# Agusta A119

- Type: Aircraft model (FAA registry)
- Registry code: 0260102
- Manufacturer (registry): AGUSTA SPA
- Model: A119
- 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: 12
- Page: https://openairdocs.org/model/agusta-a119

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 2021-16-06](https://openairdocs.org/ad/2021-16-06): Tail Rotor Drive Shaft · Leonardo A119 and AW119 MKII. Effective Sep 27, 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 2014-09-01](https://openairdocs.org/ad/2014-09-01): Tail Rotor · Agusta A109C, A109E, A109K2 and 1 more. Effective Jun 5, 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 2013-05-22](https://openairdocs.org/ad/2013-05-22): Tail rotor pitch control link assembly · Agusta A109, A109A, A109A II and 5 more. Effective Apr 30, 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
- [AD 2008-14-05](https://openairdocs.org/ad/2008-14-05): Tail rotor control · Agusta A109E and A119. Effective Aug 21, 2008
- [AD 2008-12-11](https://openairdocs.org/ad/2008-12-11): Emergency door release · Agusta A109E, A109S and A119. Effective Jul 1, 2008
- [AD 2005-09-06](https://openairdocs.org/ad/2005-09-06): Main transmission support fitting (fitting) attachment bolt (bolt) · Agusta A119. Effective Jun 13, 2005
- [AD 2002-21-04](https://openairdocs.org/ad/2002-21-04): Tail rotor blade · Agusta A119. Effective Oct 31, 2002
- [AD 2001-22-51](https://openairdocs.org/ad/2001-22-51): Part-numbered Tail Rotor Blade · Agusta A119. Effective Dec 26, 2001

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
- [AD 2002-17-52](https://openairdocs.org/ad/2002-17-52) (historical): Tail rotor blade · Agusta A119
- [AD 2002-14-51](https://openairdocs.org/ad/2002-14-51) (historical): Tail Rotor Blade · Agusta A109E and A119

## Information bulletins (advisory) (4)

- [SAIB SW-18-13](https://openairdocs.org/saib/SW-18-13): Main Transmission Plate Fitting. Issued Apr 30, 2018
- [SAIB SW-15-20](https://openairdocs.org/saib/SW-15-20): Air Conditioning System Wiring. Issued Aug 13, 2015
- [SAIB SW-12-45](https://openairdocs.org/saib/SW-12-45): Garmin Model 400W/500W Series GPS-WAAS Navigation System. Issued Oct 3, 2012
- [SAIB SW-05-82](https://openairdocs.org/saib/SW-05-82): . Issued Aug 19, 2005

## Registered aircraft (12)

- [N108AG](https://openairdocs.org/aircraft/N108AG): [Bristow LLC](https://openairdocs.org/faa-owner/BRISTOW%20LLC), [Lake Charles, LA](https://openairdocs.org/faa-place/LA/Lake%20Charles), built 2005, S/N 14053
- [N119RW](https://openairdocs.org/aircraft/N119RW): [Huntingdon Valley, PA](https://openairdocs.org/faa-place/PA/Huntingdon%20Valley), built 2006, S/N 14508, Registration pending
- [N119WG](https://openairdocs.org/aircraft/N119WG): [High Performance Helicopters Corp](https://openairdocs.org/faa-owner/HIGH%20PERFORMANCE%20HELICOPTERS%20CORP), [Crestline, CA](https://openairdocs.org/faa-place/CA/Crestline), built 2005, S/N 14502
- [N316PD](https://openairdocs.org/aircraft/N316PD): [Longhorn Air LLC](https://openairdocs.org/faa-owner/LONGHORN%20AIR%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2003, S/N 14038
- [N319PD](https://openairdocs.org/aircraft/N319PD): [Aerotrust Services Corp Trustee](https://openairdocs.org/faa-owner/AEROTRUST%20SERVICES%20CORP%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2004, S/N 14040
- [N58CM](https://openairdocs.org/aircraft/N58CM): [Crystal Motorsports LLC](https://openairdocs.org/faa-owner/CRYSTAL%20MOTORSPORTS%20LLC), [Crystal River, FL](https://openairdocs.org/faa-place/FL/Crystal%20River), S/N 14030
- [N671MH](https://openairdocs.org/aircraft/N671MH): [Mansfield Heliflight Inc](https://openairdocs.org/faa-owner/MANSFIELD%20HELIFLIGHT%20INC), [Milton, VT](https://openairdocs.org/faa-place/VT/Milton), S/N 14507
- [N709CG](https://openairdocs.org/aircraft/N709CG): [Bristow LLC](https://openairdocs.org/faa-owner/BRISTOW%20LLC), [Lake Charles, LA](https://openairdocs.org/faa-place/LA/Lake%20Charles), S/N 14052
- [N715RT](https://openairdocs.org/aircraft/N715RT): [Bristow LLC](https://openairdocs.org/faa-owner/BRISTOW%20LLC), [Lake Charles, LA](https://openairdocs.org/faa-place/LA/Lake%20Charles), built 2006, S/N 14516
- [N72SL](https://openairdocs.org/aircraft/N72SL): [Mhm Logistics LLC](https://openairdocs.org/faa-owner/MHM%20LOGISTICS%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2005, S/N 14501
- [N794DM](https://openairdocs.org/aircraft/N794DM): [Red River Aircraft Leasing LLC](https://openairdocs.org/faa-owner/RED%20RIVER%20AIRCRAFT%20LEASING%20LLC), [Anchorage, AK](https://openairdocs.org/faa-place/AK/Anchorage), built 2006, S/N 14512
- [N822MM](https://openairdocs.org/aircraft/N822MM): [Bristow LLC](https://openairdocs.org/faa-owner/BRISTOW%20LLC), [Lake Charles, LA](https://openairdocs.org/faa-place/LA/Lake%20Charles), built 2005, S/N 14055

## NTSB investigations (5)

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 GAA21WA088](https://openairdocs.org/ntsb/GAA21WA088), Apr 23, 2021: Agusta A119 (N119AA), Nuevo Laredo, Mexico, substantial damage, 1 fatal
- [NTSB WPR13IA020](https://openairdocs.org/ntsb/WPR13IA020), Oct 20, 2012: Agusta A119 (N207CF), Dolan Springs, AZ, incident, minor damage. Probable cause: Insufficient clearance between a truck and the main rotor blades of a helicopter on the ground with the engine running because of the lack of on-scene coordination between the agencies that responded…
- [NTSB WPR10FA029](https://openairdocs.org/ntsb/WPR10FA029), Oct 23, 2009: Agusta A119 (N119AH), Blythe, CA, substantial damage. Probable cause: The loss of engine power during cruise flight for undetermined reasons.
- [NTSB DEN05FA103](https://openairdocs.org/ntsb/DEN05FA103), Jun 30, 2005: Agusta A119 (N403CF), Mancos, CO, substantial damage, 3 fatal. Probable cause: a loss of engine power for undetermined reasons and the pilot's inability to get into autorotation prior to impacting the ground. A factor contributing to the accident was the helicopter's low…
- [NTSB DEN02LA010](https://openairdocs.org/ntsb/DEN02LA010), Nov 9, 2001: Agusta A119 (N119RX), Ogden, UT, destroyed. Probable cause: improper rigging of the rotary variable differential transformer by the manufacturer, resulting in incorrect fuel scheduling to the fuel control unit.

## FAA accident and incident reports (6)

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.

- [Incident 20180828012449I](https://openairdocs.org/incident/20180828012449I), Aug 28, 2018: Agusta Spa A119 (N108AG), Galveston, TX, Minor damage. While on approach to gulf oil platform HIA547B, the pilot maneuvered over the deck. He stated he had a "pla" (power lever angle) message illuminate and the…
- [Incident 20141006022809I](https://openairdocs.org/incident/20141006022809I), Oct 6, 2014: Agusta Spa A119 (N603CF), Indio, CA, Minor damage. Careflight 2, N603CF, an Agusta A119 operated by tristate careflight LLC, struck a fence with its tail rotor while picking up a patient at Chiriaco Summit…
- [Incident 20121019024449I](https://openairdocs.org/incident/20121019024449I), Oct 19, 2012: Agusta Spa A119 (N207CF), Dolan Springs, AZ, Minor damage. Aircraft landed at the scene of a motor vehicle crash involving two tour buses, resulting in multiple casualties. Aircraft was the last of multiple EMS…
- [Accident 20091022021679A](https://openairdocs.org/incident/20091022021679A), Oct 22, 2009: Agusta A119 (N119AH), Blythe, CA, Substantial damage. Operator encountered a main rotor RPM drop (power loss) and a subsequent emergency (forced) landing.
- [Accident 20050630012169A](https://openairdocs.org/incident/20050630012169A), Jun 30, 2005: Agusta A119 (N403CF), Mancos, CO, Destroyed, 3 fatal. (-23) Aircraft was observed on approach to landing zone at approximately 200 feet AGL, 9730 feet MSL, temp 20 degrees c, with suspected tail wind of…
- [Accident 20011109032959A](https://openairdocs.org/incident/20011109032959A), Nov 9, 2001: Agusta A119 (N119RX), Ogden, UT, No damage. (-23) As the pilot reduced collective pitch on final approach for landing, N2 and rotor RPM decreased and stabilized at about 96%, with the low RPM light and…

## Service difficulty reports (130, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR U0GA202403210862](https://openairdocs.org/sdr/U0GA202403210862), Mar 20, 2024: UNKNOWN. ODOR. FUEL FUMES IN THE BACK CABIN NEAR LEFT REAR SEAT. MAINTENANCE INVESTIGATION – INSPECTED FUEL SYSTEM FOR LEAKS AND SPILLAGE, NO DEFECTS NOTED. (TL-257167-2024)
- [SDR QMLA2022010720004](https://openairdocs.org/sdr/QMLA2022010720004), Jan 6, 2022: UNKNOWN. ODOR. WHILE PERFORMING OPERATIONAL CHECK FLIGHT FUEL ODOR WAS PRESENT IN AIRCRAFT CABIN. IN THE AIRCRAFT AND DID NOT SMELL ANY ODOR OF FUEL AFTER LANDING. THOROUGH IN
- [SDR QMLA2022010720003](https://openairdocs.org/sdr/QMLA2022010720003), Jan 2, 2022: FLOW DIVIDER. NONE. UPON LANDING AT KINGMAN REGIONAL AIRPORT PILOT REPORTED MASSIVE FUEL LEAK AS NOTICED DURING HIS POST FLIGHT INSPECTION.
- [SDR QMLA2022010420002](https://openairdocs.org/sdr/QMLA2022010420002), Jan 1, 2022: TRANSMISSION. NONE. UPON START UP PILOT GOT MASTER WARNIG CAUTION "TRANSMISSION CHIP LIGHT" AND SHUT DOWN AC. I CAME TO BASE AND INSPECTED BOTH TRANSMISSION CHIP DETECTORS AND FOUN
- [SDR QMLA2019081429066](https://openairdocs.org/sdr/QMLA2019081429066), Aug 2, 2019: PLATE. CRACKED. RT TORQUE PLATE HAS A 1 IN. CRACK. AIRCRAFT REMAINS OUT OF SERVICE AT THIS TIME.
- [SDR QMLA2019072619062](https://openairdocs.org/sdr/QMLA2019072619062), Jul 26, 2019: PRESSURE SWITCH. UNSERVICEABLE. DURING FLIGHT APPROX 20 MINUTES INTO IT ENGINE OIL PRESSURE LIGHT CAME ON. PILOT MADE PRECAUTIONARY LANDING IN CLEAR AREA. THE OIL PRESSURE GAUGE WAS STILL SHOW
- [SDR QMLA2019040819035](https://openairdocs.org/sdr/QMLA2019040819035), Apr 8, 2019: BULKHEAD. CRACKED. 76 MM CRACK FOUND IN A BULKHEAD AT STA 3539 BL 432 WL 1016 JUST AFT OF THE REAR BULKHEAD STA 3525. CRACK LOOKS TO BE FROM STRESS AROUND AN AN FITTING GOING THRU
- [SDR QMLA2019022219021](https://openairdocs.org/sdr/QMLA2019022219021), Feb 22, 2019: BULKHEAD. CRACKED. FOUND CRACKS ON THE LT BULKHEAD STA 3525, BL 440, WL 1700 MEASURING 18MM AND RT SIDE STA 3525, BL 440, WL 1700 MEASURING 10MM.
- [SDR QMLA2019012419013](https://openairdocs.org/sdr/QMLA2019012419013), Jan 24, 2019: ABRASION STRIP. DEBONDED. DURING PREFLIGHT OF AIRCRAFT, MAIN ROTOR BLADE P/N 709-0104-01-101 S/N L173 WAS FOUND WITH A 3-4 INCH SECTION OF THE LEADING EDGE ABRASION STRIP HAD BECOME UNBO
- [SDR QMLA2018122918138](https://openairdocs.org/sdr/QMLA2018122918138), Dec 29, 2018: ANGLE. CRACKED. WHILE INSPECTING COCKPIT OVERHEAD WIRING FOR A SEPARATE DISCREPANCY, I DISCOVERED CRACKS IN A VERTICAL ANGLE IN THE CO-PILOT OVERHEAD AREA OF THE FUSELAGE.
- [SDR QMLA2018121118131](https://openairdocs.org/sdr/QMLA2018121118131), Dec 11, 2018: BLADE. DAMAGED. DURING PREFLIGHT OF AIRCRAFT, MAIN ROTOR BLADE P/N 709-0104-01-101 S/N A5-0111 WAS FOUND WITH A 4 INCH SECTION OF THE TIP CAP LEADING EDGE THAT IS DAMAGED/CRACK
- [SDR QMLA2018120548128](https://openairdocs.org/sdr/QMLA2018120548128), Dec 4, 2018: CONNECTOR. LOOSE. CANNON PLUG FOR PRESSURE SWITCH HAD LOSE CONNECTIONS IN PLUG WHICH CAUSED RED XMSN OIL PRESS LIGHT. HAD TO REMOVED CANNON PLUG AND REINSTALL PINS. PULLED AND CL
- [SDR QMLA2018112718124](https://openairdocs.org/sdr/QMLA2018112718124), Nov 27, 2018: FIRE LOOP. CHAFED. DURING FLIGHT BACK TO BASE THE FIRE DETECT LIGHT ILLUMINATED, REPLACED FIRE DETECTOR LOOP AFTER FINDING A CHAFE
- [SDR QMLA2018112868126](https://openairdocs.org/sdr/QMLA2018112868126), Nov 26, 2018: PLATE. CRACKED. TRANSMISSION TORQUE PLATES FOUND CRACKED DURING EDDIE CURRENT INSPECTION.
- [SDR QMLA2018111118120](https://openairdocs.org/sdr/QMLA2018111118120), Nov 11, 2018: CROSSTUBE. FAILED. AFTER RETURNING FROM FLIGHT ON LANDING AIRCRAFT TILTED TO THE LEFT, FORWARD LANDING GEAR CROSSTUBE FAILED.
- [SDR QMLA2018071618081](https://openairdocs.org/sdr/QMLA2018071618081), Jul 14, 2018: BYPASS VALVE. DEFECTIVE. ROUGHLY 5 MINUTES AFTER DEPARTURE, PILOT OBSERVED A ENG HOT OIL WARNING LIGHT ILLUMINATION. HE CHECKED THE OIL TEMP GAUGE AND CONFIRMED AN ENGINE OIL TEMP EXCEE
- [SDR QMLA2018071318082](https://openairdocs.org/sdr/QMLA2018071318082), Jul 13, 2018: SKIN. CRACKED. ON VERTICAL TAIL FIN CAP FOUND CRACK APP 1-2" IN LENGTH AT AFT OF STA 9725. ON L/H COPILOT DOOR POST STA 2049.5 WL1400 BL 520 FOUND A CRACK APP.1.15" IN LENGTH 
- [SDR QMLA2018070918077](https://openairdocs.org/sdr/QMLA2018070918077), Jul 6, 2018: ANGLE. CRACKED. AFTER REVIEW OF AIRCRAFT IT WAS NOTED THAT THE CANOPY ANGLE, AFT OF THE GREEN HOUSE WINDOWS WAS CRACKED IN SEVERAL AREAS. ALSO BOTH LT AND RT VERTICAL SUPPORT C
- [SDR QMLA2018061518073](https://openairdocs.org/sdr/QMLA2018061518073), Jun 15, 2018: FITTING. CRACKED. FOUND A CRACKED LT TRANSMISSION FITTING DURING AN INSPECTION IAW ENGINEERING ORDER 49-5300-EO-2335.
- [SDR QMLA2018060518067](https://openairdocs.org/sdr/QMLA2018060518067), Jun 5, 2018: FITTING. CRACKED. FOUND CRACKED RT TRANSMISSION FITTING, 75MM LONG .
- [SDR QMLA2018052317118](https://openairdocs.org/sdr/QMLA2018052317118), May 22, 2018: BOX BEAM. CRACKED. WHILE COMPLETING UPPER TRANSMISSION DECK REPLACEMENT IT WAS DISCOVERED THE LEFT AND RIGHT LOWER SKIN OF THE BOX BEAMS WAS CRACKED NEAR THE TRANSMISSION. STATION
- [SDR QMLA2018052918064](https://openairdocs.org/sdr/QMLA2018052918064), May 21, 2018: FITTING. CRACKED. FOUND A CRACKED RT TRANSMISSION FITTING DURING AN EDDY CURRENT INSPECTION IAW EO 49-5300-EO-2335.
- [SDR QMLA2018052118061](https://openairdocs.org/sdr/QMLA2018052118061), May 21, 2018: CASE. DAMAGED. ON REMOVING THE TAIL ROTOR GEARBOX COWLING TO PERFORM AN INSPECTION, NOTED DAMAGE TO THE GEARBOX CASE CAUSED BY IMPROPER HARDWARE LOCATION. DAMAGE WAS NOTED TO 
- [SDR QMLA2018052988065](https://openairdocs.org/sdr/QMLA2018052988065), May 18, 2018: FITTING. CRACKED. FOUND A CRACKED LT TRANSMISSION FITTING, FOUND DURING AN EDDY CURRENT INSPECTION IAW EO 49-5300-EO-2335.
- [SDR QMLA2018042718050](https://openairdocs.org/sdr/QMLA2018042718050), Apr 27, 2018: NOT REPORTED. CRACKED. ONE CRACK FOUND AT B.L. 510, STATION 3627 W.L. 1349 MEASURING 30MM IN LENGTH. / TWO CRACKS FOUND AT STATION 4010, BUTT LINE 6, WATER LINE 1020 MEASURING 30MM & 
- [SDR QMLA2018042018045](https://openairdocs.org/sdr/QMLA2018042018045), Apr 20, 2018: POST. CRACKED. DURING INSPECTION, FOUND A CRACK IN THE LT PASSENGER DOOR FWD POST AT BS 2184MM AND WL 610MM.
- [SDR QMLA2018041900118](https://openairdocs.org/sdr/QMLA2018041900118), Apr 18, 2018: BULKHEAD. CRACKED. WHILE PERFORMING REPAIR OF RT FORWARD PILOT OVERHEAD BULKHEAD FRAME IAW SRM 04-01-19, MULTIPLE CRACKS WERE DISCOVERED WHEN SEALANT WAS REMOVED AND OLD FRAME WAS
- [SDR QMLA2018040918043](https://openairdocs.org/sdr/QMLA2018040918043), Apr 9, 2018: BLADE. CRACKED. 1.5 INCH CRACK FOUND ON TRAILING EDGE OF BLADE FAIRING. CRACK STARTS AT 60MM FROM TOP OF BLADE FAIRING AND RUNS DOWN AND UNDERNEATH BLADE.
- [SDR QMLA2018040218039](https://openairdocs.org/sdr/QMLA2018040218039), Apr 2, 2018: DOOR FRAME. CRACKED. DURING INSPECTION, FOUND A CRACK IN THE RT PASSENGER DOOR AFT POST AT BS 3240 AND WL 850. CRACK WAS NOTED TO BE APPROXIMATELY 5 - 6 MM LONG.
- [SDR QMLA2018031918034](https://openairdocs.org/sdr/QMLA2018031918034), Mar 19, 2018: GCU. FAILED. WHILE IN CRUISE FLIGHT OVER AN APPROXIMATE TWO MINUTE PERIOD THE FOLLOWING SYSTEMS FAILED. EACH FAILURE WAS INDICATED ON EDU 1 HOWEVER THE MASTER CAUTION NEVER 
- [SDR QMLA2018031218029](https://openairdocs.org/sdr/QMLA2018031218029), Mar 8, 2018: MODULE. MALFUNCTIONED. AIRCRAFT DEPARTED, SHORTY AFTER TAKEOFF, DURING CLIMB TO CRUISING ALTITUDE, NOTICED THE ENGINE ITT INDICATION WAS READING ERRATICALLY. THE TEMPERATURE WAS DROPP
- [SDR QMLA2018022718024](https://openairdocs.org/sdr/QMLA2018022718024), Feb 27, 2018: SKIN. CRACKED. DURING INSPECTION A 5450 OF HORIZONTAL STABILIZER A 2 INCH CRACK WAS FOUND ON THE LOWER SKIN OF THE LT STABILIZER, 3/4 OF AN INCH FROM THE LEADING EDGE OF THE S
- [SDR QMLA2018022118019](https://openairdocs.org/sdr/QMLA2018022118019), Feb 21, 2018: FITTING. CRACKED. FOUND CRACKED R/H TRANSMISSION FITTING P/N 109-0330-17-106 DURING 800 HOUR INSPECTION.
- [SDR QMLA2018020918017](https://openairdocs.org/sdr/QMLA2018020918017), Feb 9, 2018: FIREWALL. CRACKED. DURING DAILY INSPECTION, FOUR CRACKS WERE FOUND ON THE ENGINE FORWARD SLANTED FIREWALL. ALL CRACKS ARE AT BS 3390, WL 1765. 50 MM CRACK IS AT 1762,. 30 MM CRACK
- [SDR QMLA2017122017142](https://openairdocs.org/sdr/QMLA2017122017142), Dec 20, 2017: RETAINER. CRACKED. CRACK FOUND ON THE UPPER RT TRANSPARENCY RETAINER AT BS 2049.5, 2.25 INCHES IN LENGTH ALONG THE RADIUS OF ANGLE.
- [SDR QMLA2017121917140](https://openairdocs.org/sdr/QMLA2017121917140), Dec 19, 2017: SKIN. CRACKED. AFTER PILOT WASHED AIRCRAFT, BS 8081, WL 1300 ON PILOTS SIDE OF TAIL BOOM THERE WAS A 2.5 INCH CRACK SEEN BETWEEN THE MOUNTED STRINGER RIVET LINES. A SECOND CRA
- [SDR QMLA2017031317028](https://openairdocs.org/sdr/QMLA2017031317028), Mar 13, 2017: DOUBLER. CRACKED. ON TAIL ROTOR GEARBOX, 2 CRACKS WERE FOUND ON TAIL BOOM END FRAME DOUBLERS LEFT AND RIGHT, ONE CRACK EACH SIDE.
- [SDR QMLA2017021917020](https://openairdocs.org/sdr/QMLA2017021917020), Feb 19, 2017: WIRE. BROKEN. DURING CRUISE, SMELLED A STONG ACRID ODOR WHICH APPEARED TO BE THAT OF AN ELECTRICAL PROBLEM. MONITORED THE GAUGES AND SAW NO INDICATION OF ANY MALFUNCTION. CHE
- [SDR QMLA2017020617018](https://openairdocs.org/sdr/QMLA2017020617018), Feb 6, 2017: BRACKET. CRACKED. SEVERAL CRACKS HAVE BEEN FOUND ON AN AN BRACKET ATTACHED TO THE AIRCRAFT COCKPIT AND FUSELAGE. FIRST CRACK WAS ON THE LT JUST AFT OF THE GREENHOUSE WINDOW AT BS
- [SDR QMLA2017011117009](https://openairdocs.org/sdr/QMLA2017011117009), Jan 11, 2017: DOUBLER. CRACKED. DURING DAILY AIRWORTHINESS CHECK, AN APPROXIMATELY 1/2" CRACK WAS FOUND ON THE RIGHT HAND TAILROTOR GEARBOX MOUNT BULKHEAD DOUBLER PN 109-0373-21-104. CRACK IS 
- [SDR QMLA2017010917007](https://openairdocs.org/sdr/QMLA2017010917007), Jan 9, 2017: BRACKET. CRACKED. CRACKS FOUND ON THE LT BRACKET AFT PORTION OF THE VERTICAL FIN BETWEEN NUT PLATES WHERE THE CAP MOUNTS ONTO.
- [SDR QMLA2016122616147](https://openairdocs.org/sdr/QMLA2016122616147), Dec 26, 2016: GROUND WIRE. DISCONNECTED. THE CELESTIAL ILLUMINATION WAS DIMINISHING AND THE CREW ASKED FOR THE CABIN LIGHTING. TURNING ON THE LIGHTING, THE REAR CABIN LIGHTING DIMMED, FLICKERED, AND BR
- [SDR 2A6R20161213002](https://openairdocs.org/sdr/2A6R20161213002), Dec 13, 2016: TRANSCEIVER. DEFECTIVE. RECEIVED MULTIBAND RADIO TRANSCEIVER FOR A NEW INSTALLATION. THE RADIO HAS A DATA PORT ON THE FRONT FACE FOR PROGRAMMING THAT IS RECESSED TOO FAR MAKING IT DIFF
- [SDR 2A6R20161213001](https://openairdocs.org/sdr/2A6R20161213001), Dec 13, 2016: FUEL CELL. DAMAGED. SENT LEFT LOWER FUEL CELL P/N 109-0900-40-201, S/N 99000 OUT FOR CLEANING AND INSPECTION, FUEL CELL WAS RETURNED REPAIRED WITH ONE BLANKING PLATE HOLE MISALIGNE
- [SDR QMLA2016120916142](https://openairdocs.org/sdr/QMLA2016120916142), Dec 9, 2016: SUPPORT FRAME. CRACKED. A 1 INCH CRACK WAS LOCATED AT BS 4010 AFT OF FORWARD LOWER ENGINE COWLING LATCH. CRACK ORIGINATED AT THE 90 DEGREE BEND OF THE BASE TO THE EDGE OF THE MATERIAL.
- [SDR QMLA2016120616140](https://openairdocs.org/sdr/QMLA2016120616140), Dec 6, 2016: SUPPORT CHANNEL. CRACKED. AFTER REMOVING LOWER ENGINE FWD SKINS, A NEW CRACKED AREA WAS LOCATED AT STATION 3525 BULKHEAD LT AND RT SIDES WITH EXTRUDED ANGLES AT STATION 4010.
- [SDR QMLA2016120516139](https://openairdocs.org/sdr/QMLA2016120516139), Dec 5, 2016: CHANNEL. CRACKED. AFTER REMOVING LOWER ENGINE DECK SKINS, MULTIPLE CRACKS WERE FOUND AT STA 4010, WL 1020, BL 0 UNDERNEATH FORWARD ENGINE MOUNTS. THE VISIBLE CRACKS ON THE U CHAN
- [SDR QMLA2016112816136](https://openairdocs.org/sdr/QMLA2016112816136), Nov 28, 2016: CIRCUIT BREAKER. FAILED. WHILE AIRCRAFT WAS RETURNING TO BASE, SMOKE AND A BURNING SMELL WAS COMING FROM THE UPPER CIRCUIT BREAKER PANEL CLOSE TO THE GOVERNOR CONTROL BREAKER. AFTER FUR
- [SDR QMLA2016110916131](https://openairdocs.org/sdr/QMLA2016110916131), Nov 9, 2016: ANGLE. CRACKED. WHILE COMPLETING FURTHER INSPECTIONS IT WAS NOTED THAT AT STA 4010 WL 1020 A LT ANGLE WAS CRACKED INSIDE THE INSPECTION ACCESS HOLE.
- [SDR QMLA2016110916130](https://openairdocs.org/sdr/QMLA2016110916130), Nov 9, 2016: ANGLE. CRACKED. WHILE COMPLETING FURTHER INSPECTIONS IT WAS NOTED THAT AT STA 4010 WL 1020 A LT ANGLE WAS CRACKED INSIDE THE INSPECTION ACCESS HOLE.

All 130: https://openairdocs.org/model/agusta-a119/reports.md

## STCs that may be installed (OpenAirDocs) (66, 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 SR04464NY](https://openairdocs.org/stc/SR04464NY): Installation of the iPad Mount. Avio Design Group Inc
- [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 SR00182IB](https://openairdocs.org/stc/SR00182IB): Installation of the Avidyne Integrated Flight Display (IFD) Navigator(s). Horizon Design Services Ltd
- [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc
- [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 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 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 SR01525NY](https://openairdocs.org/stc/SR01525NY): Installation of an Emergency Medical System (EMS). LifePort LLC
- [STC SR01816LA](https://openairdocs.org/stc/SR01816LA): Installation of a Medical Stretcher. LifePort LLC
- [STC SR01865LA](https://openairdocs.org/stc/SR01865LA): Installation of an Emergency Medical Rescue Stretcher. LifePort LLC
- [STC SR00814DE](https://openairdocs.org/stc/SR00814DE): Installation of Garmin Helicopter Terrain Awareness and Warning System (HTAWS). Cert Works LLC
- [STC SR02257CH](https://openairdocs.org/stc/SR02257CH): Install air ambulance conversion. Snaky Creek Enterprises LLC dba Spectrum Aeromed
- [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 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 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 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 SR01124NY-D](https://openairdocs.org/stc/SR01124NY-D): Installation of an Aeromedical Liquid Oxygen System. Sikorsky Aircraft Corporation
- [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 SR03067NY](https://openairdocs.org/stc/SR03067NY): Modification of the cargo hook and addition of a long line hook control circuit. Skyline Helicopters Ltd
- [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
- [STC SR02338CH](https://openairdocs.org/stc/SR02338CH): Installation of a Foreign Object Damage (FOD) Screen or an Inlet Barrier Filter (IBF) System in accordance with Aerospace Filtration Systems, Inc. Drawing 119000, Revision B, dated August 30, 2006, or later FAA approved revision. Aerospace Filtration Systems Inc
- [STC SR02232LA](https://openairdocs.org/stc/SR02232LA): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin AT Inc
- [STC SR09519RC](https://openairdocs.org/stc/SR09519RC): Installation of Night Vision Goggle Compatible Interior Lighting System. Aero Dynamix Inc
- [STC SR01344NY](https://openairdocs.org/stc/SR01344NY): Installation of a Spectrolab SX-5 searchlight. Agusta Aerospace Corporation
- [STC SR00677DE](https://openairdocs.org/stc/SR00677DE): Installation of fixed receivers for ground handling blade folding kit. Paravion Technology Inc

All 66: https://openairdocs.org/model/agusta-a119/stcs.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Agusta Aerospace A119](https://openairdocs.org/model/agusta-aerospace-a119): 0 registered aircraft, registry code 0260104

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