr/CMWA2020060300001), May 28, 2020: LIGHT. BURNED OUT. ON APPROACH TO HNL PILOT NOTED NO LEFT MAIN GEAR DOWN GREEN LIGHT INDICATING. CREW PROCEEDED TO USE ALTERNATE GEAR EXTENSION PROCEDURE, AND LANDED WITHOUT INCID - [SDR 2020FA0000155](https://openairdocs.org/sdr/2020FA0000155), Feb 6, 2020: FUEL TANK. DAMAGED. LOWER AFT PORTION OF RIGHT TIP TANK DAMAGED BY BEING SCRAPED ON LANDING. - [SDR KC8A2018090409118](https://openairdocs.org/sdr/KC8A2018090409118), Aug 28, 2018: MODULATING VALVE. FAULTY. TROUBLESHOT EXCESSIVE HEAT IN CABIN, FOUND LEFT ENGINE MODULATING SHUT-OFF VALVE DEFECTIVE, STAYING IN FULL PRESSURE BLEED. VALVE WAS NOT REGULATING CORRECTLY. - [SDR KC8A201808300018](https://openairdocs.org/sdr/KC8A201808300018), Aug 28, 2018: UNKNOWN. SMOKE. AFTER TAKE OFF, CREW NOTICED EXCESSIVE HEAT IN CABIN, SMOKE IN CABIN COMING FROM ARM REST DUCTING OUTLETS. BOTH ENGINE MODULATING SHUT OFF VALVES SELECTED CLOSE - [SDR 2016FA0000501](https://openairdocs.org/sdr/2016FA0000501), Sep 29, 2016: VERTICAL GYRO. FAILED. FAILURE OF VG-206D VERTICAL DISPLACEMENT GYRO RESULTING IN PILOTS PRIMARY ADI INDICATING +15 DEGREES OF ROLL. - [SDR BHKA20160506002](https://openairdocs.org/sdr/BHKA20160506002), May 3, 2016: SENSING ELEMENT. DEFECTIVE. ON 3 MAY 2016 AT APPROX 2100 Z WITH 2 SOULS ONBOARD, 1 HR INTO FLIGHT WHILE OPERATING AT 24,000 FT MSL, THE NR 2 RT ENG FIRE & MSTR WARN LIGHTS ILLUMINATED. RED - [SDR BHKA20160506001](https://openairdocs.org/sdr/BHKA20160506001), May 2, 2016: WARNING SYSTEM. FALSE ACTIVATION. DURING CLIMB OUT PASSING THROUGH 13,000 FEET MSL, THE NR 2 RT ENG FIRE PULL LIGHT ILLUMINATED IN THE T HANDLE ACCOMPANIED BY FLASHING MSTR WARNING LIGHTS. THE R - [SDR CA151015015](https://openairdocs.org/sdr/CA151015015), Oct 12, 2015: THROTTLE CABLE. FAILED. (CAN) DURING CLIMBOUT LT ENGINE HAD NO RESPONSE TO POWER LEVER MOVEMENT. FLIGHT CREW QUICKLY REALIZED THAT THE LT ENGINE WAS UNRESPONSIVE AND STUCK AT HIGH POWE - [SDR G1IA20150602001](https://openairdocs.org/sdr/G1IA20150602001), May 29, 2015: BLOWER MOTOR. FAILED. FAR 135.415 REPORT. ON CLIMB APPROX 10 MILES OUT FROM THE AIRPORT THEY SMELLED SMOKE ALL OVER THE COCKPIT & CABIN, OXYGEN MASKS WERE DEPLOYED. THEY DECLARED AN - [SDR 2014FA0000006](https://openairdocs.org/sdr/2014FA0000006), Jan 5, 2014: GENERATOR. FAILED. MECHANIC REMOVED RT ENGINE COWL AND FOUND SIGNIFICANT INTERNAL AND EXTERNAL DAMAGE TO THE RT GENERATOR. AFT SECTION OF THE GENERATOR CASE WAS SEPARATED, GENERAT - [SDR CA131215001](https://openairdocs.org/sdr/CA131215001), Dec 13, 2013: WHEEL. FAILED. (CAN) DURING A POST FLIGHT INSPECTION, CREW NOTICED A FLAT TIRE AND THEN NOTICED A LARGE PORTION OF THE INBD WHEEL HALF MISSING. THERE WERE NO SIGNS OF OVERHEAT - [SDR KC8A20131104010](https://openairdocs.org/sdr/KC8A20131104010), Nov 3, 2013: PUMP. OVERHEATED. MEDICAL CREW NOTICED AN ODOR COMING FROM THE MEDICAL STRETCHER BASE. THEY FOUND THE PRESSURE PUMP WAS GETTING WARM AND ELECTED TO TURN UNIT OFF. ODOR WENT AWAY. - [SDR 2013FA0000273](https://openairdocs.org/sdr/2013FA0000273), May 9, 2013: PACKING. LEAKING. DURING LOW LEVEL TRACK, LEVEL FLIGHT, NOSE GEAR UNSAFE LIGHT CAME ON FOR ABOUT 2 MINUTES. DURING RTB AT ALTITUDE OF 12K, LIGHT CAME ON AGAIN AND HYDRAULIC PRESS - [SDR KC8A20130304001](https://openairdocs.org/sdr/KC8A20130304001), Feb 28, 2013: DOOR SEAL. PINCHED. DURING CRUISE FLIGHT, THE CAPTAIN NOTICED THE CABIN ALTITUDE CLIMBING SLOWLY. THE CABIN ALTITUDE CLIMBED TO THE POINT OF SETTING OFF THE EMERGENCY PRESSURIZATIO - [SDR ESPA2012031403](https://openairdocs.org/sdr/ESPA2012031403), Mar 14, 2012: COMPUTER. DEFECTIVE. ON ROLL OUT, ACFT EXPERIENCED A SHUTTER AND THE CREW THOUGHT THE NOSE TIRE HAD BLOWN, CREW NOTIFIED THE TOWER AND PREPARED THE ACFT FOR AN EMERGENCY LANDING, UP - [SDR CA110923012](https://openairdocs.org/sdr/CA110923012), Sep 22, 2011: PULLEY. OUT OF TOLERANCE. (CAN) DURING A MX WALK AROUND, FOUND A .7500" FREEPLAY IN THE RT AILERON. DURING INVESTIGATION, FOUND THAT THE RT AILERON PULLEY AND SHAFT WERE MOVING INDEPENDE - [SDR ESPADJ20102](https://openairdocs.org/sdr/ESPADJ20102), Oct 7, 2010: CIRCUIT BREAKER. WEAK. DEPARTED ON LIVE LEG, APPROX 12 MINUTES INTO FLIGHT AT FL 220 PITOT HEAT AND LANDING GEAR CIRCUIT BREAKERS POPPED. REQUESTED FL 250 AND ADVISED ATC THAT THERE W - [SDR CA091123001](https://openairdocs.org/sdr/CA091123001), Nov 20, 2009: HOSE. LEAKING. (CAN) UPON DESCENT, PILOTS NOTICED THE HYD PRESSURE WAS AT 0. THEY DECLARED AN EMERGENCY, EXTENDED GEAR USING EMERGENCY AIR BOTTLE AND MADE A SUCCESSFUL LANDING - [SDR KC8AN71CK](https://openairdocs.org/sdr/KC8AN71CK), Mar 13, 2009: DOOR FRAME. CRACKED. DURING ROUTINE AIRCRAFT INSPECTION TWO CRACKS WHERE FOUND IN THE LOWER CABIN DOOR AFT FRAME. ONE CRACK LOCATED IN THE BOTTOM OUTBOARD DOOR CABLE PULLEY BRACKET - [SDR ESPADA20091](https://openairdocs.org/sdr/ESPADA20091), Jan 30, 2009: BEARING. SEPARATED. DURING COMPLIANCE WITH SB TFE731-72-3696 (REPLACEMENT OF AIR/OIL SEPARATOR IN THE ACCESSORY GEARBOX) FOUND THE FWD PART OF THE BALL BEARING CAGE SEPARATED FROM - [SDR ESPADJ2088-1](https://openairdocs.org/sdr/ESPADJ2088-1), Oct 4, 2008: ENGINE. LACK OF LUBE. DEPARTED CARTERSVILLE AIRPORT AND PASSING 2000FT MSL THE MASTER CAUTION AND OIL PRESSURE LIGHTS ILLUMINATED. THE CREW NOTED 0 OIL PRESSURE ON THE LEFT ENGINE AN - [SDR N71CK](https://openairdocs.org/sdr/N71CK), Mar 18, 2008: LIMITER. DAMAGED. DURING CLIMB, THE CREW NOTICED THE CABIN ALTITUDE CLIMBING. FOLLOWING PROCEDURES IN THE AIRCRAFT FLIGHT MANUAL, THE CREW NOTIFIED ATC OF THE PROBLEM AND DESCEND - [SDR 090107](https://openairdocs.org/sdr/090107), Sep 4, 2007: ENGINE. UNKNOWN. DURING CLIMB OUT SHORTLY AFTER TAKEOFF LT ENGINE QUIT. CREW DECLARED AN EMERGENCY WITH DEPARTURE CONTROL, THEY VECTOR AIRPLANE TO PROPER MSA ALTITUDE AND RETURN - [SDR N71CK81407](https://openairdocs.org/sdr/N71CK81407), Aug 13, 2007: FIRE LOOP. OUT OF POSITION. THIS IS AN UPDATE TO THE PREVIOUS SDR DATED 8/13/2007. RT ENGINE FIRE WARNING LIGHT ILLUMINATED DURING FLIGHT. INVESTIGATION FOUND THE AFT FIRE SENSE LOOP IN TH - [SDR N71CK81307](https://openairdocs.org/sdr/N71CK81307), Aug 13, 2007: FIRE WARNING. FALSE ACTIVATION. RT ENGINE HAD A FIRE WARNING LIGHT ILLUMINATE. THE CAUSE OF THE WARNING HAS NOT BEEN DETERMINED AS OF THIS DATE. THERE IS NO INDICATION OF A FIRE OR A HOT SPOT - [SDR 82206N71CK](https://openairdocs.org/sdr/82206N71CK), Aug 21, 2006: O-RING. TORN. ENGINE OIL PRESSURE WAS FLUCTUATING DURING CRUISE. ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE. AIRCRAFT RETURNED TO DEPARTURE. FOUND RT ENGINE OIL TANK FILL - [SDR CA060317002](https://openairdocs.org/sdr/CA060317002), Mar 10, 2006: CONNECTOR. SHORTED. (CAN) AIRCRAFT DEPARTED APPROXIMATELY 30 MINUTES AFTER DEPARTURE SMOKE WAS NOTED UNDER GLARESHIELD AND EMERGENCY LANDING EXECUTED. MAINTENANCE PERSONNEL FOUND S - [SDR KC82006F00002](https://openairdocs.org/sdr/KC82006F00002), Feb 27, 2006: FILLERCAP. LEAKING. RT ENGINE OIL PRESSURE LOW AFTER TAKEOFF. AIRCRAFT RETURNED FOR MAINTENANCE. AFTER ARRIVAL BACK TO THE AIRPORT, PILOT FOUND OIL LEAKING FROM COWLING DRAIN, AND - [SDR KC82006F00001](https://openairdocs.org/sdr/KC82006F00001), Feb 27, 2006: SEAL. TORN. RT ENGINE OIL PRESSURE LOW AFTER TAKEOFF. AC RETURNED FOR MAINTENANCE. AFTER ARRIVAL BACK TO THE AIRPORT, THE PILOT FOUND OIL LEAKING FROM COWLING DRAIN, AND OI - [SDR KC82006F00000](https://openairdocs.org/sdr/KC82006F00000), Dec 27, 2005: WIRE. ARCED. PILOT REPORTED SMOKE IN THE COCKPIT. HE TURNED OF THE GLARESHIELD LIGHTING AND THE SMOKE STOPPED. FOUND GLARESHIELD FLORESCENT TUBE LEAD WIRES ARCING TO GROUND. - [SDR KC82005F00007](https://openairdocs.org/sdr/KC82005F00007), Sep 7, 2005: HOSE. LEAKING. CREW NOTICED A LOSS OF HYDRAULIC PRESSURE. PERFORMED EMERGENCY GEAR EXTENSION AND LANDED WITHOUT INCIDENT. AUX HYDRAULIC PUMP SUPPLIED PRESSURE FOR FLAPS AND BR - [SDR KC82005F00006](https://openairdocs.org/sdr/KC82005F00006), Aug 16, 2005: COMPUTER. ERRATIC. BEFORE TAKEOFF, THE PILOT NOTICED THAT THE ENGINE IDLE AND TAKEOFF RPM ERRATIC IN THE NORMAL ENGINE CONTROL MODE, IN MANUAL ENGINE CONTROL MODE, ENGINE PERFORMA - [SDR KC82003F00002](https://openairdocs.org/sdr/KC82003F00002), Jul 29, 2003: SEAL. LEAKING. PILOT REPORTED RIGHT BLEED AIR LIGHT ALUMINATED DURING FLIGHT. FOUND SEALS WERE LEAKING AND CAUSED THE RT BLEED ANNUNCIATOR TO LIGHT. PYLON AREA WAS INSPECTED I - [SDR 2002FA0000969](https://openairdocs.org/sdr/2002FA0000969), Jul 29, 2002: SWITCH. FAILED. ANEROID SWITCH FAILED SPECIFIC PRESSURE LIMITS. - [SDR 2002FA0000968](https://openairdocs.org/sdr/2002FA0000968), Jul 29, 2002: SWITCH. FAILED. ANEROID SWITCH FAILED SPECIFIC PRESSURE LIMITS. - [SDR 2002FA0000967](https://openairdocs.org/sdr/2002FA0000967), Jul 29, 2002: SWITCH. FAILED. ANEROID SWITCH FAILED SPECIFIC PRESSURE LIMITS. - [SDR 2002FA0000966](https://openairdocs.org/sdr/2002FA0000966), Jul 29, 2002: SWITCH. FAILED. ANEROID SWITCH FAILED SPECIFIC PRESSURE LIMITS. - [SDR 2002FA0000965](https://openairdocs.org/sdr/2002FA0000965), Jul 29, 2002: SWITCH. FAILED. ANEROID SWITCH FAIL SPECIFIC PRESSURE LIMITS. - [SDR 13001N71CK](https://openairdocs.org/sdr/13001N71CK), Feb 2, 2001: COMPUTER. INOPERATIVE. LT ENGINE RPM ROLLED BACK 40 PERCENT DURING CLIMB, UNEVENTFULL LANDING ACCOMPLISHED. REPLACED LEFT ENGINE FUEL COMPUTER WITH SERVICEABLE UNIT. GROUND RUN AND FL - [SDR 20000417SH002](https://openairdocs.org/sdr/20000417SH002), Mar 17, 2000: BEARING. CRACKED. DURING REMOVAL OF BOTH LEFT AND RIGHT LANDING GEAR FORWARD TRUNNION BEARINGS, FOUND THE OUTER HOUSING WAS CRACKED COMPLETELY THROUGH. OLD BEARINGS WERE BEING RE - [SDR 20000330SH015](https://openairdocs.org/sdr/20000330SH015), Jan 17, 2000: CARBON SEAL. FAILED. ENGINE EXPERIENCED IN-FLIGHT SHUTDOWN 230.5 HRS FOLLOWING CZI (COMPRESSOR ZONE INSP) AND INSTALL OF NEW STYLE CARBON SEALS PER SB 72-3596 REV 7. ENG TEARDOWN RE - [SDR 97ZZZX1131](https://openairdocs.org/sdr/97ZZZX1131), Feb 1, 1997: CONNECTOR. CORRODED. INTERMITTENT CONNECTION OF PLUG CAUSES INTERMITTENT AVAILABILITY OF VARIABLE AUTHORITY OF NOSE WHEEL STEERING. THE PLUG IS TOO SUSCEPTIBLE TO MOISTURE AND CORRO - [SDR 96ZZZX5830](https://openairdocs.org/sdr/96ZZZX5830), Nov 8, 1996: VALVE. LOOSE CONNECTOR. EMERGENCY PRESSURIZATION KICKED ON AT 14,500. TIGHTENED AND RE-SAFTIED CONNECTOR ON RT EMERGENCY BLEED VALVE. GROUND AND TEST FLIGHT CHECK NORMAL. - [SDR 96ZZZX4391](https://openairdocs.org/sdr/96ZZZX4391), Jul 22, 1996: GENERATOR. FAILED. THE AIRCRAFT EXPERIENCED VIBRATIONS AND AMP FLUCTUATIONS. THE PROBLEM WAS ISOLATED TO THE RIGHT GENERATOR. GENERATOR REMOVAL REVEALED BEARING FAILURE. THIS WAS - [SDR 96ZZZX3044](https://openairdocs.org/sdr/96ZZZX3044), Jun 6, 1996: MOUNT BEAM. CHAFE. MOUNT BEAM CHAFING ON PYLON SIDE PANEL MOUNT FEED-THROUGH DOUBLER RING UPPER 3 ATTACH RIVETS. SUSPECT PYLON SIDE PANEL MOVEMENT. SUBMITTER STATES TO REMOVE OLD - [SDR 96ZZZX3043](https://openairdocs.org/sdr/96ZZZX3043), Jun 6, 1996: MOUNT BEAM. CHAFE. MOUNT BEAM CHAFING ON PYLON SIDE PANEL MOUNT FEED THROUGH DOUBLER RING UPPER 3 ATTACH RIVETS. SUSPECT CAUSE: PYLON SIDE PANEL MOVEMENT. SUBMITTER STATES TO REMO - [SDR 96ZZZX332](https://openairdocs.org/sdr/96ZZZX332), Nov 21, 1995: B-NUT. LOOSE. BTV/PWA - FLT 1121 - CHARTER FLIGHT FAR 135. AIRCRAFT DEVELOPED A TOTAL LOSS OF HYDRAULIC PRESSURE AND FLUID QUANTITY. AIRCRAFT DIVERTED TO FWA AND PRIORITY HAN - [SDR 95ZZZX5972](https://openairdocs.org/sdr/95ZZZX5972), Sep 25, 1995: FLOOR SKIN. DELAMINATING. WHILE PRESSURIZING AIRCRAFT FOR 1,200 HOUR INSPECTION, AIRCRAFT WOULD NOT MAKE ALLOWABLE LEAK RATE. FOUND LOWER SKIN OF DIVAN SEAT FLOOR SITTING ON TOP OF WING - [SDR 95ZZZX971](https://openairdocs.org/sdr/95ZZZX971), Jan 19, 1995: CENTERING CAM. CORRODED. DURING NLG STRUT RESEALING, THE LOWER CENTERING CAM WAS FOUND UNSERVICEABLE DUE TO CORROSION. FIFTY PERCENT OF THE FLANGE SEPARATING THE FELT WIPER AND THE SCRA ## STCs that may be installed (OpenAirDocs) (183, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc - [STC ST12087CH](https://openairdocs.org/stc/ST12087CH): Installation replacement Cabin/Cockpit Handheld Fire Extinguishers. Avcon Industries Inc - [STC ST02416SE](https://openairdocs.org/stc/ST02416SE): Installation of the replacement rate gyro, Butler National Part Number 501-1169-01 MOD A or 501-1169-02 MOD A. Symetric Industries, DBA Extant Aerospace - [STC ST02417SE](https://openairdocs.org/stc/ST02417SE): Installation of the replacement stall warning vertical accelerometer, Butler National Part Number 02904001-101. Symetric Industries, DBA Extant Aerospace - [STC ST02515SE](https://openairdocs.org/stc/ST02515SE): Installation of the replacement vertical accelerometer, Butler National Part Number 501-1287-02 MOD A. Symetric Industries, DBA Extant Aerospace - [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc - [STC ST00738WI](https://openairdocs.org/stc/ST00738WI): Increased service life. Data required. Phoenix Air Group Inc - [STC ST02036WI](https://openairdocs.org/stc/ST02036WI): Installation of an additional Garmin G700 TXi Primary Flight Display or Multifunction Display. Butler National Corporation - [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC - [STC ST01138DE](https://openairdocs.org/stc/ST01138DE): Installation of MidContinent MD23 standby altimeter and/or attitude indicators. Butler National Corporation - [STC ST01083DE](https://openairdocs.org/stc/ST01083DE): Installation of the Aviation Clean Air Airborne Air & Surface Purification System. Lee Aerospace, Inc - [STC ST04728NY](https://openairdocs.org/stc/ST04728NY): Installation of LAI CoolView Cabin Window. Lee Aerospace Inc - [STC SA709NE](https://openairdocs.org/stc/SA709NE): Installation of Marquardt MTR-101 Tow Reel System. Phoenix Air Group Inc - [STC ST00814WI](https://openairdocs.org/stc/ST00814WI): Landing Gear Life Extension. Phoenix Air Group Inc - [STC ST00999WI](https://openairdocs.org/stc/ST00999WI): Installation of Special Mission Power and Control Wiring, provisions for Carriage of Mission Stores with Hardpoints installed by STC SA1604SO or SA1670CE, and Takeoff weight increased to 16,300 lbs. Phoenix Air Group Inc - [STC ST10217SC](https://openairdocs.org/stc/ST10217SC): Approval of underwing stores including carriage of the MTR101 Tow Reel System (and targets) on the Strongback-Lear (Sentel) hardpoint. Phoenix Air Group Inc - [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC - [STC ST01517WI](https://openairdocs.org/stc/ST01517WI): Installation of the Glareshield LED Lighting System. Global Aviation Tech LLC - [STC ST01602WI](https://openairdocs.org/stc/ST01602WI): Installation of Luminescent Overlay panels upgrade. Global Aviation Tech LLC - [STC ST04393CH](https://openairdocs.org/stc/ST04393CH): Avionics upgrade installation of a Garmin GTN (TM) 750 Touchscreen Navigator interfaced to existing pilot side instruments and existing FC-200 or FC-530/-550 Autopilot and added GWX (TM) 70 Weather Radar. The Garmin GTN (TM) 750 GPS is paired with the added GTX (TM) 345R (or GTX 33/33D) Transponders for Automatic Broadcast Surveillance (ADS-B) OUT and ADS-B IN (GDL-88) capability with wireless download connectivity utilizing Garmin Connext®. Optional second Garmin GTN (TM) 650/750 interfaced to existing copilot side instruments only. Royal Air Inc - [STC ST01070DE](https://openairdocs.org/stc/ST01070DE): Installation of the Curtiss-Wright Fortress Flight Data Recorder (with Cockpit Voice Recorder). Peregrine - [STC ST01682WI](https://openairdocs.org/stc/ST01682WI): Installation of Heads Up Technologies (HUT) Cabin Entertainment System (CES). Heads Up Technologies Inc - [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited - [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine - [STC ST02635AT](https://openairdocs.org/stc/ST02635AT): Deactivation of Aeronca (Learjet) Thrust Reversers. Summit Aviation Inc - [STC ST01881WI](https://openairdocs.org/stc/ST01881WI): Installation of the Garmin GTS 8000 TCAS II System and Dual GTX 3000 Transponders for ADS-B Out Compliance and Interface of factory installed FC-530 Autopilot System to Single/Dual GTN 7XX/6XX Navigators. Avcon Industries Inc - [STC ST02230SE](https://openairdocs.org/stc/ST02230SE): The installation of dual Garmin GTX-33ES Mode-S transponders and single or dual Garmin GTN 650/750 panel mounted navigation and global positioning system (GPS) units, or dual Garmin GTX-335R and/or GTX-345R Mode-S transponders and single or dual Garmin GTN 650/750/625/725 panel mounted navigation and GPS units. Butler National Corporation - [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC - [STC ST01102WI](https://openairdocs.org/stc/ST01102WI): Installation of a Universal Avionics MFD-640 Multi-Function Display. Blackhawk Aerospace Technologies Inc - [STC ST01103WI](https://openairdocs.org/stc/ST01103WI): Installation of a Universal Avionics (TAWS) Terrain Awareness and Avoidance System. Blackhawk Aerospace Technologies Inc - [STC ST04481CH](https://openairdocs.org/stc/ST04481CH): Replacement of similar functioning circuit and switch for obsolete steering interface unit (SIU) in accordance with Butler National Master Data List 0200 I 020 Revisio n (A) , dat ed 14 MAY 2021, or later FAA Approved Revision. Butler National Corporation - [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc - [STC ST01926WI](https://openairdocs.org/stc/ST01926WI): Interface of factory installed FC-530/FC-535 Autopilot System to Single/Dual GTN 750/650 Navigators. Avcon Industries Inc - [STC ST04478NY](https://openairdocs.org/stc/ST04478NY): Installation of a Honeywell CAS-66A TCAS I and MFRD (Multi-Function Radar Display). Executive Air Craft Ltd - [STC ST04447CH](https://openairdocs.org/stc/ST04447CH): Installation of Garmin GTS (TM) 8000 TCAS/ACAS II Traffic Surveillance system, dual GTX (TM) 3000 Mode-S Extended Squitter Transponders and GDL® 88 receiver for a complete ADS-B In/Out capability and a Flight Stream 210 for wireless download connectivity using Garmin Connext®. Installation in accordance with Royal Air Master Document List No. RACB-MDL-3000, Revision A, dated January 06, 2020, or later FAA approved revision. Royal Air Inc - [STC ST04457NY](https://openairdocs.org/stc/ST04457NY): Installation of the Honeywell CAS 67A TCAS II / Dual MST 67A Mode S Transponder Upgrade. Executive Air Craft Ltd - [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC ST02681AT-D](https://openairdocs.org/stc/ST02681AT-D): Installation of Cockpit / Cabin Blower Assy. Summit Aviation Inc - [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc - [STC ST00882DE](https://openairdocs.org/stc/ST00882DE): Installation of Becker Avionics BXT6553 transponder. Peregrine - [STC ST02455SE](https://openairdocs.org/stc/ST02455SE): Installation of Dual GTX-3000 Transponders, GDL-88 Automatic Dependent Surveillance-Broadcast (ADS-B) (In) with Wide Area Augmentation System (WAAS) Global Positioning System (GPS) sensor and Flight Stream 210 Bluetooth Connectivity installed for ADS-B (Out) compliance. Butler National Corporation - [STC ST09366SC](https://openairdocs.org/stc/ST09366SC): Installation of an Electric-Driven Vapor Cycle air conditioning system. Air Comm Corporation - [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS - [STC ST00835DE](https://openairdocs.org/stc/ST00835DE): Installation of Automatic Dependent Surveillance - Broadcast (ADS-B) Out and In functionality using the Garmin GTX 335R and GTX 345R Transponders plus qualified position sensor. Peregrine - [STC SA4836SW](https://openairdocs.org/stc/SA4836SW): Installation of TR4000 thrust reversers. The NORDAM Group LLC - [STC SA4999NM](https://openairdocs.org/stc/SA4999NM): Installation of lifeport patient loading and support system. LifePort LLC - [STC ST00790DE](https://openairdocs.org/stc/ST00790DE): Installation of BendixKing CAS 67B Traffic Alert and Collision Avoidance System (TCAS) II Version 7.1. Peregrine All 183: https://openairdocs.org/model/gates-lear-jet-36a/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.