# Leonardo S P A AW119 MKII - Type: Aircraft model (FAA registry) - Registry code: 33601QH - Manufacturer (registry): LEONARDO S P A - Model: AW119 MKII - Aircraft type: Rotorcraft - Category: Rotorcraft - Engines: 1 · Turbo-shaft - Seats: 8 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS R00007RD](https://openairdocs.org/tcds/R00007RD) (OpenAirDocs) - Holder: Leonardo S.p.A. - Registered aircraft: 1 - Page: https://openairdocs.org/model/leonardo-s-p-a-aw119-mkii 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. None matched. ## Registered aircraft (1) - [N602FB](https://openairdocs.org/aircraft/N602FB): [Bristow LLC](https://openairdocs.org/faa-owner/BRISTOW%20LLC), [Lake Charles, LA](https://openairdocs.org/faa-place/LA/Lake%20Charles), built 2007, S/N 14528 ## 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/leonardo-s-p-a-aw119-mkii/reports.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 - [Agusta AW119MKII](https://openairdocs.org/model/agusta-aw119mkii): 1 registered aircraft, registry code 0260130 --- 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.