# Agusta AW119MKII - Type: Aircraft model (FAA registry) - Registry code: 0260130 - Manufacturer (registry): AGUSTA SPA - Model: AW119MKII - Aircraft type: Rotorcraft - Category: Rotorcraft - Engines: 1 · Turbo-shaft - Seats: 8 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS H7EU](https://openairdocs.org/tcds/H7EU) (OpenAirDocs) - Holder: Leonardo S.p.A. - Registered aircraft: 1 - Page: https://openairdocs.org/model/agusta-aw119mkii 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 2026-17-07](https://openairdocs.org/ad/2026-17-07): Main rotor mast/swashplate · Leonardo A109A, A109A II, A109C and 6 more. Effective Oct 2, 2026 - [AD 2025-25-13](https://openairdocs.org/ad/2025-25-13): Powerplant System · Leonardo AW119 MKII and A119. Effective Jan 13, 2026 - [AD 2025-18-01](https://openairdocs.org/ad/2025-18-01): Main Rotor Head · Leonardo A109E, A109S, AW109SP and 2 more. Effective Sep 25, 2025 - [AD 2025-17-10](https://openairdocs.org/ad/2025-17-10): Main Rotor Control · Leonardo A109A, A109A II, A109C and 3 more. Effective Sep 9, 2025 - [AD 2025-09-06](https://openairdocs.org/ad/2025-09-06): Battery/charger system · Leonardo A119 and AW119 MKII. Effective Jun 16, 2025 - [AD 2024-18-01](https://openairdocs.org/ad/2024-18-01): Rotorcraft Flight Control · Leonardo A119 and AW119 MKII. Effective Nov 12, 2024 - [AD 2023-25-08](https://openairdocs.org/ad/2023-25-08): Main Rotor System · Leonardo A109E, A109S, AW109SP and 2 more. Effective Feb 2, 2024 - [AD 2023-17-07](https://openairdocs.org/ad/2023-17-07): Starter-Generator · Leonardo A119 and AW119 MKII. Effective Nov 1, 2023 - [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023 - [AD 2021-21-03](https://openairdocs.org/ad/2021-21-03): Rotorcraft Flight Control, Rotorcraft Servo System · Leonardo A109A, A109A II, A109C and 6 more. Effective Dec 10, 2021 - [AD 2021-20-18](https://openairdocs.org/ad/2021-20-18): Passenger compartment doors · Leonardo AW119 MKII. Effective Nov 3, 2021 - [AD 2021-16-06](https://openairdocs.org/ad/2021-16-06): Tail Rotor Drive Shaft · Leonardo A119 and AW119 MKII. Effective Sep 27, 2021 - [AD 2021-14-14](https://openairdocs.org/ad/2021-14-14): Instrument System Wiring · Leonardo AW119 MKII. Effective Jul 26, 2021 - [AD 2021-03-15](https://openairdocs.org/ad/2021-03-15): Tail Rotor System · Leonardo A119 and AW119 MKII. Effective Apr 1, 2021 - [AD 2020-26-10](https://openairdocs.org/ad/2020-26-10): Placards and markings · Leonardo A119 and AW119 MKII. Effective Feb 1, 2021 - [AD 2020-21-21](https://openairdocs.org/ad/2020-21-21): Main Rotor Head · Leonardo A109E, A109S, A119 and 2 more. Effective Nov 24, 2020 - [AD 2020-15-16](https://openairdocs.org/ad/2020-15-16): Tail Rotor Drive System · Leonardo A109E, A109K2, A109S and 3 more. Effective Aug 27, 2020 - [AD 2018-06-51](https://openairdocs.org/ad/2018-06-51): Main Rotor Mast/Swashplate · Agusta A109A, A109A II, A109C and 6 more. Effective Jun 7, 2018 - [AD 2018-07-02](https://openairdocs.org/ad/2018-07-02): Main Rotor Blades · Agusta A109E, A109S, A119 and 2 more. Effective Apr 13, 2018 - [AD 2015-05-52](https://openairdocs.org/ad/2015-05-52): Tail Rotor Controls · Agusta A109, A109A, A109A II and 7 more. Effective Apr 29, 2015 - [AD 2015-05-05](https://openairdocs.org/ad/2015-05-05): Main Rotor System · Agusta A109S, A119, AW109SP and 1 more. Effective Apr 23, 2015 - [AD 2014-23-02](https://openairdocs.org/ad/2014-23-02): Main Rotor Gearbox · Agusta A109E, A109K2, A119 and 1 more. Effective Dec 26, 2014 - [AD 2014-11-07](https://openairdocs.org/ad/2014-11-07): Main Rotor System · Agusta A109A, A109A II, A109C and 6 more. Effective Jun 18, 2014 - [AD 2013-20-51](https://openairdocs.org/ad/2013-20-51): Tail rotor system · Agusta A109A, A109A II, A109C and 6 more. Effective Oct 25, 2013 - [AD 2013-19-01](https://openairdocs.org/ad/2013-19-01): Flight Compartment Windows · Agusta A119 and AW119 MKII. Effective Oct 25, 2013 - [AD 2013-09-06](https://openairdocs.org/ad/2013-09-06): Rotors Flight Control · Agusta A119 and AW119 MKII. Effective Jun 20, 2013 - [AD 2010-12-51](https://openairdocs.org/ad/2010-12-51): Tail Rotor Gearbox · Agusta A119 and AW119 MKII. Effective Sep 17, 2010 - [AD 2009-12-07](https://openairdocs.org/ad/2009-12-07): Cargo hook lever · Agusta A109E, A109S, A119 and 1 more. Effective Jul 17, 2009 Historical (superseded or no longer in force): - [AD 2021-22-05](https://openairdocs.org/ad/2021-22-05) (historical): Rotorcraft Flight Control · Leonardo A119 and AW119 MKII. Effective Jan 3, 2022 - [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021 - [AD 2020-19-11](https://openairdocs.org/ad/2020-19-11) (historical): Tail Rotor Gearbox · Leonardo A119 and AW119 MKII. Effective Oct 27, 2020 - [AD 2020-13-02](https://openairdocs.org/ad/2020-13-02) (historical): Tail Rotor System · Leonardo A119 and AW119 MKII. Effective Jul 8, 2020 - [AD 2018-07-08](https://openairdocs.org/ad/2018-07-08) (historical): Tail Rotor Drive System · Agusta A109E, A109K2, A109S and 3 more. Effective Apr 26, 2018 - [AD 2014-04-14](https://openairdocs.org/ad/2014-04-14) (historical): Main Rotor System · Agusta A109S, A119, AW109SP and 1 more. Effective Apr 7, 2014 - [AD 2010-15-51](https://openairdocs.org/ad/2010-15-51) (historical): Rotors Flight Control · Agusta A119 and AW119 MKII. Effective Sep 2, 2010 ## Information bulletins (advisory) (2) - [SAIB SW-18-13](https://openairdocs.org/saib/SW-18-13): Main Transmission Plate Fitting. Issued Apr 30, 2018 - [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System. Issued Oct 3, 2012 ## Registered aircraft (1) - [N330JN](https://openairdocs.org/aircraft/N330JN): [Bristow LLC](https://openairdocs.org/faa-owner/BRISTOW%20LLC), [Lake Charles, LA](https://openairdocs.org/faa-place/LA/Lake%20Charles), built 2006, S/N 14510 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (71, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2NSA100326727029](https://openairdocs.org/sdr/2NSA100326727029), Oct 3, 2026: BYPASS VALVE. FAILED. PILOT EXPERIENCED RISE IN ENGINE OIL TEMPERATURE DURING STRAIGHT AND LEVEL FLIGHT. PILOT COULD NOT RECTIFY THROUGH INITIAL EMERGENCY PROCEDURES AND INITIATED A - [SDR 37CA2026070900144](https://openairdocs.org/sdr/37CA2026070900144), Jul 9, 2026: SKID. CORRODED. CORROSION WAS IDENTIFIED IN THE SKID TUBE BUSHING AREA WHERE SKID SHOE THROUGH BOLTS ATTACH. - [SDR 37CA202607090143](https://openairdocs.org/sdr/37CA202607090143), Jul 9, 2026: SKID. CORRODED. CORROSION WAS IDENTIFIED IN THE SKID TUBE BUSHING AREA WHERE SKID SHOE THROUGH BOLTS ATTACH. - [SDR U0GA20260000431](https://openairdocs.org/sdr/U0GA20260000431), May 26, 2026: RADIO. SHORTED. PILOT REPORT - WAS FLYING ALONG STRAIGHT AND LEVEL AND SUDDENLY SMELLED A PLASTICKY ELECTRIC SMELL. STARTED TO TROUBLE SHOOT CIRCUIT BREAKERS AND INSTRUMENT PAN - [SDR 2026FA0000340](https://openairdocs.org/sdr/2026FA0000340), May 3, 2026: BYPASS VALVE. FAILED. PILOT EXPERIENCED A RISE IN TEMPERATURE DURING FLIGHT, UP TO 114 CELCIUS. PILOT REDUCE POWER AND AIRSPEED TO UNLOAD ENGINE TO AID IN COOLING. ENGINE OIL TEMP RE - [SDR 37CA2026022407233](https://openairdocs.org/sdr/37CA2026022407233), Feb 24, 2026: SLIDING WINDOW. DEBONDED. LEFT CABIN DOOR SLIDING WINDOW DE BONDED. FOUND DURING PRE-FLIGHT AIRWORTHINESS CHECK. - [SDR 37CA202602230001](https://openairdocs.org/sdr/37CA202602230001), Feb 21, 2026: GUIDE. DEPARTED. AFTER DEPARTING ASHLAND HOSPITAL IN SUPERIOR WI, THE R/H CABIN WINDOW SLIDER DEPARTED THE AIRCRAFT. - [SDR 2026FA0000012](https://openairdocs.org/sdr/2026FA0000012), Jan 9, 2026: PITOT TUBE. DAMAGED. COMPONENTS ARE FAILING DUE TO OVERHEATING, CAUSING THE CONNECTOR’S SOLDER JOINTS TO MELT AND CAUSE THERMAL DAMAGE TO THE PITOT PROBE ELECTRICAL CONTACTS. 50 INS - [SDR 2025FA0000638](https://openairdocs.org/sdr/2025FA0000638), Sep 11, 2025: BUSHING. INCORRECT. MAIN ROTOR HEAD DAMPER BUSHING P/N 109-0111-32-10X WAS INSTALLED INCORRECTLY DURING AIRCRAFT PRODUCTION. AIRCRAFT VIBRATIONS ARE SUSPECTED AS A RESULT OF THE IN - [SDR 2025FA0000336](https://openairdocs.org/sdr/2025FA0000336), Apr 14, 2025: TERMINAL BLOCK. FAULTED. PILOT NOTED THE SMELL OF OZONE OR ELECTRICAL CIRCUIT GETTING HOT WHILE DEPARTING NK-71. NO SMOKE OR SYSTEM FAILURE WAS INDICATED. AS HE WAS STILL NEAR BASE OF O - [SDR 37CA2025/02/2601](https://openairdocs.org/sdr/37CA2025%2F02%2F2601), Feb 20, 2025: TACH GENERATOR. DEFECTIVE. N1 TACHOMETER GENERATOR ERRATIC READINGS DURING START UP CAUSING A MIS-COMPARE P CAUTION MESSAGE. - [SDR 2025F00040](https://openairdocs.org/sdr/2025F00040), Feb 12, 2025: BOLT. WORN. THE UPPER PC LINK BOLT ON ONE MRB BLADE WAS FOUND TO HAVE RED IRON STAINING ON MRH BLADE PITCH CHANGE HORN. PLAY NOT EASILY NOTICED UNLESS THE MRB WAS REPOSITIO - [SDR 2023FA0000684](https://openairdocs.org/sdr/2023FA0000684), Oct 26, 2023: HOSE. FATIGUED. CORRUGATED FUEL LINE WAS FOUND CRACKED DURING A SYSTEM DISTRIBUTION CHECK. US NAVY INVESTIGATION FOUND TUBE FAILED IN FATIGUE ORIGINATING ON BOTH THE INNER AND - [SDR 2023FA0000282](https://openairdocs.org/sdr/2023FA0000282), May 30, 2023: PIN. MALFUNCTIONED. DURING AN AVIONIC TEST FLIGHT THE TAIL ROTOR PEDAL LOCKOUT EXPANDABLE PIN FELL APART FROM THE PIN HANDLE. THERE ARE NO INSTRUCTION TO IDENTIFY THIS ISSUE IN THE - [SDR 2022F00381](https://openairdocs.org/sdr/2022F00381), Sep 29, 2022: MAGNETOMETER. FAILED. AIRCRAFT HAS BURNT ELECTRICAL SMELL THROUGHOUT COCKPIT AND CABIN. AIRCRAFT WAS AT 3500 FT MSL STARTED DECENT, SMELL GOT STRONGER. DECIDED TO LAND IN FIELD, ON T - [SDR 8LFA2022FA0000454](https://openairdocs.org/sdr/8LFA2022FA0000454), Aug 18, 2022: SADDLE. CRACKED. FOUND LANDING GEAR SADDLE CRACKED - [SDR 37CA202106300001](https://openairdocs.org/sdr/37CA202106300001), Jun 29, 2021: O-RING. LEAKING. CREW REPORTED FUEL SMELL IN THE CABIN, FOUND SEEPING O-RING AT AUX TANK BLANKING PLATE. - [SDR QMLA2021040920016](https://openairdocs.org/sdr/QMLA2021040920016), Mar 12, 2021: TAIL BOOM. CRACKED. A 3.8 INCH CRACK WAS FOUND ON THE TAIL BOOM NEAR THE LOWER FIN MOUNTING AREA. UPON FURTHER INSPECTION, DELAMINATION OF THE TAILBOOM SKIN (AROUND THE CRACK) WAS - [SDR 2021FA0000048](https://openairdocs.org/sdr/2021FA0000048), Feb 13, 2021: BLADE. DAMAGED. MAIN ROTOR BLADE DAMAGE. DURING CLIMB EXPERIENCED LOUD THUD PERFORMED PER-CAUTIONARY TO BASE LANDING FOUND HOLE THROUGH BLUE MAIN ROTOR BLADE AND LEADING EDGE D - [SDR 8LFA20200423001](https://openairdocs.org/sdr/8LFA20200423001), Apr 23, 2020: HOUSING. CRACKED. DURING INSPECTION, LAG DAMPER UPPER INBOARD ATTACHMENT HOUSING FOUND CRACKED ALL THE WAY THROUGH. - [SDR QMLA2020020762007](https://openairdocs.org/sdr/QMLA2020020762007), Feb 6, 2020: TRANSMISSION. MAKING METAL. 14934 HAD TRANSMSION CHIPS ON DETECTOR LOWER, PERFORMED OIL AND FILTER CHANGE. GROUND RUN AIRCRAFT AND NO CHIPS, FLEW AIRCAFT AND CHIP LIGHT ILLUMINATED, INSPEC - [SDR 8LFA2020012714001](https://openairdocs.org/sdr/8LFA2020012714001), Jan 14, 2020: TRANSMISSION. MAKING METAL. MAIN GEAR BOX TRANSMISSION LIGHT IN FLIGHT. GEAR BOX REQUIRED REPLACEMENT DUE TO CHIP MATERIAL. THIS IS THE THIRD CHIP EVENT ON THE MGB, TWO PREVIOUS INSTANCES - [SDR QMLA2019042271939](https://openairdocs.org/sdr/QMLA2019042271939), Apr 17, 2019: PRESSURE SWITCH. FAILED. SHORTLY AFTER DEPARTURE PILOT RECEIVED "XMSN OIL PRESSURE" WARNING LIGHT ALONG WITH AN INCREASE IN INDICATED PRESSURE. PERFORMED PRECAUTIONARY LANDING AND MAINT - [SDR QMLA2019010719003](https://openairdocs.org/sdr/QMLA2019010719003), Jan 7, 2019: FITTING. CRACKED. FOUND 25.4 MM CRACK IN LT TRANSMISSION FITTING P/N 109-0330-17-105 DURING EDDY CURRENT INSPECTION. - [SDR 8LFA20190104001](https://openairdocs.org/sdr/8LFA20190104001), Jan 4, 2019: FITTING. CRACKED. DURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT HAND PLATE FITTING CRACKED. - [SDR QMLA2018102918116](https://openairdocs.org/sdr/QMLA2018102918116), Oct 29, 2018: SUPPORT ANGLE. CRACKED. UPPER GREENHOUSE WINDOW FRAME ON THE RIGHT HAND SIDE HAS A CRACK IN THE SUPPORT ANGLE RADIUS WL 1500 BL480.0. THIS IS A COMMON FLAW AND THE MANUFACTURER HAS PRO - [SDR 8LFA20180820001](https://openairdocs.org/sdr/8LFA20180820001), Aug 20, 2018: FITTING. CRACKED. DURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT PLATE FITTING CRACKED. - [SDR 8LFA20180619001](https://openairdocs.org/sdr/8LFA20180619001), Jun 19, 2018: SWASHPLATE. CRACKED. DURING 2400 HOUR INSPECTION, NDT (FLUORESCENT PENETRATION) PERFORMED ON SWASH-PLATE FIXED ASSEMBLY WHERE INDICATIONS OF CRACKS WERE PRESENT IN THE RECESS WHERE - [SDR QMLA2018061418071](https://openairdocs.org/sdr/QMLA2018061418071), Jun 14, 2018: DAMPER. CRACKED. DURING INSPECTION, FOUND THE MAIN ROTOR DAMPER ON THE YELLOW BLADE WAS CRACKED ALONG INBOARD MOUNTING FLANGE, COMPLETELY THROUGH THE UPPER FORK AND STARTING ON - [SDR 8LFA2018051608001](https://openairdocs.org/sdr/8LFA2018051608001), May 8, 2018: FITTING. CRACKED. DURING INSPECTION FOUND MAIN TRANSMISSION LEFT PLATE FITTING CRACKED. - [SDR 2018FA0000130](https://openairdocs.org/sdr/2018FA0000130), Apr 3, 2018: FITTING. CRACKED. CRACKED MGB SUPPORT FITTING. COUNTER TORQUE CROSSBEAM FITTING PLATE WAS FOUND CRACKED. - [SDR 2018FA0000129](https://openairdocs.org/sdr/2018FA0000129), Apr 3, 2018: SUPPORT FITTING. CRACKED. CRACKED MGB SUPPORT FITTING. WHILE COMPLETING LEONARDO SB 119-087 LEFT HAND COUNTER TORQUE CROSSBEAM FITTING PLATE WAS FOUND CRACKED. - [SDR EIBA2018040300123](https://openairdocs.org/sdr/EIBA2018040300123), Apr 3, 2018: BRACKET. FAILED. PILOT CONDUCTING A POST FLIGHT WALK-AROUND FOUND THE FLUX COMPENSATOR HANGING UNDERNEATH THE AFT CENTER PORTION OF THE TAILBOOM. FLUX VALVE MOUNT BRACKET RING H - [SDR 8LFA201803200001](https://openairdocs.org/sdr/8LFA201803200001), Mar 18, 2018: FITTING. CRACKED. DURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT HAND PLATE FITTING CRACKED. - [SDR 2018F00124](https://openairdocs.org/sdr/2018F00124), Mar 6, 2018: MOUNT FITTING. CRACKED. CRACKED MGB SUPPORT FITTING. WHILE COMPLETING SB 119-087, LEFT COUNTER TORQUE CROSSBEAM FITTING PLATE WAS FOUND CRACKED. - [SDR QMLA2018021218018](https://openairdocs.org/sdr/QMLA2018021218018), Feb 12, 2018: SKIN. DAMAGED. RIGHT FORWARD SLIDING DOOR SKIN WRINKLED DUE TO EXCESSIVE FORCE USED TO CLOSE THE DOOR. - [SDR 8LFA201800320001](https://openairdocs.org/sdr/8LFA201800320001), Jan 26, 2018: FITTING. CRACKED. DURING INSPECTION, FOUND MAIN TRANSMISSION AFT RIGHT PLATE FITTING CRACKED. - [SDR QMLA2018012318005](https://openairdocs.org/sdr/QMLA2018012318005), Jan 23, 2018: FITTING. CRACKED. FOUND CRACKED RT TRANSMISSION FITTING P/N 109-0330-17-106 DURING 800 HOUR INSPECTION. - [SDR 8LFA20171218001](https://openairdocs.org/sdr/8LFA20171218001), Dec 18, 2017: FITTING. CRACKED. DURING INSPECTION, FOUND MAIN TRANSMISSION AFT RIGHT PLATE FITTING CRACKED. - [SDR QMLA2017110117123](https://openairdocs.org/sdr/QMLA2017110117123), Nov 1, 2017: MOUNT. CRACKED. DURING MAIN ROTOR TRANSMISSION CHANGE, FOUND THE LT AND RT AIRFRAME TRANSMISSION DECK FITTINGS CRACKED. - [SDR 8LFA20171025001](https://openairdocs.org/sdr/8LFA20171025001), Oct 25, 2017: GEARBOX. FAILED. DURING A MAINTENANCE FLIGHT, MAIN GEAR BOX CHIP ILLUMINATED. AIRCRAFT RETURNED TO ORIGINAL DEPARTURE WITHOUT FURTHER INCIDENT. MAIN GEARBOX HAD .2 HOURS SINCE R - [SDR 8LFA20171011001](https://openairdocs.org/sdr/8LFA20171011001), Oct 11, 2017: FITTING. CRACKED. DURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT PLATE FITTING CRACKED. - [SDR 8LFA20170907001](https://openairdocs.org/sdr/8LFA20170907001), Sep 7, 2017: FITTING. CRACKED. DURING INSPECTION, FOUND MAIN TRANSMISSION AFT RIGHT PLATE FITTING CRACKED. - [SDR 8LFA20170901001](https://openairdocs.org/sdr/8LFA20170901001), Sep 1, 2017: FITTING. CRACKED. DURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT PLATE FITTING CRACKED - [SDR 8LFA20170815003](https://openairdocs.org/sdr/8LFA20170815003), Aug 11, 2017: FITTING. CRACKED. DURING INSPECTION, FOUND THE MAIN TRANSMISSION AFT RIGHT PLATE FITTING CRACKED. - [SDR 8LFA20170815002](https://openairdocs.org/sdr/8LFA20170815002), Aug 2, 2017: FITTING. CRACKED. DURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT PLATE FITTING CRACKED. - [SDR 8LFA08152017001](https://openairdocs.org/sdr/8LFA08152017001), Jul 21, 2017: FITTING. CRACKED. DURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT PLATE FITTING CRACKED. - [SDR 2017F00127](https://openairdocs.org/sdr/2017F00127), Jul 20, 2017: FUEL CONTROL. SURGES. ENGINE TORQUE AND N1 FROM 3-5% DURING APPROACH IN A HOVER AND AFTER TOUCH DOWN. - [SDR 8LFA20170815001](https://openairdocs.org/sdr/8LFA20170815001), Jul 19, 2017: FITTING. CRACKED. DURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT PLATE FITTING CRACKED. - [SDR 8LFA20170712001](https://openairdocs.org/sdr/8LFA20170712001), Jul 12, 2017: FITTING. CRACKED. DURING INSPECTION FOUND MAIN TRANSMISSION AFT RIGHT PLATE FITTING CRACKED. All 71: https://openairdocs.org/model/agusta-aw119mkii/reports.md ## STCs that may be installed (OpenAirDocs) (58, 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 SR12441MC](https://openairdocs.org/stc/SR12441MC): Installation of exterior NVIS compatible formation lights. Leonardo Helicopters US Corporation - [STC SR02520AK](https://openairdocs.org/stc/SR02520AK): Installation of Avionics and auxiliary generator (Configurations A1, A2, A3, E1, D1, X) for certification of Single Pilot Instrument Flight Rules (SPIFR) Operations. Leonardo Helicopters US Corporation - [STC SR03280NY](https://openairdocs.org/stc/SR03280NY): Installation of a Garmin G1000H PFD/MFD Display System. Leonardo Helicopters US Corporation - [STC SR04231NY](https://openairdocs.org/stc/SR04231NY): Installation of the Utility Installations, ID No. AWPC-ENG-17-037-A1 through AWPC-ENG-17-037-A27. Leonardo Helicopters US Corporation - [STC SR04601NY](https://openairdocs.org/stc/SR04601NY): Installation of a crash resistant fuel system (CRFS) and optional closed circuit refueling receiver (CCRR). Leonardo Helicopters US Corporation - [STC SR04464NY](https://openairdocs.org/stc/SR04464NY): Installation of the iPad Mount. Avio Design Group Inc - [STC SR04842NY](https://openairdocs.org/stc/SR04842NY): Installation of RMCI Inc. Expandable Rotorcraft Diagnostic System (XRDS). Sterling Helicopter - [STC SR00824DE](https://openairdocs.org/stc/SR00824DE): Installation of an Emergency Medical Services Interior and alternate cabin seating interior configurations. AMS Heli Design - [STC SR03201CH](https://openairdocs.org/stc/SR03201CH): Installation of Heli-Preheat System, P/N 2862-1 for 115 volt application. Hartzell Propeller LLC - [STC SR04838NY](https://openairdocs.org/stc/SR04838NY): Installation of optional recording system under Configuration A1, which consists of L3Harris Modular Airborne Data recording/Acquisition Systems (MADRAS) Cockpit Voice and Data Recorder (CVDR) system. AgustaWestland Philadelphia Corporation (AWPC) - [STC SR02454LA](https://openairdocs.org/stc/SR02454LA): Installation of Essex Cryogenics LOX System. M7 Aerospace LLC - [STC SR04557AT](https://openairdocs.org/stc/SR04557AT): Cabin and crew floor protector installations. Helifab East LLC - [STC SR01392LA](https://openairdocs.org/stc/SR01392LA): Installation of Apical Industries, Inc. Emergency Float Kits. Dart Aerospace ULC - [STC SR00463DE](https://openairdocs.org/stc/SR00463DE): Installation of Cabin Air Conditioning System. Air Comm Corporation - [STC SR04007AT](https://openairdocs.org/stc/SR04007AT): Replace original equipment Nickel-Cadmium (NiCd) or Concorde Lead-Acid main battery with higher capacity Concorde Lead-Acid, main battery on Agusta A119 and AW119 MKII rotorcraft and associated hardware. Concorde Battery Corporation - [STC SR04601 NY](https://openairdocs.org/stc/SR04601%20NY): Installation of a crash resistant fuel system (CRFS). AgustaWestland Philadelphia Corporation - [STC SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC - [STC SR01476SE](https://openairdocs.org/stc/SR01476SE): Installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc - [STC SR00949SE](https://openairdocs.org/stc/SR00949SE): Fabrication of Dart D119-647-011 Bearpaws. Dart Aerospace USA Inc - [STC SR04453CH](https://openairdocs.org/stc/SR04453CH): Installation of Appareo Systems LLC Stratus ES & Stratus ESG ADS-B transponder. Appareo Systems LLC - [STC SR02124SE](https://openairdocs.org/stc/SR02124SE): Installation functionality. of Data Garmin Required: transponders: (1) Garmin GTX Master 345/345R Drawing with List ADS-B (MDL), Out and In 005-00734-A4, functionality;. Garmin International Inc - [STC SR04441NY](https://openairdocs.org/stc/SR04441NY): Installation of Night Vision Goggle (NVG) Compatible Lighting System, Configuration A. AgustaWestland Philadelphia Corporation - [STC SR04390CH](https://openairdocs.org/stc/SR04390CH): Installation of an Electronic Flight Instrument System (EFIS) in accordance with StandardAero Master Data List 1036284, Revision (B), dated June 5, 2019 or later FAA approved revision. StandardAero Business Aviation Services LLC - [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SR00814DE](https://openairdocs.org/stc/SR00814DE): Installation of Garmin Helicopter Terrain Awareness and Warning System (HTAWS). Cert Works LLC - [STC SR02894CH](https://openairdocs.org/stc/SR02894CH): Install EMS ITS Deck with the Factory EMS Interior. Spectrum Aeromed LLC dba Spectrum Aeromed - [STC SR00948SE](https://openairdocs.org/stc/SR00948SE): Fabrication of Dart D119-675-011 and -012 Heli-Access-Steps. Dart Aerospace USA Inc - [STC SR01043SE](https://openairdocs.org/stc/SR01043SE): Fabrication of Dart D119-696-011/013 cargo mirrors and installation of system. Dart Aerospace USA Inc - [STC SR02024SE](https://openairdocs.org/stc/SR02024SE): Fabrication of DART D119-646 Replacement Skidtube Installation. Dart Aerospace USA Inc - [STC SR02258SE](https://openairdocs.org/stc/SR02258SE): Installation of a tail rotor pedal lockout kit. Dart Aerospace USA Inc - [STC SR04230NY](https://openairdocs.org/stc/SR04230NY): Installation of a TRAKKA A800 Searchlight. AgustaWestland Philadelphia Corporation - [STC SR02377AK](https://openairdocs.org/stc/SR02377AK): Installation of a fixed mounted Max-Viz Enhanced Vision System (EVS) Model 1500 to include a sensor Line Replaceable Unit (LRU) with conformal housing, power supply, Detached Electrical Box (DEB) and a glareshield-mounted, dedicated display monitor. Avio Design Group Inc - [STC SR00860DE](https://openairdocs.org/stc/SR00860DE): Installation of Teledyne Battery Products Valve-Regulated Lead-Acid. Teledyne Battery Products - [STC SR03055CH](https://openairdocs.org/stc/SR03055CH): Installation of Flight Data Monitoring System. MSP Aero LLC - [STC SR02789NY](https://openairdocs.org/stc/SR02789NY): Installation of a Border Guard Configuration. AgustaWestland Philadelphia Corporation - [STC SR00812DE](https://openairdocs.org/stc/SR00812DE): Installation of Honeywell Sky Connect Tracker III system. Cert Works LLC - [STC SR02487AK](https://openairdocs.org/stc/SR02487AK): Installation of L-3 Communications Avionics Systems ESI-500 Standby Instrument System. ADS-B Technologies, LLC - [STC SR01651NY](https://openairdocs.org/stc/SR01651NY): The installation of a Super Night Searchlight. AgustaWestland Philadelphia Corporation - [STC SR02428NY](https://openairdocs.org/stc/SR02428NY): The installation of High Visibility Crew Doors. AgustaWestland Philadelphia Corporation - [STC SR03504NY](https://openairdocs.org/stc/SR03504NY): Installation of Crosstube. Dart Aerospace Limited - [STC SR02394AK](https://openairdocs.org/stc/SR02394AK): Replacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting system. Seaplanes North LLC - [STC SR03478NY](https://openairdocs.org/stc/SR03478NY): Modification of EMS interior to allow primary litter to be installed diagonally across the cabin. AgustaWestland Philadelphia Corporation - [STC SR02425LA](https://openairdocs.org/stc/SR02425LA): Installation of Apical Industries, Inc. Cable Cutters Kit. Apical Industries, Inc. dba Dart Aerospace - [STC SH4676SW](https://openairdocs.org/stc/SH4676SW): Installation of Tail Rotor Floodlights on the upper surface of the horizontal stabilizer. DeVore Aviation Corporation of America, a New Mexico Corporation - [STC SR02265NY](https://openairdocs.org/stc/SR02265NY): Installation of Pedal Extensions. AgustaWestland Philadelphia Corporation - [STC SR02135NY](https://openairdocs.org/stc/SR02135NY): Helicopter configured with pilot and crew doors removed. AgustaWestland Philadelphia Corporation - [STC SR02239NY](https://openairdocs.org/stc/SR02239NY): The installation of a Spectrolab SX-16 Searchlight. AgustaWestland Philadelphia Corporation - [STC SR09360RC](https://openairdocs.org/stc/SR09360RC): Installation of Concorde Battery Model RG-407, Valve regulated sealed lead acid battery. Concorde Battery Corporation - [STC SR03027NY](https://openairdocs.org/stc/SR03027NY): Installation of an External ITT and Torque Indicating System. Aero-Dyne Repair Services Ltd - [STC SR02139SE](https://openairdocs.org/stc/SR02139SE): Fabrication of Onboard Systems Model 200-355-00 and 200-369-00 Cargo Hook Fixed Provision Kits, Model 200-356-00 Cargo Hook Suspension Kit, and Model 200-357-00 Load Weigh Kit, in accordance with FAA Approved Onboard Systems Master Drawing List No. 155-160-00, Revision 2, dated September 27, 2011, or later FAA approved revision. Installation of the Onboard Systems Model 200-355-00, 200-356-00, 200-357-00, or 200-369-00 kits in accordance with FAA approved Onboard Systems Owners Manual 120-141-00, Revision 0, dated April 25, 2011, or later FAA approved revision. This modification must be inspected and maintained in accordance with section ATA 5 of FAA approved Onboard Systems Instructions for Continued Airworthiness Document 123-036-00, Revision 0, dated May 5, 2011, or later FAA approved revision, and Onboard Systems Cargo Hook. Onboard Systems International All 58: https://openairdocs.org/model/agusta-aw119mkii/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Agustawestland Philadelphia AW119MKII](https://openairdocs.org/model/agustawestland-philadelphia-aw119mkii): 180 registered aircraft, registry code 0260401 - [Agusta Aerospace AW119 MKII](https://openairdocs.org/model/agusta-aerospace-aw119-mkii): 6 registered aircraft, registry code 0260105 - [Leonardo S P A AW119 MKII](https://openairdocs.org/model/leonardo-s-p-a-aw119-mkii): 1 registered aircraft, registry code 33601QH --- 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.