# Service difficulty reports: Turbomeca ARRIEL-2B

A list on [Turbomeca ARRIEL-2B](https://openairdocs.org/engine/turbomeca-arriel-2b.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 7 · 332 reports

- [SDR QMLA2026080920052](https://openairdocs.org/sdr/QMLA2026080920052.md): Elec Connector · burned · Aug 8, 2026 · N910U · Urocop EC130B4 · Air Conditioning System Wiring
  > ON APPROACH PILOT AND CREW DETECTED FAINT ELECTRICAL SMELL NO SMOKE PRESENT. AMT DISCOVERED 1 EACH MOLEX CONNECTER WITH DISCOLORATION REPLAIRED DAMAGED WIRING.
- [SDR QMLA2024110420142](https://openairdocs.org/sdr/QMLA2024110420142.md): Connector · contaminated · Oct 31, 2024 · N237SH · Urocop EC130T2 · Electrical Power System Wiring
  > FAULT PRESENTED IN FLIGHT FL1 FAIL OVERLIMIT DETECTED, FAILURE DETECTED MSG, THIS OCCURRED ON THE WAY TO PICK UP PATIENT FROM NEARBY HOSPITAL AND PILOT RETURNED TO BASE AND MADE WRITEUP IN LOGBOOK. THIS MALFUNCTION WAS IDENIFIED ON THE LEG WITH NO PATIENT ON B
- [SDR 2024F00106](https://openairdocs.org/sdr/2024F00106.md): Servo · unknown · Mar 30, 2024 · N43VP · Snias AS350B3 · Hydraulic System, Main
  > WHEN DOING HYDRAULICS OFF TRAINING, ON LANDING THE HYDRAULICS WERE TURNED BACK ON AND THE CYCLIC "MOTORED" TO THE LEFT.
- [SDR QMLA2023100520082](https://openairdocs.org/sdr/QMLA2023100520082.md): Terminal · broken · Oct 2, 2023 · N245AM · Urocop EC130B4 · Electrical Power System Wiring
  > IN CRUISE FLIGHT DURING PATIENT TRANSPORT ALL AVIONICS TURNED OFF. A PRECAUTIONARY LANDING WAS PERFORMED AT A SOCCER FIELD IN LOVELESS PARK. CORRECTIVE ACTION:RING TERMINAL BROKE OFF OF POSITIVE TREMINAL ON ACFT BATTERY POST. ELECTICAL POWER LOSS ON XPONDER,
- [SDR 2023F00279](https://openairdocs.org/sdr/2023F00279.md): Friction Pad · faulty · Sep 18, 2023 · N350HF · Snias AS350B3 · Rotorcraft Flight Control
  > THE FRICTION SHOE/PAD CAME UNBONDED IN FLIGHT CAUSING A "JAM" IN THE COLLECTIVE. WHEN THE PILOT LOOKED DOWN AND SAW WHAT WAS FOULING THE COLLECTIVE HE WAS ABLE TO REMOVE THE FRICTION SHOE.
- [SDR 2022FA0000184](https://openairdocs.org/sdr/2022FA0000184.md): Hose · loose · Mar 29, 2022 · N544AS · Snias AS350B3 · Fuel Storage
  > DURING A TRAINING FLIGHT, THE FUEL PRESSURE CAUTION LIGHT ILLUMINATED. THE PILOT IMMEDIATELY TURNED ON THE FUEL PUMP AND PERFORMED A PRECAUTIONARY LANDING. AFTER SHUTDOWN, FUEL WAS OBSERVED ON THE FUSELAGE. SUBSEQUENT EXAMINATION BY A MECHANIC REVEALED A LO
- [SDR 2020F00259](https://openairdocs.org/sdr/2020F00259.md): Solenoid · loose · Jan 10, 2020 · N98TE · Snias AS350B3 · Engine Controls
  > PILOT WAS CONDUCTING ENGINE GOVERNING FAILURE TRAINING IN AN AS350B3 W/2B ENGINE. DURING TRAINING PILOT SWITCHED GOVERNOR SWITCH FROM AUTO TO MANUAL. PILOT THEN ATTEMPTED TO ROLL TWIST GRIP TO INCREASE ENGINE SPEED. PILOT WAS NOT ABLE TO ADVANCE TWIST GRIP
- [SDR QMLA2019111119084](https://openairdocs.org/sdr/QMLA2019111119084.md): Structure · cracked · Nov 11, 2019 · N396LG · Snias AS350B3 · Rotorcraft Tail Boom
  > DURING A 600 HOUR INSPECTION, THE MECHANIC FOUND 4 CRACKS UNDER THE DEVORE LIGHT DOUBLER ON THE TOP RIGHT HAND SIDE OF THE HORIZONTAL STABILIZER. *** THIS AIRCRAFT REMAINS OUT OF SERVICE AT THE TIME OF THIS SUBMISSION ***
- [SDR QMLA2019111019083](https://openairdocs.org/sdr/QMLA2019111019083.md): Bolt · loose · Nov 10, 2019 · N396LG · Snias AS350B3 · Rotorcraft Tail Boom
  > DURING 600 HOUR INSPECTION, FOUND TORQUE LOSS ON UPPER VERTICAL FIN BOLTS WHERE IT ATTACHES TO THE TAILBOOM. REMOVED UPPER AND LOWER FIN ASSY.FOUND THAT DOUBLER HOLDING NUT PLATES IS WORKING AGAINST TAILBOOM RING FRAME. HEARD A POPPING CRACKLING SOUND FROM UPP
- [SDR QMLA2019083091973](https://openairdocs.org/sdr/QMLA2019083091973.md): Air Filter · overserviced · Aug 29, 2019 · N108LN · Snias AS350B3 · Turbine Engine Oil System
  > A PRECAUTIONARY LANDING WAS MADE AFTER AN UNIDENTIFIED ODOR CAME INTO THE CABIN FROM THE ENGINE COMPARTMENT. IT WAS THEN DISCOVERED THAT THE AIR FILTER WAS OVERSERVICED AND THE OIL WAS DRIPPING ONTO THE HOT ENGINE. THE ENGINE WAS CLEANED AND THE EXCESS OIL WAS
- [SDR CA190603014](https://openairdocs.org/sdr/CA190603014.md): Servo · leaking · May 30, 2019 · Snias AS350B3 · Rotorcraft Servo System
  > (CAN) HYRAULIC SERVO STARTED LEAKING BEYOND LIMITS AND WAS REMOVED FOR REPAIR AND REPLACED WITH OVERHAULED UNIT. NOR FURTHER ACTION REQUIRED. (TC# 20190603014)
- [SDR QMLA2019012319014](https://openairdocs.org/sdr/QMLA2019012319014.md): Engine · fluid loss · Jan 23, 2019 · N5230J · Snias AS350B3 · Engine (Turbine/Turboprop)
  > JUST PRIOR TO A POST MAINTENANCE ROC CHECK FLIGHT, THE ENGINE OIL TANK CAP AND OIL LEVEL WAS VERIFIED BEFORE FLIGHT. DURING THE FLIGHT, THE ENGINE OIL PRESSURE LIGHT ILLUMINATED. THE PILOT RETURNED TO THE BASE/AIRPORT. UPON A POST INSPECTION, THERE WAS NO OIL
- [SDR QMLA2019010119001](https://openairdocs.org/sdr/QMLA2019010119001.md): Filter · contaminated · Jan 1, 2019 · N103LN · Snias AS350B3 · Engine Air Intake System
  > TWO MINUTES INTO AN INTER-FACILTY FLIGHT, AND AS THE PILOT AND CREW WERE APPROACHING AIRPORT WHEN THE LOW INLET PRESSURE LIGHT ILLUMINATED. THE PILOT OPENED THE BYPASS DOORS AND DIVERTED TO THE AIRPORT. UPON LANDING, THE PILOT INSPECTED THE INLET FILTER AND SA
- [SDR QMLA2018111218121](https://openairdocs.org/sdr/QMLA2018111218121.md): Float Switch · failed · Nov 10, 2018 · N397LG · Snias AS350B3 · Fuel Indicating System
  > UPON LANDING, THE "FUEL" CAUTION ILLUMINATED WITH 51 GALLONS INDICATED. THE MECHANIC ARRIVED AND DETERMINED THAT THE LOW FUEL FLOAT SWITCH WAS THE SOURCE OF THE FAILURE. THIS AIRCRAFT REMAINS OOS AT THIS TIME TO REPLACE THIS SWITCH AS WELL AS PERFORM OTHER SCH
- [SDR QMLA2018101218111](https://openairdocs.org/sdr/QMLA2018101218111.md): Brake Assy · damaged · Oct 9, 2018 · N397LG · Snias AS350B3 · Main Rotor Brake
  > UPON DISASSEMBLY OF ROTOR BRAKE. BRAKE ASSEMBLY DRIVE FLANGE AND HYDRAULIC DRIVE COUPLING HAD EXTREME HEAT DAMAGE AND METAL TRANSFER. THE DAMAGE CONTAINED TO THESE ITEMS PARTS WERE ORDERED AND REPLACED GROUND RUN MOC CHECKS COMPLETED AND AIRCRAFT RETURNED TO S
- [SDR QMLA2017100717109](https://openairdocs.org/sdr/QMLA2017100717109.md): Generator · failed · Oct 14, 2017 · N350MV · Snias AS350B3 · AC Generator-Alternator
  > ENROUTE, THE GENERATOR LIGHT ILLUMINATED. DIMMING OF COCKPIT INSTRUMENTATION, AND YELLOW HIGHLIGHTED VOLTAGE INDICATOR. ATTEMPTED TO RESET THE GENERATOR ONCE, WHICH FAULTED AGAIN. RESET THE GENERATOR A SECOND TIME, WHICH SUCCESSFULLY BROUGHT THE GENERATO
- [SDR QMLA2017081117080](https://openairdocs.org/sdr/QMLA2017081117080.md): Module · seized · Aug 11, 2017 · N913LH · Urocop EC135T2 · Engine (Turbine/Turboprop)
  > DURING GROUND RUN CHECKS ON AIRCRAFT FOLLOWING AN ENGINE MODULE CHANGE, AN ENGINE FIRE OCCURRED AFTER ENGINE SHUTDOWN. FIRE MASTER CAUTION WAS ILLUMINATED AFTER SHUTDOWN THAT THE PILOT AND MECHANIC TO SHUT DOWN THE NR 2 ENGINE. POST INCIDENT INSPECTION REVEA
- [SDR O4VA20170626003](https://openairdocs.org/sdr/O4VA20170626003.md): Fadec · failed · Jun 24, 2017 · N98TE · Snias AS350B3 · Fuel Controlling System
  > AFTER LANDING, A RED GOV LIGHT ILLUMINATED ON THE CAUTION AND WARNING PANEL INDICATING A MAJOR FADEC FAILURE.
- [SDR 2017FA0000321](https://openairdocs.org/sdr/2017FA0000321.md): Bearing · seized · Jun 17, 2017 · N354SH · Snias AS350B3 · Reciprocating Engine Power Section
  > THE HELICOPTER WAS CONDUCTING A SNOW SURVEY, AT APPROXIMATELY 11,500FT, AN ENGINE CHIP LIGHT ILLUMINATED ON THE CAUTION PANEL OF THE ACFT RIGHT AFTER TAKEOFF. THE PILOT IMMEDIATELY LANDED AND PROCEED TO INSPECT THE MAGNETIC ENGINE CHIP PLUGS WHICH WERE FOUND
- [SDR 2017FA0000338](https://openairdocs.org/sdr/2017FA0000338.md): Bearing · seized · Jan 26, 2017 · N354SH · Snias AS350B3 · Engine (Turbine/Turboprop)
  > APPROXIMATELY 3PM LOCAL TIME, CONDUCTING A SNOW SURVEY AT APPROXIMATELY 11500 FT. AN ENGINE CHIP LIGHT ILLUMINATED ON THE CAUTION PANEL OF THE ACFT RIGHT AFTER TAKEOFF. THE PILOT IMMEDIATELY LANDED AND PROCEEDED TO INSPECT THE MAGNETIC ENGINE CHIP PLUGS WHIC
- [SDR 2016FA0000485](https://openairdocs.org/sdr/2016FA0000485.md): Mixing Unit · misinstalled · Oct 11, 2016 · N853BP · Snias AS350B3 · Main Rotor Control
  > MAIN ROTOR FLIGHT CONTROL MIXING UNIT HAS BLIND RIVET FASTENERS IN USE WHERE THE ANTICIPATOR CONTROL ARM ATTACHES THE MIXING UNIT.
- [SDR QMLA2016092016106](https://openairdocs.org/sdr/QMLA2016092016106.md): Hose · cracked · Sep 20, 2016 · N439AE · Snias AS350B3 · Cabin Compressor System
  > ENROUTE THE CREW NOTICE SMOKE IN CABIN AREA PILOT FOLLOWED EMERGENCY PROCEDURES OPENED FRESH AIR VENTS AND WINDOWS NOTIFIED AIR COMM OVER RADIO FOUND SUITABLE LANDING AREA IN PASTURE S.E. OF PERKINS OK. AFTER SHUT DOWN CALLED AIR COMM VIA MOBLE PHONE WHICH NO
- [SDR QMLA2016072016083](https://openairdocs.org/sdr/QMLA2016072016083.md): Indication Sys · failed · Jul 20, 2016 · N392LG · Snias AS350B3 · Engine Indicating System
  > VEMD LANE 1 FAILED IN FLIGHT.
- [SDR HDNA 20160609959](https://openairdocs.org/sdr/HDNA%2020160609959.md): Drive Belt · broken · Jun 7, 2016 · N911MT · Snias AS350B3 · Hydraulic System, Main
  > DURING STRAIGHT AND LEVEL FLIGHT, ACFT EXPERIENCED A COMPLETE HYDRAULIC FAILURE, FOLLOWED BY THE HYDRAULIC LIGHT.. EMERGENCY PROCEDURE WAS FOLLOWED IAW THE CHECK LIST AND ACFT WAS SAFELY LANDED WITH NO FURTHER DAMAGE. DURING POST FLIGHT, HYDRAULIC BELT WAS F
- [SDR QMLA2016053016057](https://openairdocs.org/sdr/QMLA2016053016057.md): Control Box · defective · May 30, 2016 · N103LN · Snias AS350B3 · Central Warning
  > AFTER TAKEOFF, PILOT NOTICED THAT THE TOP VEMD SCREEN HAD REVERTED BACK FROM THE STANDARD FLI IN FLIGHT SCREEN TO THE 3 PARAMETERS SCREEN & HAD A FLI FAILURE IN YELLOW ON THE INFO BLOCK. NO OTHER CAUTIONS & WARNINGS WERE NOTED OR PRESENT. PILOT ABORTED FLIGH
- [SDR QMLA2016052616055](https://openairdocs.org/sdr/QMLA2016052616055.md): Connector · dirty · May 26, 2016 · N103LN · Snias AS350B3 · Instrument System Wiring
  > AFTER TAKEOFF, THE PILOT NOTICED THAT THE TOP OF THE VEMD SCREEN HAD REVERTED BACK FROM THE STANDARD FLI IN FLIGHT SCREEN TO THE 3 PARAMETERS SCREEN & HAD A FLI FAILURE IN YELLOW ON THE INFORMATION BLOCK OF THE SCREEN. ABORTED FLIGHT & LANDED SAFELY & ONLY WHE
- [SDR QMLA2016041316040](https://openairdocs.org/sdr/QMLA2016041316040.md): Unknown · malfunctioned · Apr 13, 2016 · N392LG · Snias AS350B3 · Electrical Power System
  > WHILE EN-ROUTE, THE ACFT EXPERIENCED A MOMENTARY COMPLETE LOSS OF ELEC POWER THAT LASTED ABOUT 2 SECONDS, THEN RETURNED TO NORMAL WITH AN AMBER GOV LIGHT ILLUMINATED. WE RETURNED TO BASE FOLLOWING THE EMER PROCEDURE FOR AN AMBER GOV LIGHT & LANDED WITHOUT INC
- [SDR QMLA2016041216039](https://openairdocs.org/sdr/QMLA2016041216039.md): Skin · cracked · Apr 12, 2016 · N433AE · Snias AS350B3 · Rotorcraft Tail Boom
  > DURING ROUTINE MX, THERE WAS A CRACK DISCOVERED ON THE HORIZONTAL STABILIZER. IT IS ON THE TE OF THE RT SIDE OF THE STABILIZER. THAT SECTION OF THE STABILIZER IS A SINGLE SKIN WITH NO DOUBLED OR BACKUP SUPPORT.
- [SDR CA160309003](https://openairdocs.org/sdr/CA160309003.md): Actuator · failed · Mar 8, 2016 · Snias AS350B3 · Engine Air Intake System
  > (CAN) INTAKE AIR BYPASS DOORS FAILED TO OPEN DURING A DAILY INSPECTION. REPLACED THE ACTUATOR, PART OF STC SR00811SE.
- [SDR CA151120009](https://openairdocs.org/sdr/CA151120009.md): Linkage · worn · Nov 19, 2015 · Snias AS350B3 · Hydraulic System, Main
  > (CAN) WHILE DOING A TEE INSPECTION, HAD TO DISCONNECT THE INPUT LINKAGE TO THE M/R ROTOR SERVOS TO ACCOMPLISH A TASK. THEN NOTICED THAT THE BOLT THAT GOES TO THE PILOT VALVE WAS SMOKING. WHICH IN COMPARISON WITH THE OTHER TWO M/R SERVO`S THE AFFECTED BOLT WA
- [SDR CA151202006](https://openairdocs.org/sdr/CA151202006.md): Deck Plate · cracked · Oct 26, 2015 · Snias AS350B3 · Fuselage Main, Structure
  > (CAN) WHILE PERFORMING A 4T INSPECTION, THE ENGINE WAS REMOVED FOR MAINTENANCE. CLEANING THE ENGINE DECK A SMALL CRACK WAS NOTED EMANATING FROM A RIVET. ACFT MFG WAS CONTACTED AND WE WERE ISSUED A REPAIR DESIGN APPROVAL SHEET AND A PATCH WAS PLACED OVER THE
- [SDR CA151217011](https://openairdocs.org/sdr/CA151217011.md): Bearing · rough · Oct 26, 2015 · Snias AS350B3 · Hydraulic Pump (Electric/Engine), Main
  > (CAN) AT AIRFRAME HRS 10363.6, PUMP SUPPORT ASSY WAS INSTALLED TO UPGRADE THE ACFT TO POST MOD 079568 STATUS. PRIOR TO INSTALLATION THE BEARING WAS INSPECTED AND GREASED TO ENSURE IT WAS FIT FOR SERVICE. NOTED THAT DURING THE TACTILE CHECK IT FELT ROUGH.
- [SDR CA150828012](https://openairdocs.org/sdr/CA150828012.md): Lock · malfunctioned · Aug 27, 2015 · Snias AS350B3 · Power Lever
  > (CAN) A GROUND RUN WAS BEING PERFORMED FOR ROUTINE MAINTENANCE FOR THE FUNCTIONAL CHECK IN MIXED MODE OF THE FUEL CONTROL UNIT. DURING THE SECOND STAGE OF THE CHECK WHEN THE MANUAL TWIST GRIP WAS BEING RETURNED TO THE FLIGHT DETENT IN ONE SECOND, THE DETENT W
- [SDR CA150803008](https://openairdocs.org/sdr/CA150803008.md): Chip Detector · damaged · Aug 2, 2015 · Snias AS350B3 · Turbine Engine Oil System
  > (CAN) A FRESHLY O/H ENGINE WAS INSTALLED INTO ACFT OVER THE WEEKEND. STARTED IT UP FOR THE FIRST GROUND RUN/LEAK CHECK. THE RUN WENT FINE, SHUTDOWN AND CHECKED ALL THE CHIP PLUGS FOR METAL. THE NON-WIRED MODULE 1 CHIP PLUG WAS REMOVED AND NOTICED TO BE CO
- [SDR CA150619015](https://openairdocs.org/sdr/CA150619015.md): Skin · cracked · Jun 17, 2015 · Snias AS350B3 · Vertical Stabilizer, Plate/Skin
  > (CAN) VISUAL INSPECTION WITH A FLASHLIGHT ABOVE THE TAIL CONE & AT THE LOWEST RIVET ROW OF THE FIN, THE AFT RT TOE CAP RIVET SHOP HEAD WAS MISSING. FIN ASSEMBLY REMOVED FROM ACFT & FURTHER INSPECTION REVEALED THE TWO OTHER RT TOE CAP RIVETS FWD OF THE SUSPECT
- [SDR 2015FA0000274](https://openairdocs.org/sdr/2015FA0000274.md): Freq Adapter · cracked · Jun 16, 2015 · N850BP · Snias AS350B3 · Main Rotor Head
  > THE FREQUENCY ADAPTER ON THE YELLOW SLEEVE ASSEMBLY WAS FOUND WITH A 14MM CRACK DOWN THE L/E SIDE OF THE UNIT, 10MM IS THE LIMIT.
- [SDR CA150604018](https://openairdocs.org/sdr/CA150604018.md): Tape · unsecure · Jun 2, 2015 · Snias AS350B3 · Main Rotor Mast/Swashplate
  > (CAN) WHILE DOING A DAILY INSPECTION, NOTICED A PIECE OF THE SWASHPLATE GUIDE TAPE STICKING OUT FROM UNDER THE UNIBALL AND A LOT BLACK MATERIAL ON THE SWASHPLATE AND SCISSOR LINK. AFTER INVESTIGATING IT WAS DETERMINED THAT THE PTFE TAPE ON THE SWASHPLATE GUID
- [SDR CA150601013](https://openairdocs.org/sdr/CA150601013.md): Cell · mismanufactured · Jun 1, 2015 · Snias AS350B3 · Battery/Charger System
  > (CAN) THE CELL WAS POORLY MANUFACTURED WITH THE CELL CAP WITH POLARITY MARKINGS WERE INSTALLED BACKWARDS. LEADING TO A MUCH HIGHER PROBABILITY OF THE CELL BEING INSTALLED IN THE BATTERY ASSY IN REVERSE.
- [SDR QMLA2015032315020](https://openairdocs.org/sdr/QMLA2015032315020.md): Audio Panel · faulty · Mar 23, 2015 · N150AE · Snias AS350B3 · Audio Integrating System
  > DURING CRUISE, PILOT REPORTED HEARING THE AUDIBLE GONG FOR THE FIRE WARNING SYS WITH NO OTHER INDICATION. TROUBLE SHOT SYS. REPLACED PILOTS AUDIO BOX. SYS OPERATED NORMAL ON GND. PERFORMED APPROX 30 MIN TEST FLIGHT. NO DEFECTS NOTED. ACFT RETURNED TO SER
- [SDR QMLA2015031815018](https://openairdocs.org/sdr/QMLA2015031815018.md): Starter Gen · damaged · Mar 18, 2015 · N54178 · Aerosp AS355* · Starter-Generator
  > WHILE ACFT WAS IN FLIGHT WITH A PATIENT ABOARD, PILOT NOTICED A GRADUAL LOSS OF VOLTAGE & AMPERAGE. AFTER SHEDDING SECONDARY ELEC EQUIP, VOLTAGE & AMPERAGE CONTINUED TO DECREASE WHILE A GEN LIGHT ILLUMINATED DURING FINAL DESCENT ON TO A MALL PARKING LOT. REM
- [SDR CA150330010](https://openairdocs.org/sdr/CA150330010.md): Bracket · cracked · Mar 17, 2015 · Snias AS350* · Tail Rotor Drive Shaft
  > (CAN) FOLLOWING AN INSPECTION, FOUND TWO CRACKS ON THE FWD TAIL ROTOR DRIVE SHAFT BRACKET BETWEEN THE SHORT AND LONG SHAFT. THE FLANGE WAS FOUND TO HAVE PLAY DUE TO THE NUT BEING LOOSE AND WAS MOST LIKELY THE CAUSE FOR THE BRACKET CRACKING DUE TO EXCESSIVE VI
- [SDR CA150211001](https://openairdocs.org/sdr/CA150211001.md): Wire Harness · chafed · Feb 6, 2015 · Snias AS350B3 · Light System Wiring
  > (CAN) POSITION STROBE LIGHT WIRE HARNESS FOUND CHAFED AT TAILBOOM JUNCTION. 3 STRANDS OF OF CONDUCTOR WERE FOUND DAMAGED BY RUBBING ON THE STABILIZER. THE HARNESS IS PART OF THE OEM INSTALLATION FOR STROBE LIGHTS ON THE HORIZONTAL STABILIZER IAW SB 33.90.30.
- [SDR CA141107001](https://openairdocs.org/sdr/CA141107001.md): Wire · burned · Nov 5, 2014 · Snias AS350B3 · Exterior Lighting
  > (CAN) WEDNESDAY MORNING THE HELICOPTER WAS GETTING READY FOR A FLIGHT, DURING A LIGHT CHECK, NOTICED THAT THE RT STROBE LIGHT WAS BURNED. PROCEEDED TO REPLACE THE STROBE TUBE AND NOTICED THAT THE WIRES WERE SHORTED AND BURNED, AFTER A QUICK INSPECTION OF THE
- [SDR QMLA2014102114123](https://openairdocs.org/sdr/QMLA2014102114123.md): Circuit Card · unserviceable · Oct 21, 2014 · N904CF · Snias AS350B3 · DC Regulator
  > GENERATOR ADVISER LIGHT ILLUMINATED WITH DECLINING VOLTAGE. Z1 VOLTAGE REGULATOR CARD REMOVED, TIME SINCE REPAIR 10HRS 55MIN. INSTALLED SERVICEABLE CARD FUNCTION CHECKED GOOD.
- [SDR CA140924008](https://openairdocs.org/sdr/CA140924008.md): Extinguisher · unserviceable · Sep 23, 2014 · Snias AS350B3 · Fire Bottle, Portable
  > (CAN) WHILE PERFORMING A SCHEDULED INSPECTION ON ACFT, HAPPENED TO REMOVE THE CABIN FIRE EXTINGUISHER AND NOTICED A LOUD RATTLE COMING FROM INSIDE THE FIRE EXTINGUISHER. ORDERED A NEW ONE AND ONCE I RECEIVED IT, DISASSEMBLED THE OLD ONE AND FOUND THE STANDPIPE
- [SDR 2014FA0000610](https://openairdocs.org/sdr/2014FA0000610.md): Servo · binding · Sep 19, 2014 · N708HP · Snias AS350B3 · Rotorcraft Flight Control
  > OVERHAULED SERVO INSTALLED FOR REPLACEMENT. PILOT REPORTED SLIGHT BINDING, NOT OPERATING SMOOTHLY, OF THE CYCLIC CONTROLS AFTER.8 HRS OF OPERATION WHEN COLLECTIVE "UP" INPUTS APPLIED. CYCLIC CONTROLS REACTED WITH FORWARD MOVEMENT. WHEN COLLECTIVE CONTROL M
- [SDR QMLA2014072614090](https://openairdocs.org/sdr/QMLA2014072614090.md): Unknown · odor · Jul 26, 2014 · N133LN · Urocop EC130B4 · Air Distribution System
  > FOLLOWING DEPARTURE CREW NOTED STRONG ELEC SMELL IN CABIN. AIR CONDITIONER SWITCHED OFF WHILE SIMULTANEOUSLY ABORTING TAKEOFF & RETURNING TO BASE. ELEC SMELL DISSIPATED. ACFT SHUTDOWN & CHECKED EXTENSIVELY FOR SOURCE BY PILOT & MECHANIC. NO SOURCE IDENTIFI
- [SDR QMLA2014072614092](https://openairdocs.org/sdr/QMLA2014072614092.md): Battery · unserviceable · Jul 26, 2014 · N4204 · Snias AS350B3 · Battery/Charger System
  > THE RADIOS & VEMD WENT OFF LINE & HE COULD SMELL SMOKE. REMOVED INSTRUMENT PANEL HOOD & INSPECTED THE WIRING FOR THE RADIOS & VEMD FOUND NO DISCREPANCIES. REMOVED THE 30 ALPHA PANEL & INSPECTED WIRING NO DISCREPANCIES. INSPECTED 31 ALPHA PANEL WHICH HOUSES
- [SDR HCM2014F00000](https://openairdocs.org/sdr/HCM2014F00000.md): Engine · making metal · May 2, 2014 · N11FQ · Urocop EC130T2 · Engine (Turbine/Turboprop)
  > DURING FLIGHT, ENGINE CHIP LIGHT ILLUMINATED AND PILOT MADE A PRECAUTIONARY LANDING. MECHANIC INSPECTED ENGINE CHIP PLUGS. A SIGNIFICANT AMOUNT OF METAL WAS FOUND ON THE ELECTRIC PLUG, MODULE 01 CHIP PLUG AND THE ENGINE OIL TANK CHIP PLUG. IT WAS DETERMINE
- [SDR QMLA2014042814044](https://openairdocs.org/sdr/QMLA2014042814044.md): Compressor · failed · Apr 28, 2014 · N904CF · Urocop AS365N3 · Cabin Cooling System
  > BURNING SMELL & SMOKE IN THE CABIN. AIR CONDITIONING & FAN TURNED OFF & IT SUBSIDED. AIR CONDITIONER COMPRESSOR INTERNAL FAILURE.

Next page: https://openairdocs.org/engine/turbomeca-arriel-2b/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 engine_model_key = 'ARRIEL2B'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/turbomeca-arriel-2b/reports

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