# Service difficulty reports: Agusta A119

A list on [Agusta A119](https://openairdocs.org/model/agusta-a119.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 130 reports

- [SDR U0GA202403210862](https://openairdocs.org/sdr/U0GA202403210862.md): Unknown · odor · Mar 20, 2024 · N715R · Agusta A119 · Air Distribution System
  > 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.md): Unknown · odor · Jan 6, 2022 · N605CF · Agusta A119 · Air Distribution System
  > 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 INSPECTION WAS PERFORMED AND NO LEAKAGE WAS FOUND. SUSPECT RESIDUAL ODOR WAS STILL PRESENT ON EQUIP
- [SDR QMLA2022010720003](https://openairdocs.org/sdr/QMLA2022010720003.md): Flow Divider · none · Jan 2, 2022 · N605CF · Agusta A119 · Aircraft Fuel System
  > 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.md): Transmission · none · Jan 1, 2022 · N803CF · Agusta A119 · Main Rotor Drive System
  > 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 FOUND MULTIPLE CHIPS ON BOTH. AFTYER DRAINING SYSTEM AND ISPECTING FLUID FROM FILTER HOUSING, GEARBOX AN
- [SDR QMLA2019081429066](https://openairdocs.org/sdr/QMLA2019081429066.md): Plate · cracked · Aug 2, 2019 · N303CF · Agusta A119 · Fuselage Main, Plate/Skin
  > RT TORQUE PLATE HAS A 1 IN. CRACK. AIRCRAFT REMAINS OUT OF SERVICE AT THIS TIME.
- [SDR QMLA2019072619062](https://openairdocs.org/sdr/QMLA2019072619062.md): Pressure Switch · unserviceable · Jul 26, 2019 · N207CF · Agusta A119 · Engine Oil Pressure
  > 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 SHOWING GOOD PRESSURE, BUT THE LIGHT WAS ILLUMANTED ON MASTER CAUTION PANEL. REMOVED AND REPLACED OIL
- [SDR QMLA2019040819035](https://openairdocs.org/sdr/QMLA2019040819035.md): Bulkhead · cracked · Apr 8, 2019 · N521RQ · Agusta A119 · Fuselage Main, Bulkhead
  > 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 THE BULKHEAD.
- [SDR QMLA2019022219021](https://openairdocs.org/sdr/QMLA2019022219021.md): Bulkhead · cracked · Feb 22, 2019 · Agusta A119 · Fuselage Main, Bulkhead
  > 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.md): Abrasion Strip · debonded · Jan 24, 2019 · N521RQ · Agusta A119 · Main Rotor Blades
  > 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 UNBONDED ON THE MOST INBOARD LOWER SIDE OF THE ABRASION STRIP.
- [SDR QMLA2018122918138](https://openairdocs.org/sdr/QMLA2018122918138.md): Angle · cracked · Dec 29, 2018 · N605CF · Agusta A119 · Fuselage Miscellaneous Structure
  > 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.md): Blade · damaged · Dec 11, 2018 · N521RQ · Agusta A119 · Main Rotor Blades
  > 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/CRACKED.
- [SDR QMLA2018120548128](https://openairdocs.org/sdr/QMLA2018120548128.md): Connector · loose · Dec 4, 2018 · N604CF · Agusta A119 · Main Rotor Drive System Wiring
  > 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 CLEANED CANNON PLUG FOR PRESSURE TRANSDUCER COULD NOT DUPLICATE DROP IN PRESSURE. PREFORMED OP GROU
- [SDR QMLA2018112718124](https://openairdocs.org/sdr/QMLA2018112718124.md): Fire Loop · chafed · Nov 27, 2018 · N603CF · Agusta A119 · Fire Detection
  > 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.md): Plate · cracked · Nov 26, 2018 · N202CF · Agusta A119 · Main Rotor Gearbox
  > TRANSMISSION TORQUE PLATES FOUND CRACKED DURING EDDIE CURRENT INSPECTION.
- [SDR QMLA2018111118120](https://openairdocs.org/sdr/QMLA2018111118120.md): Crosstube · failed · Nov 11, 2018 · N803CF · Agusta A119 · Main Landing Gear Strut/Axle/Truck
  > AFTER RETURNING FROM FLIGHT ON LANDING AIRCRAFT TILTED TO THE LEFT, FORWARD LANDING GEAR CROSSTUBE FAILED.
- [SDR QMLA2018071618081](https://openairdocs.org/sdr/QMLA2018071618081.md): Bypass Valve · defective · Jul 14, 2018 · N353LL · Agusta A119 · Engine Oil Temperature Regulator
  > 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 EXCEEDANCE. HE ANNOUNCED THE WARNING LIGHT AND REDUCED POWER AND AIRSPEED. HE PERFORMED A PRE-LANDING GAU
- [SDR QMLA2018071318082](https://openairdocs.org/sdr/QMLA2018071318082.md): Skin · cracked · Jul 13, 2018 · N604CF · Agusta A119 · Fuselage Main, Plate/Skin
  > 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 REF ASRP 3C-A-53-13-01-02A-664A-D CREW DOOR POST SPECIAL REPAIR.
- [SDR QMLA2018070918077](https://openairdocs.org/sdr/QMLA2018070918077.md): Angle · cracked · Jul 6, 2018 · N605CF · Agusta A119 · Fuselage Miscellaneous Structure
  > 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 CHANNELS ARE CRACKED.
- [SDR QMLA2018061518073](https://openairdocs.org/sdr/QMLA2018061518073.md): Fitting · cracked · Jun 15, 2018 · N357LL · Agusta A119 · Fuselage Main, Attach Fittings
  > FOUND A CRACKED LT TRANSMISSION FITTING DURING AN INSPECTION IAW ENGINEERING ORDER 49-5300-EO-2335.
- [SDR QMLA2018060518067](https://openairdocs.org/sdr/QMLA2018060518067.md): Fitting · cracked · Jun 5, 2018 · N353LL · Agusta A119 · Main Rotor Transmission Mount
  > FOUND CRACKED RT TRANSMISSION FITTING, 75MM LONG.
- [SDR QMLA2018052317118](https://openairdocs.org/sdr/QMLA2018052317118.md): Box Beam · cracked · May 22, 2018 · N207CF · Agusta A119 · Fuselage Main, Structure
  > 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 3525, WATER LINE 1400, BUTT LINE 520 LEFT AND RIGHT
- [SDR QMLA2018052918064](https://openairdocs.org/sdr/QMLA2018052918064.md): Fitting · cracked · May 21, 2018 · N355LL · Agusta A119 · Main Rotor Transmission Mount
  > FOUND A CRACKED RT TRANSMISSION FITTING DURING AN EDDY CURRENT INSPECTION IAW EO 49-5300-EO-2335.
- [SDR QMLA2018052118061](https://openairdocs.org/sdr/QMLA2018052118061.md): Case · damaged · May 21, 2018 · N511SL · Agusta A119 · Tail Rotor Gearbox
  > 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 BE 3.34MM DEEP.
- [SDR QMLA2018052988065](https://openairdocs.org/sdr/QMLA2018052988065.md): Fitting · cracked · May 18, 2018 · N352LL · Agusta A119 · Main Rotor Transmission Mount
  > 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.md): Not Reported · cracked · Apr 27, 2018 · N609CF · Agusta A119 · Fuselage Structure (General)
  > 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 & 50MM. / TWO CRACKS FOUND AT STATION 4010, BUTT LINE 0 & 1, WATER LINE 1020 MEASURING 8MM & 10MM. / O
- [SDR QMLA2018042018045](https://openairdocs.org/sdr/QMLA2018042018045.md): Post · cracked · Apr 20, 2018 · N511SL · Agusta A119 · Fuselage Main, Structure
  > 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.md): Bulkhead · cracked · Apr 18, 2018 · N207CF · Agusta A119 · Fuselage Main, Bulkhead
  > 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 REMOVED. ON FUSELAGE STATION 2049.5, WL 1550, LBL 520 LT AND RT SIDES UPPER BULKHEADS HAVE 1-2 INC
- [SDR QMLA2018040918043](https://openairdocs.org/sdr/QMLA2018040918043.md): Blade · cracked · Apr 9, 2018 · N609CF · Agusta A119 · Main Rotor Blades
  > 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.md): Door Frame · cracked · Apr 2, 2018 · N511SL · Agusta A119 · Fuselage Main, Structure
  > 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.md): Gcu · failed · Mar 19, 2018 · N603CF · Agusta A119 · DC Generating System
  > 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 ILLUMINATED. FAILURES LISTED IN APPROXIMATE CHRONOLOGICAL ORDER: -INVERTER 1 -INVERTER 2 (THIS INITI
- [SDR QMLA2018031218029](https://openairdocs.org/sdr/QMLA2018031218029.md): Module · malfunctioned · Mar 8, 2018 · N603CF · Agusta A119 · Engine Temperature Indicating System
  > AIRCRAFT DEPARTED, SHORTY AFTER TAKEOFF, DURING CLIMB TO CRUISING ALTITUDE, NOTICED THE ENGINE ITT INDICATION WAS READING ERRATICALLY. THE TEMPERATURE WAS DROPPING FROM THE NORMAL 660, TO 605 AND EVEN DIPPED TO 590 AT ONE POINT. THIS HAPPENED SEVERAL TIMES
- [SDR QMLA2018022718024](https://openairdocs.org/sdr/QMLA2018022718024.md): Skin · cracked · Feb 27, 2018 · N521RQ · Agusta A119 · Horizontal Stabilizer, Plate/Skin
  > 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 SKIN ASSEMBLY, AND 4 INCHES OF THE OUT BOARD EDGE OF THE STABILIZER SKIN, PARALLEL TO THE SPAR.
- [SDR QMLA2018022118019](https://openairdocs.org/sdr/QMLA2018022118019.md): Fitting · cracked · Feb 21, 2018 · N351LL · Agusta A119 · Fuselage Miscellaneous Structure
  > FOUND CRACKED R/H TRANSMISSION FITTING P/N 109-0330-17-106 DURING 800 HOUR INSPECTION.
- [SDR QMLA2018020918017](https://openairdocs.org/sdr/QMLA2018020918017.md): Firewall · cracked · Feb 9, 2018 · N604CF · Agusta A119 · Fuselage Main, Bulkhead
  > 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 IS AT ABOUT 5 INCHES LEFT OF THE BL LINE. THE 50MM CRACK IS AT 3 INCHES LEFT OF THE BL LINE. ON
- [SDR QMLA2017122017142](https://openairdocs.org/sdr/QMLA2017122017142.md): Retainer · cracked · Dec 20, 2017 · N351LL · Agusta A119 · Fuselage Main, Structure
  > 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.md): Skin · cracked · Dec 19, 2017 · N609CF · Agusta A119 · Rotorcraft Tail Boom
  > 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 CRACK WAS LOCATED AT BS 8085, WL 1400 ON PILOTS SIDE OF TAILBOOM THERE WAS A 2.25 INCH CRACK NOTED A
- [SDR QMLA2017031317028](https://openairdocs.org/sdr/QMLA2017031317028.md): Doubler · cracked · Mar 13, 2017 · N803CF · Agusta A119 · Rotorcraft Tail Boom
  > 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.md): Wire · broken · Feb 19, 2017 · N207CF · Agusta A119 · Electrical Power System Wiring
  > 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. CHECKED THE COCKPIT FOR ANY SMOKE AND NONE NOTED. CONTINUE TO THE CLOSEST AIRPORT, ON LANDING AND
- [SDR QMLA2017020617018](https://openairdocs.org/sdr/QMLA2017020617018.md): Bracket · cracked · Feb 6, 2017 · N103CF · Agusta A119 · Fuselage Main, Attach Fittings
  > 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 2049.5, WL 1550-1400, LBL 125 AND MEASURED 3.5 INCHES. THE SECOND CRACK WAS LOCATED ON THE RT SIDE
- [SDR QMLA2017011117009](https://openairdocs.org/sdr/QMLA2017011117009.md): Doubler · cracked · Jan 11, 2017 · N609CF · Agusta A119 · Rotorcraft Tail Boom
  > 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 LOCATED IN THE RADIUS BEND OF DOUBLER TOWARDS UPPER RIGHT HAND EDGE BEHIND NUTPLATE.
- [SDR QMLA2017010917007](https://openairdocs.org/sdr/QMLA2017010917007.md): Bracket · cracked · Jan 9, 2017 · N203CF · Agusta A119 · Rotorcraft Tail Boom
  > 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.md): Ground Wire · disconnected · Dec 26, 2016 · N603CF · Agusta A119 · Oxygen System Wiring
  > THE CELESTIAL ILLUMINATION WAS DIMINISHING AND THE CREW ASKED FOR THE CABIN LIGHTING. TURNING ON THE LIGHTING, THE REAR CABIN LIGHTING DIMMED, FLICKERED, AND BRIGHTENED BEFORE GOING OUT. THE CABIN LIGHTING SWITCH RESET TO OFF. REPORT OF SMOKE AND FUMES IN THE
- [SDR 2A6R20161213002](https://openairdocs.org/sdr/2A6R20161213002.md): Transceiver · defective · Dec 13, 2016 · N511SL · Agusta A119 · Communications System
  > 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 DIFFICULT TO CONNECT FOR PROGRAMMING. WE ARE SENDING THE RADIO OUT FOR REPAIR.
- [SDR 2A6R20161213001](https://openairdocs.org/sdr/2A6R20161213001.md): Fuel Cell · damaged · Dec 13, 2016 · N511SL · Agusta A119 · Fuel Storage
  > 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 MISALIGNED, UNABLE TO USE FUEL CELL, WILL RETURN FOR REPAIR OR REPLACE FUEL CELL WITH SERVICEABLE PART.
- [SDR QMLA2016120916142](https://openairdocs.org/sdr/QMLA2016120916142.md): Support Frame · cracked · Dec 9, 2016 · N303CF · Agusta A119 · Fuselage Main, Structure
  > 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.md): Support Channel · cracked · Dec 6, 2016 · N203CF · Agusta A119 · Fuselage Miscellaneous Structure
  > 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.md): Channel · cracked · Dec 5, 2016 · N203CF · Agusta A119 · Fuselage Main, Plate/Skin
  > 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 CHANNEL "SPINE" EMANATE AROUND THE FASTENER HOLES FOR THE FORWARD ENGINE MOUNT. THE CRACKS ARE AROUND TH
- [SDR QMLA2016112816136](https://openairdocs.org/sdr/QMLA2016112816136.md): Circuit Breaker · failed · Nov 28, 2016 · N207CF · Agusta A119 · DC Power Distribution System
  > 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 FURTHER TROUBLESHOOTING, IT WAS DETERMINED THAT A WIRE FOR THE GOV CONTROL BREAKER HAD CHAFED NEXT TO A
- [SDR QMLA2016110916131](https://openairdocs.org/sdr/QMLA2016110916131.md): Angle · cracked · Nov 9, 2016 · N203CF · Agusta A119 · Fuselage Miscellaneous Structure
  > 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.md): Angle · cracked · Nov 9, 2016 · N202CF · Agusta A119 · Fuselage Miscellaneous Structure
  > WHILE COMPLETING FURTHER INSPECTIONS IT WAS NOTED THAT AT STA 4010 WL 1020 A LT ANGLE WAS CRACKED INSIDE THE INSPECTION ACCESS HOLE.

Next page: https://openairdocs.org/model/agusta-a119/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = 'A119'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/agusta-a119/reports

---
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