# Turbomeca ARRIUS-2B1

- Type: Engine model (FAA registry)
- Registry code: 60015
- Manufacturer (registry): TURBOMECA
- Model: ARRIUS 2B1
- Engine type: Turbo-shaft
- Power: 577 hp
- Data sheet: [TCDS E34NE](https://openairdocs.org/tcds/E34NE) (OpenAirDocs)
- Holder: Safran Helicopter Engines S.A.
- Installed in: 13 registered aircraft
- Page: https://openairdocs.org/engine/turbomeca-arrius-2b1

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2021-26-26](https://openairdocs.org/ad/2021-26-26): Engine Controls · Safran Helicopter Engines Arrius 2B1, Arrius 2B1A and Arrius 2B2. Effective Feb 23, 2022
- [AD 2021-17-05](https://openairdocs.org/ad/2021-17-05): Fuel Controlling System · Safran Helicopter Engines Arrius 2B1, Arrius 2B1A, Arrius 2B2 and 1 more. Effective Oct 12, 2021
- [AD 2018-12-03](https://openairdocs.org/ad/2018-12-03): Fuel Controlling System · Safran Helicopter Engines Arrius 2B1 and Arrius 2F. Effective Aug 9, 2018
- [AD 2018-07-17](https://openairdocs.org/ad/2018-07-17): Turbine Section · Safran Helicopter Engines Arrius 2B1, Arrius 2B1A, Arrius 2B2 and 1 more. Effective Apr 27, 2018
- [AD 2008-19-11](https://openairdocs.org/ad/2008-19-11): Electronic control (EEC) unit · Turbomeca Arrius 2B1, Arrius 2B1A, Arrius 2B2 and 1 more. Effective Oct 8, 2008
- [AD 2006-26-07](https://openairdocs.org/ad/2006-26-07): A simultaneous interruption of the lubrication on both engines may lead to a double non-commanded in-flight shutdown. · Turbomeca Arrius 2B1, Arrius 2B1A and Arrius 2B2. Effective Jan 18, 2007
- [AD 2003-19-06](https://openairdocs.org/ad/2003-19-06): Gas generator high pressure (HP) turbine disk · Turbomeca Arrius 2B1, Arrius 2B1A and Arrius 2K1. Effective Oct 22, 2003

Historical (superseded or no longer in force):

- [AD 2014-04-06](https://openairdocs.org/ad/2014-04-06) (historical): Hydro-mechanical metering unit (HMU) · Turbomeca Arrius 2B1, Arrius 2B1A, Arrius 2B2 and 1 more. Effective Mar 31, 2014
- [AD 2013-11-09](https://openairdocs.org/ad/2013-11-09) (historical): Fuel injection manifolds and the privilege injector · Turbomeca Arrius 2B1 and Arrius 2F. Effective Jul 5, 2013
- [AD 2001-08-14 R1](https://openairdocs.org/ad/2001-08-14-R1) (historical): Right injector half manifold and left injector half manifold · Turbomeca Arrius 2B, Arrius 2B1 and Arrius 2F. Effective Feb 23, 2006
- [AD 2005-12-08](https://openairdocs.org/ad/2005-12-08) (historical): Engine Electronic Control Unit (EECU) · Turbomeca Arrius 2B1, Arrius 2B1A and Arrius 2B2. Effective Jun 29, 2005
- [AD 2001-08-14](https://openairdocs.org/ad/2001-08-14) (historical): Fuel Injector Manifold · Turbomeca Arrius 2B, Arrius 2B1 and Arrius 2F. Effective May 31, 2001

## Registered aircraft (13)

- [N109BC](https://openairdocs.org/aircraft/N109BC): [Broward County Sheriffs Office](https://openairdocs.org/faa-owner/BROWARD%20COUNTY%20SHERIFFS%20OFFICE), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), built 1999, S/N 0139
- [N122TH](https://openairdocs.org/aircraft/N122TH): [Mwn Holdings LLC](https://openairdocs.org/faa-owner/MWN%20HOLDINGS%20LLC), [Saint Louis, MO](https://openairdocs.org/faa-place/MO/Saint%20Louis), built 1998, S/N 1017
- [N123RT](https://openairdocs.org/aircraft/N123RT): [Mather Air LLC](https://openairdocs.org/faa-owner/MATHER%20AIR%20LLC), [Paris, KY](https://openairdocs.org/faa-place/KY/Paris), built 2004, S/N 3841
- [N356MP](https://openairdocs.org/aircraft/N356MP): [Altair Helicopter Service LLC](https://openairdocs.org/faa-owner/ALTAIR%20HELICOPTER%20SERVICE%20LLC), [Marshfield, MA](https://openairdocs.org/faa-place/MA/Marshfield), built 2000, S/N 0163
- [N60ZX](https://openairdocs.org/aircraft/N60ZX): [Tonik Air LLC](https://openairdocs.org/faa-owner/TONIK%20AIR%20LLC), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), built 1998, S/N 0039
- [N802MH](https://openairdocs.org/aircraft/N802MH): [World Trade Enterprises LLC](https://openairdocs.org/faa-owner/WORLD%20TRADE%20ENTERPRISES%20LLC), [Lucas, TX](https://openairdocs.org/faa-place/TX/Lucas), built 2003, S/N 3707
- [N891T](https://openairdocs.org/aircraft/N891T): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1998, S/N 0051
- [N892T](https://openairdocs.org/aircraft/N892T): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1998, S/N 0052
- [N89EM](https://openairdocs.org/aircraft/N89EM): [Integra Aviation LLC](https://openairdocs.org/faa-owner/INTEGRA%20AVIATION%20LLC), [Amarillo, TX](https://openairdocs.org/faa-place/TX/Amarillo), built 1998, S/N 0049
- [N911XA](https://openairdocs.org/aircraft/N911XA): [Air Med Services LLC](https://openairdocs.org/faa-owner/AIR%20MED%20SERVICES%20LLC), [Lafayette, LA](https://openairdocs.org/faa-place/LA/Lafayette), built 2000, S/N 0132
- [N911XB](https://openairdocs.org/aircraft/N911XB): [Air Med Services LLC](https://openairdocs.org/faa-owner/AIR%20MED%20SERVICES%20LLC), [Lafayette, LA](https://openairdocs.org/faa-place/LA/Lafayette), built 2000, S/N 0154
- [N911XG](https://openairdocs.org/aircraft/N911XG): [Air Med Services LLC](https://openairdocs.org/faa-owner/AIR%20MED%20SERVICES%20LLC), [Lafayette, LA](https://openairdocs.org/faa-place/LA/Lafayette), built 2000, S/N 0157
- [N911ZG](https://openairdocs.org/aircraft/N911ZG): [Guardian Flight Holdings Inc](https://openairdocs.org/faa-owner/GUARDIAN%20FLIGHT%20HOLDINGS%20INC), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 2001, S/N 0164

## NTSB investigations (4)

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 ERA23FA352](https://openairdocs.org/ntsb/ERA23FA352), Aug 28, 2023: Eurocopter EC135 (N109BC), Pompano Beach, FL, destroyed, 2 fatal. Probable cause: An inflight fire outside of the engine firewalls, likely from overheating of the No. 1 engine for undetermined reasons, which resulted in a partial tailboom separation.
- [NTSB WPR10FA133](https://openairdocs.org/ntsb/WPR10FA133), Feb 14, 2010: Eurocopter EC135 (N127TS), Cave Creek, AZ, substantial damage, 5 fatal. Probable cause: The sudden and inadvertent lowering of the collective to near the lower stop, followed by a simultaneous movement of the collective back up and the cyclic control to a nearly full-aft position, which…
- [NTSB WPR10CA028](https://openairdocs.org/ntsb/WPR10CA028), Oct 22, 2009: Eurocopter AS 350 B3 (N105LN), Marana, AZ, substantial damage. Probable cause: The improper use of the throttle by the pilot receiving instruction, and the check pilot's inadequate supervision and delayed remedial action, which resulted in the collision with terrain.
- [NTSB FTW99LA085](https://openairdocs.org/ntsb/FTW99LA085), Feb 26, 1999: Eurocopter Colibri EC120B (N122TH), Springtown, TX, substantial damage. Probable cause: The improper touchdown executed by the pilot. Factors were the tail wind condition, and the manufacturer's inadequate design of the P3 pipe supports, which resulted in a fatigue fracture of the P3…

## FAA accident and incident reports (4)

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.

- [Accident 20230828022749A](https://openairdocs.org/incident/20230828022749A), Aug 28, 2023: Eurocopter Deutschland Gmbh EC135T1 (N109BC), Pompano Beach, FL, Destroyed, 2 fatal. A Eurocopter Deutschland Gmbh EC135T1, N109BC, was destroyed when it was involved in an accident near Pompano Beach, Florida. The commercial pilot sustained…
- [Accident 20100214027809A](https://openairdocs.org/incident/20100214027809A), Feb 14, 2010: Eurocopter EC135T1 (N127TS), Cave Creek, AZ, Destroyed, 5 fatal. On February 14, 2010, @ approx. 1505 mountain standard time, a Eurocopter EC135 T1, N127TS, a twin engine turbine powered helicopter, was destroyed following a…
- [Accident 20091022022229A](https://openairdocs.org/incident/20091022022229A), Oct 22, 2009: Snias AS350B3 (N105LN), Tucson, AZ, Substantial damage. Mr. Teeb was giving [privacy data omitted] a check ride following an accident [privacy data omitted] had in September, 2009. After 30 minutes of maneuvers, Mr.…
- [Accident 19990226001789A](https://openairdocs.org/incident/19990226001789A), Feb 26, 1999: Urocop EC120B (N122TH), Springtown, TX, Substantial damage. Eurocopter colibri EC-120B helicopter was on a ferry flight when it made an emergency landing in a field for unknown reasons and rolled over on landing, other…

## Service difficulty reports (92, newest 50)

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

- [SDR 2026F00116](https://openairdocs.org/sdr/2026F00116), May 26, 2026: ENGINE. FLAMED OUT. DURING ENROUTE PHASE OF FLIGHT, ENGINE #1 FLAMED OUT. PILOT REPORTED FUEL PRESSURE CAUTION LIGHT ILLUMINATED. PILOT UTILIZED #2 ENGINE TO PERFORM A RUN ON LANDI
- [SDR QMLA2024102120135](https://openairdocs.org/sdr/QMLA2024102120135), Oct 20, 2024: POTENTIOMETER. FAULTED. TORQUE SPLIT ON TAKE OFF. REDUCED COLLECTIVE, AND TORQUE MATCHED. TORQUE SPLIT AGAIN IN CRUISE FLIGHT. #1 TORQUE WAS 12-15% HIGHER AND FLUCTUATING. TORQUES HELD
- [SDR B1EA20231127109BC](https://openairdocs.org/sdr/B1EA20231127109BC), Aug 28, 2023: UNKNOWN. UNKNOWN. SHORTLY AFTER TAKEOFF PILOT/CREW HEARD A BANG. PILOT NOTICED #1 ENGINE TOT RISING RAPIDLY AND DETERMINED THERE WAS AN ENGINE FAILURE. PILOT TURNED THE AIRCRAFT 
- [SDR UX9R2021F00047](https://openairdocs.org/sdr/UX9R2021F00047), Jan 28, 2021: FLOOR SUPPORT. CORRODED. DISCOVERED FILIFORM CORROSION ON THE LEFT HAND OUTER CABIN FLOOR EDGE BETWEEN FUSELAGE STATION 33.30 TO 61.02. CORROSION WAS NOTICED BY VISUAL INSPECTION USING 
- [SDR QMLA02020083141](https://openairdocs.org/sdr/QMLA02020083141), Aug 28, 2020: CHIP DETECTOR. FALSE ACTIVATION. WHILE IN ROUTE BACK TO OUR BASE, THE FLIGHT MEDIC AND MYSELF NOTICED AN ENGINE CHIP LIGHT ON THE NUMBER ONE ENGINE. THE MEDIC WENT TO THE EC 135 EMERGENCY BOOK 
- [SDR CA190204014](https://openairdocs.org/sdr/CA190204014), Jan 26, 2019: ENGINE. MAKING METAL. (CAN) AFTER STARTING THE ENGINE, AND, WHILE THE PILOT WAS SELECTING THE `FLIGHT` MODE, HE NOTICED THAT THE `ENGINE CD 1 INOP: MESSAGE WAS DISPLAYED ON THE AVION
- [SDR 2019F00052](https://openairdocs.org/sdr/2019F00052), Aug 14, 2018: UNKNOWN. ODOR. CREW IN CABIN AREA REPORTED ELECTRICAL BURNING ODOR NEAR THE MED AVIONICS PANEL, COINCIDING WITH ATTEMPTING TO TRANSMIT ON THE AUX SELECTOR. REMOVED RADIOS FROM
- [SDR CCHA20180608001](https://openairdocs.org/sdr/CCHA20180608001), May 21, 2018: ENGINE. FAILED. PILOT HEARD A LOUD BANG COMING FROM THE NR 1 ENGINE AND FELT A SLIGHT YAW. THE NR 1 ENG CHIP, NR 1 ENG FAIL AND NR 1 ENG FIRE CAUTION LIGHTS ILLUMINATED. PILOT 
- [SDR CA180530013](https://openairdocs.org/sdr/CA180530013), May 17, 2018: BEARING. LOOSE. (CAN) THE FOLLOWING WAS REPORTED TO BELL: ONE OF THE SPHERICAL BEARINGS WAS LOOSE AND HAD SPUN IN THE HORN OF THE INNER RING. THE SAME SWASHPLATE ASSEMBLY WAS A
- [SDR HDNA20170323016](https://openairdocs.org/sdr/HDNA20170323016), Mar 23, 2017: ENGINE. FAILED. CREW HEARD A POP WITH SMALL YAW MOVEMENT. ENGINE CHIP INDICATION. UPON INSPECTION AFTER LANDING FOUND MULTIPLE METAL PARTICLES ON ENGINE CHIP DETECTORS. OIL LEA
- [SDR 7AJA20170209001](https://openairdocs.org/sdr/7AJA20170209001), Jan 19, 2017: WARNING LIGHT. ILLUMINATED. NR 2 ENGINE LOW OIL PRESSURE CAUTION ANNUNCIATOR ILLUMINATED SHORTLY AFTER TAKEOFF.
- [SDR HDNA20150513004](https://openairdocs.org/sdr/HDNA20150513004), May 20, 2015: PRESSURE SENSOR. DEFECTIVE. NUMBER 2 ENG INDICTED OIL PRESS TO BE OVER LIMITS SPECIFIED. PILOT WAS FORCED TO MAKE A PRECAUTIONARY LANDING.
- [SDR QMLA2014110714130](https://openairdocs.org/sdr/QMLA2014110714130), Nov 7, 2014: UNKNOWN. ODOR. PILOT REPORTED SMELLING SOMETHING HOT IN THE COCKPIT, NO SMOKE PRESENT. INSPECTED THE ACFT, THEN THEY FLEW FOR APPROX ONE HOUR. COULD NOT DUPLICATE PROBLEM.
- [SDR HDNA2013F00138](https://openairdocs.org/sdr/HDNA2013F00138), Jun 28, 2013: EEC. SHUTDOWN. PILOT INITIATED A HOVER CLIMB TAKE OFF TO APPROX 150 FT PRIOR TO DEPARTING FROM HOSPITAL HELIPAD. AT THAT TIME, THE TORQUES STARTED TO SPLIT AND THE NR 2 ENGINE
- [SDR QMLA2012042312069](https://openairdocs.org/sdr/QMLA2012042312069), Apr 23, 2012: BELT. BROKEN. WHILE RETURNING TO BASE, EXPERIENCED A BURNING ODOR AND SMOKE IN CABIN. SMOKE CLEARED, MADE A PRECAUTIONARY LANDING. AFTER LANDING AND SHUTTING DOWN IT WAS DETE
- [SDR QMLDMG2492](https://openairdocs.org/sdr/QMLDMG2492), Aug 26, 2011: GEAR. WORN. WHILE PERFORMING AN INSP OF THE MAIN ROTOR MAST, FOUND LATERAL PLAY IN THE COLLECTOR GEAR. UPON REMOVAL OF THE MAST NUT THE LOWER MAST BEARING FELL OUT OF THE M
- [SDR QMLA2011040311044](https://openairdocs.org/sdr/QMLA2011040311044), Apr 3, 2011: SHAFT. SHEARED. DURING GROUND RUN, THE PILOT OBSERVED THE NR 1 ENGINE OIL TEMP WAS ELEVATED. UPON ARRIVING BACK TO DEPARTURE, IT WAS FOUND THAT THE LT OIL COOLER BLOWER WAS NOT
- [SDR QMLA2011021111041](https://openairdocs.org/sdr/QMLA2011021111041), Feb 11, 2011: BEARING. FAILED. DURING A GROUND RUN, THE NR 1 ENGINE CHIP LIGHT ILLUMINATED. THE MECHANIC INSPECTED THE ACFT AND FOUND CHIPS IN THE GEARBOX CHIP PLUG. THE MECHANIC CONSULTED WI
- [SDR CA090702006](https://openairdocs.org/sdr/CA090702006), Jul 1, 2009: ELECTRICAL SYS. MALFUNCTIONED. INVESTIGATION REVEALED THAT THE CAROUSEL RELAY PROVIDES AN UNANTICIPATED 6 TO 9 VOLTS VDC TO PIN C OF THE UTILITY CONNECTION ON THE BELLY OF THE AIRFRAME WHEN I
- [SDR 2008FA0000483](https://openairdocs.org/sdr/2008FA0000483), Jul 4, 2008: BELT. BROKEN. GROUND CREW NOTICED THE SMELL OF FUEL AND VAPOR COMING FROM AIRCRAFT AFTER LIFTING FROM SCENE. PIC NOTIFIED OF THE CIRCUMSTANCES. PIC MADE A PRECAUTIONARY LANDI
- [SDR QMLA010108001](https://openairdocs.org/sdr/QMLA010108001), Jan 1, 2008: CANISTER. FULL. AFTER DEPARTURE FROM BASE HOSPITAL AND ENROUTE TO SENDING HOSPITAL, PILOT NOTICED A PERSISTENT FUEL ODOR IN THE CABIN. THE PILOT THEN ABORTED THE MISSION AND RE
- [SDR E3MA071115001](https://openairdocs.org/sdr/E3MA071115001), Oct 18, 2007: BEARING. ROUGH. DURING A DAILY CHECK OF THE AIRCRAFT A GRINDING NOISE WAS DETECTED FROM THE TAIL ROTOR DRIVESHAFT COVER, AFTER AN INVESTIGATION THE GRINDING NOISE WAS FOUND TO 
- [SDR BAQA200700025](https://openairdocs.org/sdr/BAQA200700025), May 18, 2007: SWITCH. WORN. DURING REGULAR FUNCTIONAL CHECK OF ENGINE START SWITCHES, DISCOVERED THE NR1 AND NR2 ENGINE STARTING SWITCHES TO HAVE WORN DETENT IN THE SWITCH. THE SWITCH WAS 
- [SDR 0511070132](https://openairdocs.org/sdr/0511070132), May 11, 2007: BEARING CAGE. FAILED. THE -CHIP LIGHT- WARNING WAS ILLUMINATED ON THE CAD. FOUND BROKEN BEARING CAGE MATERIAL LAYING IN THE BASE OF THE MAIN GEAR BOX. MATERIAL APPEARED TO COME FROM 
- [SDR B65A112894](https://openairdocs.org/sdr/B65A112894), Nov 21, 2006: GAUGE. FLUCTUATES. ROTOR SPEED FLUCTUATED AND THEN FAILED.
- [SDR BAQ2006F00002](https://openairdocs.org/sdr/BAQ2006F00002), Jul 3, 2006: LINE. CONTAMINATED. WATER GETTING INTO FIRE DISCHARGE LINES AND HAS NO WAY TO GET OUT. (K)
- [SDR MHIA106721](https://openairdocs.org/sdr/MHIA106721), Nov 4, 2005: FRAME. DAMAGED. SMALL HOLE FOUND ON BOTTEM OF TAIL BOOM AFT OF 2ND FRAME IN TAIL BOOM. 556MM AFT OF TAIL BOOM FLANGE. REPAIRED IAW MFG REPAIR SCHEME MG110220053 NO REVISION, DA
- [SDR Z1RA106192](https://openairdocs.org/sdr/Z1RA106192), Sep 26, 2005: TRANSDUCER. INTERMITTENT. DURING FLIGHT AL-300 DISPLAYS 1E30 CODE INTERMITTENTLY.
- [SDR B65A105845](https://openairdocs.org/sdr/B65A105845), Aug 14, 2005: PUMP. UNSERVICEABLE. PART FAILED IN FLIGHT, REPLACED PART.
- [SDR ALG2005F00036](https://openairdocs.org/sdr/ALG2005F00036), Jun 30, 2005: ACCUMULATOR. MALFUNCTIONED. AT HOVER FOR TAKEOFF, PICKED AIRCRAFT UP TO A HOVER 2 TIMES AND BOTH TIMES AT A STEADY HOVER, AIRCRAFT OSCILLATED FORE AND AFT WITH NO PILOT INPUT (NOSE UP AND 
- [SDR ALGA096029](https://openairdocs.org/sdr/ALGA096029), Jul 8, 2004: BOLT. CORRODED. BOLT PITTED. REPLACED BY FIELD MAINT.
- [SDR HE66096544](https://openairdocs.org/sdr/HE66096544), Jul 8, 2004: COMPUTER. UNRELIABLE. COMPUTER CAUSING THE TRANSPONDER TO REPORT INACCURATE INFORMATION TO FLIGHT SERVICES.
- [SDR HE66096791](https://openairdocs.org/sdr/HE66096791), Jul 8, 2004: ALTIMETER. OUT OF TOLERANCE. BOUNCES ALL OVER THE PLACE, NOT GOOD FOR IFR FLIGHT.
- [SDR HE66094420](https://openairdocs.org/sdr/HE66094420), May 7, 2004: COMPUTER. UNSERVICEABLE. TRANSPONDER WOULD NOT WORK ABOVE 4000 FT AND NR 2 DME WOULD NOT WORK. AFTER HAVING THE TRANSPONDER REPAIRED SEVERAL TIMES AND FINALLY REPLACED PROBLEM STILL NOT
- [SDR HE66094217](https://openairdocs.org/sdr/HE66094217), Apr 16, 2004: BUTTON. BROKEN. WHEN ACTIVATING ALT HOLD, THE LIGHT WOULD NOT IGNITE CONFIRMING ALT HOLD WAS ENGAGED.
- [SDR BAQA094225](https://openairdocs.org/sdr/BAQA094225), Apr 13, 2004: ACTUATOR. WORN. EXCHANGE. OUTPUT SHAFT HAS EXCESSIVE SIDE PLAY. HARDCARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT. 04/22/2004
- [SDR BAQA094194](https://openairdocs.org/sdr/BAQA094194), Apr 1, 2004: PANEL. CRACKED. PANEL HAD STRESS CRACK IAW SITE MECHANIC, UPON REMOVAL, PANEL SHATTERED AND MECHANIC SCRAPPED ON SITE. REPLACED WITH SERVICEABLE PANEL FROM AEC, 04/16/2004
- [SDR HE66094001](https://openairdocs.org/sdr/HE66094001), Mar 29, 2004: AUTOPILOT SYS. INTERMITTENT. AUTO PILOT FAILED INFLIGHT. AFTER RESETTING AUTOPILOT, IT WOULD FAIL AGAIN.
- [SDR BAQA093969](https://openairdocs.org/sdr/BAQA093969), Mar 29, 2004: CABLE. DISCONNECTED. WARRANTY. CABLE UNWEDGED FROM AFT CABLE. REPLACED WITH SERVICABLE UNIT. 04/07/2004
- [SDR BAQA094226](https://openairdocs.org/sdr/BAQA094226), Mar 29, 2004: IGNITER. UNSERVICEABLE. WARRANTY. ELECTRODE GONE IN UNIT. REPLACED WITH SERVICEABLE ASSET UNIT. 04/26/2004
- [SDR BAQA094029](https://openairdocs.org/sdr/BAQA094029), Mar 26, 2004: INJECTOR. CLOGGED. INJECTOR REMOVED DUE TO SUSPECTED CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004
- [SDR BAQ2004F00000](https://openairdocs.org/sdr/BAQ2004F00000), Mar 26, 2004: HOUSING. BROKEN. THE TAIL ROTOR/ ANTI-TORQUE BALL BEARING CONTROL SYSTEM CONTROL CABLE HOUSING BROKE AND SEPARATED FROM THE ACTUATOR HOUSING NEAR THE AFT SUPPORT ON THE TAIL BOO
- [SDR BAQA093758](https://openairdocs.org/sdr/BAQA093758), Mar 24, 2004: MOUNT. LEAKING. LEAKING AND RETRACTED TOO FAR. REPLACED WITH SERVICABLE UNIT. 03/26/2004
- [SDR BAQA093759](https://openairdocs.org/sdr/BAQA093759), Mar 24, 2004: MOUNT. LEAKING. LEAKING FLUID, AND RETRACTED ALL THE WAY INTO UNIT. REPLACED WITH SERVICABLE UNIT. 03/26/2004
- [SDR BAQA094030](https://openairdocs.org/sdr/BAQA094030), Mar 24, 2004: MANIFOLD. CLOGGED. UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004
- [SDR BAQA094031](https://openairdocs.org/sdr/BAQA094031), Mar 24, 2004: MANIFOLD. CLOGGED. UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004
- [SDR BAQA094032](https://openairdocs.org/sdr/BAQA094032), Mar 24, 2004: INJECTOR. CLOGGED. UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004
- [SDR BAQA094033](https://openairdocs.org/sdr/BAQA094033), Mar 24, 2004: MANIFOLD. CLOGGED. UNIT REMOVED DUE TO SUSPECT CLOGGING. REPLACED WITH SERVICABLE UNIT. 04/01/2004
- [SDR BAQA094034](https://openairdocs.org/sdr/BAQA094034), Mar 24, 2004: MANIFOLD. CLOGGED. UNIT REMOVED DUE TO SUSPECT CLOGGING, RETURNED TO TEC BY TONY N, WITHOUT NOTIFICATION. HARCARD WAS ENCLOSED. REPLACED WITH SERVICABLE UNIT. 04/01/2004
- [SDR BAQA093774](https://openairdocs.org/sdr/BAQA093774), Mar 22, 2004: WARNING SYSTEM. NOISY. EXCESSIVE ICS BACKGROUND NOISE, AND EXCESSIVELY LOUD WARNING TONES. REPLACED WITH SERVICABLE UNIT. 03/22/2004

All 92: https://openairdocs.org/engine/turbomeca-arrius-2b1/reports.md

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