# Service difficulty reports: Bell 206L

A list on [Bell 206L](https://openairdocs.org/model/bell-206l.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 7 · 344 reports

- [SDR EVCA202610120026](https://openairdocs.org/sdr/EVCA202610120026.md): Hydraulic Line · chafed · Oct 9, 2026 · N132AE · Bell 206L · Hydraulic System, Main
  > LOSS OF HYDRAULIC POWER. DUE TO LOSS OF HYDRAULIC FLUID. DUE TO CHAFED OF TWO LINES. HYDRAULIC LINES WERE CHAFED AGAINST EACH OTHER CAUSING THE RUPTURE OF THE PRESSURE HOSE.
- [SDR EVCA20261006001](https://openairdocs.org/sdr/EVCA20261006001.md): Switch · unserviceable · Sep 30, 2026 · N133AE · Bell 206L · Aircraft Fuel System
  > RAW FUEL ODOR IN CABIN AND COCKPIT AREAS IN FLIGHT.
- [SDR 2024F00071](https://openairdocs.org/sdr/2024F00071.md): Support · corroded · Mar 14, 2024 · N206SL · Bell 206L · Nacelle/Pylon Structure
  > BTH-206L1-MM-1-5-31 ( TAIL BOOM),BTH-206L1-MM-1-27-60 PAR 5. REMOVAL AND INSPECTION OF TAIL BOOM STABILIZER REVEALED WEAR AND CORROSION EXCEEDING MANUFACTURES LIMITS. REMOVED AND REPLACED COMPONENT PER MANUFACTURES INSTRUCTIONS. NO FURTHER DEFECTS NOTED.
- [SDR EVCA0608221](https://openairdocs.org/sdr/EVCA0608221.md): Unknown · odor · Jun 7, 2022 · N409AE · Bell 206L · Air Conditioning System
  > ELECTRICAL SMELL IN AC.
- [SDR CA190704013](https://openairdocs.org/sdr/CA190704013.md): Lock Pin · inoperative · Jul 3, 2019 · Bell 206L · Rotorcraft Flight Control
  > (CAN) WE RECENTLY BOUGHT AND INSTALLED THE DART TAIL ROTOR PEDAL LOCK OUT KIT IN OUR BELL 206L AND 407.. YESTERDAY, IN FLIGHT THE PASSENGER TOUCHED THE AFT END OF THE ROD (FIG 3.2 OF DART INN-D119-827) AND IT POPPED OF THE LOCK PIN ALLOWING THE PEDAL TO FALL F
- [SDR CA160108005](https://openairdocs.org/sdr/CA160108005.md): Turbine · failed · Jan 4, 2016 · Bell 206L · Turbine Section
  > (CAN) TURBINE HAD A CATASTROPHIC FAILURE, ACFT AUTO ROTATED TO A CLEARING. 1 MAIN ROTOR BLADE RECEIVED MINOR DAMAGE FROM TURBINE PIECES, NO OTHER ACFT DAMAGE.
- [SDR CA160107008](https://openairdocs.org/sdr/CA160107008.md): Turbine · failed · Jan 4, 2016 · Bell 206L · Turbine Section
  > (CAN) THE TURBINE HAD A CATASTROPHIC FAILURE.
- [SDR CA150428003](https://openairdocs.org/sdr/CA150428003.md): Impeller · failed · Apr 26, 2015 · Bell 206L · Engine Oil Cooler
  > (CAN) 2 MILES FROM FINAL PILOT HEARD A LOUD BANG. ALL GAUGES MONITORED AND SITUATION ASSESSED. ENGINE OIL TEMPERATURE SLOWLY STARTED RISING. ACFT LANDED SAFELY. DURING ENGINE SHUTDOWN PROCEDURE ENGINE OIL TEMPERATURE ROSE TO APPROXIMATELY 140C. AME WAS SENT
- [SDR CA150421002](https://openairdocs.org/sdr/CA150421002.md): Starter Gen · failed · Apr 9, 2015 · Bell 206L · Starter-Generator
  > (CAN) SPECIFIC PART CAUSING DIFFICULTY: STARTER GENERATOR VOLTAGE REGULATOR. STARTER GENERATOR WENT OFFLINE. REMOVED BOTH STARTER GENERATOR & VOLTAGE REGULATOR & REPLACED WITH IDENTICAL PN SERVICEABLE PORTS.
- [SDR CA150220002](https://openairdocs.org/sdr/CA150220002.md): Vent Line · leaking · Feb 17, 2015 · Bell 206L · Fuel Storage
  > (CAN) DURING FORWARD FLIGHT WITH UNDERSLUNG LOAD AND SIGNIFICANT NOSE DOWN ATTITUDE FUEL ODOR WAS NOTICED IN CABIN. ACFT WAS RETURNED TO BASE AND GROUNDED FOR TROUBLESHOOTING. TROUBLESHOOTING WAS COMMENCED LATER IN THE WEEK AND FUEL VENT LINE LOCATED IN VERTI
- [SDR CA150217005](https://openairdocs.org/sdr/CA150217005.md): Stiffener · cracked · Jan 29, 2015 · Bell 206L · Fuselage Miscellaneous Structure
  > (CAN) FOUND 3 CM CURVED HORIZONTAL CRACK ALONG LT LOWER SIDE AND 3.5 CM CURVED HORIZONTAL CRACK ALONG RT SIDE OF HORIZONTAL STIFFENER. ALSO, FOUND 0.5 CM CRACK FROM RT SIDE OF UPPER RT RIVET HOLE TO RT SIDE OF PART ON UPPER SIDE OF HORIZONTAL STIFFENER. CRAC
- [SDR CA141017005](https://openairdocs.org/sdr/CA141017005.md): Cartridge · leaking · Oct 8, 2014 · Bell 206L · Fuel Boost Pump
  > (CAN) BOOST PUMP FUEL CARTRIDGE LEAKING FUEL AND REQUIRES O/H, REPLACED WITH TSO 0.0.
- [SDR CA140918013](https://openairdocs.org/sdr/CA140918013.md): Nozzle · cracked · Sep 16, 2014 · Bell 206L · Turbine Section
  > (CAN) TURBINE MODULE SENT IN FOR O/H. DURING PART INSPECTION AFTER UNIT DISASSEMBLY THE NOZZLE WAS SCRAPPED FOR OUTER BAND CRACKS AS WELL AS FILLET CRACK AT THE VANE AREAS. THE DIAPHRAGM WAS ALSO DISCOVERED CRACKED THRU AT ABOUT 80 PERCENT OF THE UNITS CIRCU
- [SDR CA140717014](https://openairdocs.org/sdr/CA140717014.md): Fuel Control · malfunctioned · Jul 4, 2014 · Bell 206L · Fuel Control/Turbine Engines
  > (CAN) THIS ACFT WAS OUT FLYING FOR THE DAY AND WHEN IT RETURNED TO BASE AND THE PIC DECREASED THE THROTTLE TO GROUND IDLE THE ENGINE WENT PAST IDLE AND SHUTDOWN. ALL ACFT THROTTLE CONTROL RIGGING WAS CHECKED AND FOUND TO BE SERVICEABLE MM. PX AND PY ORFICES
- [SDR CA140527010](https://openairdocs.org/sdr/CA140527010.md): Throttle Cable · damaged · May 26, 2014 · Bell 206L · Power Lever
  > (CAN) PILOT WAS STARTING ACFT. WHEN HE GOT TO 62 N1 HE LT OFF OF THE START SWITCH ACFT IMMEDIATELY WENT TO 110 NR. TORQUE WENT AS HIGH AS 90 PERCENT. HE CLOSED THE FUEL VALVE AND TURNED OFF THE BOOST PUMPS. 110 NR FOR ABOUT 5 SECONDS BEFORE THE FUEL RAN
- [SDR CA140522010](https://openairdocs.org/sdr/CA140522010.md): Bushing · worn · May 12, 2014 · Bell 206L · Main Rotor Gearbox
  > (CAN) TORQUE TRANSMISSION RESTRAINT DUE TO EXCESSIVE PLAY. REMOVED LT STOP ASSY DUE TO WORN BUSHINGS. INSTALLED NEW & SERVICEABLE TSI 0.0 PARTS IN COMPLIANCE WITH TB 206L-94-1971.
- [SDR CA140522006](https://openairdocs.org/sdr/CA140522006.md): Indicator · stuck · May 12, 2014 · Bell 206L · Engine BMEP/Torque Indicating
  > (CAN) TORQUE INDICATOR WOULD NOT INDICATE DUE TO NEEDLE "FROZEN" NOT MOVING. REMOVED SN 302 AND INSTALLED PN 206-075-185-003, TSI 0.0.
- [SDR CA130610013](https://openairdocs.org/sdr/CA130610013.md): Seal · failed · Jun 6, 2013 · Bell 206L · Tail Rotor Gearbox
  > (CAN) NEW SEAL INSTALLED IN ACFT. TAIL ROTOR GEAR BOX DURING O/H. SEAL FAILED AFTER 120.2 HRS IN SERVICE. SEAL REPLACED WITH NEW AND RETURNED TO SERVICE.
- [SDR CA130506008](https://openairdocs.org/sdr/CA130506008.md): Governor · malfunctioned · May 2, 2013 · Bell 206L · Turbine Governor
  > (CAN) DURING TAKEOFF, PILOT REPORTS N2 DROOP FROM 100 PERCENT TO 98 PERCENT. PILOT TRIED TO ACTUATE THE GOVERNOR BACK TO 100 PERCENT, AT THAT POINT IT DROPPED FURTHER TO 95-96 PERCENT. PILOT ENTERED AUTO ROTATION AND LANDED ON A LOGGING ROAD. NO DAMAGE TO A
- [SDR CA130416018](https://openairdocs.org/sdr/CA130416018.md): Switch · leaking · Apr 4, 2013 · Bell 206L · Fuel Flow Sensor
  > (CAN) FUEL LEAKING FROM FUEL FLOW SWITCH. REPLACED WITH SERVICEABLE SWITCH.
- [SDR CA121019012](https://openairdocs.org/sdr/CA121019012.md): Turbine · seized · Oct 17, 2012 · Bell 206L · Turbine Section
  > (CAN) WHILE DECENDING FOR AN APPROACH INTO CAMP, AT APPROXIMATELY 200 FEET AGL, PILOT HEARD A LOUD BANG FOLLOWED BY A YAW, AND A LOSS OF ENGINE POWER. PILOT ENTERED AN AUTOROTATION, AND ELECTED TO GO TO THE SHALLOW RIVER BED NEARBY AS OTHER OPTIONS WERE HEAVI
- [SDR CA121011009](https://openairdocs.org/sdr/CA121011009.md): Filter · broken · Oct 7, 2012 · Bell 206L · Aircraft Fuel Filter/Strainer
  > (CAN) DURING START CYCLE, PILOT HEARD A BANG. HE ABORTED THE START AND WENT TO LOOK FOR THE SOURCE OF THE NOISE. UPON OPENING ENGINE COWLING HE SAW FUEL POURING OUT OF THE AIR FRAME FUEL FILTER BOWL. PILOT RETURNED TO COCKPIT AND SHUTOFF BOOST PUMPS. HE REM
- [SDR CA110930012](https://openairdocs.org/sdr/CA110930012.md): Blade · missing · Sep 27, 2011 · Bell 206L · Turbine Engine Compressor Section
  > (CAN) TWO STATOR BLADES FOUND MISSING ON THE 6TH STAGE OF THE COMPRESSOR HALVES.
- [SDR EVCA20110301001](https://openairdocs.org/sdr/EVCA20110301001.md): Altimeter · malfunctioned · Mar 1, 2011 · Bell 206L · Altimeter, Barometric/Encoder
  > PROBLEMS WITH TRA-3000 RADAR ALTIMETER. OVER THE PAST TWO YEARS WE HAVE HAD NUMEROUS ISSUES WITH THE TRA-3000 RADAR ATIMETER AND THE ACCOMPANYING TRI-40 ANTENNA.
- [SDR CA101116010](https://openairdocs.org/sdr/CA101116010.md): Pump · damaged · Nov 7, 2010 · Bell 206L · Fuel Boost Pump
  > EXCESSIVE NOISE ON START ATTEMPT. REMOVED FUEL PUMP T 1061006 + TRACED NOISE TO FUEL PUMP. SEND TO O/H SHOP. INSTALLED ANOTHER TSO 0.0 UNIT NDF.
- [SDR CA101115021](https://openairdocs.org/sdr/CA101115021.md): Solenoid · burned · Nov 5, 2010 · Bell 206L · Cargo Compartments
  > (CAN) BLEW CIRCUIT BREAKER. ON INSPECTION, SOLENOID WAS BURNT. SENT TO O/H SHOP. INSTALLED TSO 0.0 UNIT.
- [SDR CA100927010](https://openairdocs.org/sdr/CA100927010.md): Bearing · spalled · Sep 15, 2010 · Bell 206L · Main Rotor Gearbox
  > TRANSMISSION CHIP LIGHT CAUSED BY STEADY BEARING ON INPUT PINION.
- [SDR CA100927011](https://openairdocs.org/sdr/CA100927011.md): Bearing · spalled · Jul 23, 2010 · Bell 206L · Turbine Engine Accessory Drive
  > ENGINE CHIP LIGHT CAUSED BY 2.5 BEARING.
- [SDR CA100430004](https://openairdocs.org/sdr/CA100430004.md): Clutch · seized · Apr 26, 2010 · Bell 206L · Engine/Transmission Coupling
  > (CAN) UNUSUAL NOISE DETECTED BY THE PILOT ON SHUT DOWN. FURTHER INVESTIGATION REVEALS SEIZED FREEWHEEL. FREE WHEEL REMOVED AND SENT TO INVESTIGATION TO SKYLINE HELICOPTERS. A REPORT WILL BE SUBMITED SHORTLY.
- [SDR CA091109007](https://openairdocs.org/sdr/CA091109007.md): Indicator · misrepaired · Nov 6, 2009 · Bell 206L · Engine EGT/TIT Indicating System
  > (CAN) RECEIVED THIS INDICATOR FROM O/H AND IT WAS FOUND TO BE INDICATING 300 DEGREES CELSIUIS TO HIGH UPON INSTALLATION AND TEST. WE ARE ASSUMING THIS PROBLEM WAS DUE TO POOR QC OR DAMAGE DUE TO SHIPPING BUT THE BOX THE T.O.T. INDICATOR CAME IN LOOKED UNDAMAG
- [SDR CA091013003](https://openairdocs.org/sdr/CA091013003.md): Blade · delaminated · Oct 10, 2009 · Bell 206L · Tail Rotor Blades
  > (CAN) DURING DAILY INSP PILOT NOTICED THE OTBD T/E SKIN WAS DELAMINATED 6 INCHES FROM THE TIP ON TAIL ROTOR BLADE PN 206-016-201-131, SN CS-12194 BLADE HAS 120.8 HOURS REMAINING BEFOR RETIREMENT. BOTH BLADES WERE REPLACE WITH NEW BLADES AND THE ASSY WAS BALANC
- [SDR CA091008004](https://openairdocs.org/sdr/CA091008004.md): Bearing · worn · Oct 8, 2009 · Bell 206L · Turbine Engine Reduction Gear
  > (CAN) ENGINE CHIP LIGHT FOUND PROBLEM WITH THE BALL BEARING ON THE POWER TAKEOFF OUTPUT SHAFT.
- [SDR CA090902007](https://openairdocs.org/sdr/CA090902007.md): Bearing · spalled · Aug 21, 2009 · Bell 206L · Main Rotor Gearbox
  > ENG CHIP LIGHT, FOUND PROBLEM WITH THE PWR TAKEOFF OUTPUT SHAFT BEARING, INNER AND OUTER RACE WORN.
- [SDR CA090902006](https://openairdocs.org/sdr/CA090902006.md): Bearing · spalled · Aug 21, 2009 · Bell 206L · Fuselage Miscellaneous Structure
  > ENG CHIP LIGHT PROBLEM FOUND WITH THE BALL BRG ON THE PWR TAKEOFF OUTPUT SHAFT.
- [SDR CA091103006](https://openairdocs.org/sdr/CA091103006.md): Bearing · failed · Jun 9, 2009 · Bell 206L · Turbine Engine Reduction Gear
  > (CAN) ENG WAS REMOVED AFTER METAL CONTAMINATION AND SENT TO A REPAIR FACILITY. THE 2.5 BEARING WAS FOUND TO HAVE SPALLED ROLLERS AND RACE AND WAS MISSING A ROLLER. THIS BEARING WAS A PMA PART PN 23034787AL SN TA NR 0511363 AND WAS INSTALLED NEW 385 HOURS AGO.
- [SDR CA090518001](https://openairdocs.org/sdr/CA090518001.md): Bearing · corroded · May 15, 2009 · Bell 206L · Main Rotor Head
  > (CAN) RECEIVED MAIN ROTOR HUB FOR 1200 HOUR INTERIM INSP. WHEN DISASSEMBLED FOUND BOTH OTBD EXCLUDERS IN GRIP ASSEMBLIES WERE NO LONGER RETAINING LUBRICANT AND ALLOWING IT TO PASS INTO THE YOKE SPINDLE BORES. THE YOKE SPINDLES INBD RACE AREA DID NOT HAVE SUF
- [SDR CA090512002](https://openairdocs.org/sdr/CA090512002.md): Bearing · worn · Apr 11, 2009 · Bell 206L · Turbine Section
  > (CAN) PILOT HAD A ENGINE CHIP LIGHT INDICATION, ENGINE WAS REPLACED, INSP REVEALED TURBINE NR 5 BEARING WAS WORN AND SOME BALLS MISSING.
- [SDR CA090407012](https://openairdocs.org/sdr/CA090407012.md): Bearing · damaged · Apr 7, 2009 · Bell 206L · Tail Rotor Blades
  > (CAN) DURING A SERVICEABILITY CHECK AT T/R ASSY SECTION (BLADE S/N CS-10215) BEARING MOVING INSIDE THE BLADE, FOUND.
- [SDR CA090401009](https://openairdocs.org/sdr/CA090401009.md): Bushing · cracked · Mar 31, 2009 · Bell 206L · Main Rotor Control
  > ROUTINE INSPECTION DISCOVERED A CRACK BETWEEN THE THROTTLE ARM BUSHING AND ROLL PIN ACCESS HOLE. COLLECTIVE ELBOW FOUND TO BE CORRECTLY INSTALLED AND NO OTHER DEFECTS NOTED. ELBOW ASSY REPLACED AND ACFT RETURNED TO SERVICE.
- [SDR CA090407013](https://openairdocs.org/sdr/CA090407013.md): Stator Vane · unserviceable · Mar 23, 2009 · Bell 206L · Turbine Engine Compressor Section
  > (CAN) DURING COMPRESSOR HALVES INSP, ONE STATOR BLADE OF THE LAST AXIAL COMPRESSOR STAGE WAS TORN AND WAS SIDEWAYS CONTACTING THE ONE NEXT TO IT. THE BLADE WAS ONLY HELD IN PLACE BY 5-10 PERCENT OF THE BLADE ROOT. THIS COULD HAVE CAUSED THE BLADE TO GO THRU TH
- [SDR CA090304008](https://openairdocs.org/sdr/CA090304008.md): Bearing · damaged · Feb 27, 2009 · Bell 206L · Main Rotor Head
  > (CAN) RECEIVED MAIN ROTOR HUB FOR REPLACEMENT OF TIME EXPIRED COMPONENTS. WHEN DISASSEMBLED FOUND THAT BOTH OTBD EXCLUDERS IN GRIP ASSEMBLIES WERE NO LONGER RETAINING THE LUBRICANT AND ALLOWING IT TO PASS INTO THE YOKE SPINDLE BORES. THE INBD BEARING CONTACT A
- [SDR CA081223003](https://openairdocs.org/sdr/CA081223003.md): Release Cable · separated · Dec 9, 2008 · Bell 206L · Cargo Compartments
  > (CAN) PILOT REPORTED UN-COMMANDED HOOK RELEASE (LOSS OF LEAD) UPON INSPECTION FOUND FAULTY MANUAL RELEASE CABLE WHEN HOOK PULLED TO FAR END OF SWAGED END SEPARATED CAUSING UNCOMMENDED HOOK RELEASE HOOK END CABLE REMOVED FROM A/C AND NEW CABLE ORDERED ALL OTHER
- [SDR CA081017007](https://openairdocs.org/sdr/CA081017007.md): Governor · malfunctioned · Oct 17, 2008 · Bell 206L · Turbine Governor
  > (CAN) UPON REMOVAL OF THE GOVERNOR IT WAS NOTED THAT THE DRIVE GEAR HAD COME SEPARATED. ALL PARTS WERE FOUND IN THE DRIVE GEAR FOR THE GOVERNOR. THERE WAS DIFFICULTY GETTING FULL RANGE OF THE GOVERNOR, COULD NOT ADJUST FOR 100 PERCENT ON THE GROUND. THE DRIVE
- [SDR CA080923004](https://openairdocs.org/sdr/CA080923004.md): Oil System · overtemp · Sep 22, 2008 · Bell 206L · Engine Oil Temperature
  > (CAN) ENGINE OIL TEMPERATURE INCREASED TO 100 DEG. C.
- [SDR CA080813002](https://openairdocs.org/sdr/CA080813002.md): Pitch Horn · loose · Aug 13, 2008 · Bell 206L · Tail Rotor Blades
  > (CAN) THE STUD WHICH HOLDS THE PITCH LINKS ONTO THE PITCH HORN CAME LOOSE. THIS CAUSED A VIBRATION FELT IN THE PEDALS. THE TAILROTOR HUB WAS 2400 HOURS TSO AND BLADES WERE 2300 TSN. THERE IS NO REQUIREMENT TO OVERHAUL THE PITCH HORNS SO NO RECORD AS TO TOTAL T
- [SDR CA080625005](https://openairdocs.org/sdr/CA080625005.md): Blade · delaminated · Jun 12, 2008 · Bell 206L · Main Rotor Blades
  > (CAN) DELAMINATION AT ROOT OF BLADE ON UPPER SURFACE OF THE GIP PLATE FINGER. VISUAL SEPARATION NOTED ON DAILY INSP.
- [SDR CA080103007](https://openairdocs.org/sdr/CA080103007.md): Bolt · broken · Jan 3, 2008 · Bell 206L · Tail Rotor Control System
  > (CAN) ON INSPECTION OF THE AIRCRAFT IT WAS NOTED THAT THE (1) OF THE (3) BOLTS WAS BROKEN AND THE OTHERS SHOWED SIGNS OF CORROSION ALL (3) BOLTS WHERE REPLACED WITH NEW. (TC NR 20080103007)
- [SDR CA071029004](https://openairdocs.org/sdr/CA071029004.md): Housing · cracked · Aug 9, 2007 · Bell 206L · Main Rotor Gearbox
  > (CAN) OIL FOUND ON TRANSMISSION DECK AFTER BRIEF DAILY INSPECTION, OIL LEAK FOUND FROM THE BOTTOM OF THE TRANSMISSION. UPON FURTHER INVESTIGATION TRANSMISSION REMOVED AND BOTTOM CASING FOUND TO BE CRACKED AT LOWER MAST SUPPORT BRG. (TC NR 20071029004)
- [SDR CA070814002](https://openairdocs.org/sdr/CA070814002.md): Blade · damaged · Jul 10, 2007 · Bell 206L · Main Rotor Blades
  > (CAN) UPON LANDING IN A BRUSH AREA, THE PILOT LOWERED THE COLLECTIVE, WHICH IN TURN RAISED (2) TREES THAT WERE SITUATED ON THE LEFT AND THEN HIT THE ROTOR DISK. THE PILOT THEN DISPLACED THE AIRCRAFT TO THE RT. AN ENGINE SHUTDOWN WAS PERFORMED AND VISUAL INSPE
- [SDR CA070726003](https://openairdocs.org/sdr/CA070726003.md): Sleeve · cracked · Jul 9, 2007 · Bell 206L · Fuel Control/Turbine Engines
  > (CAN) PILOT STARTING A/C, THROTTLE OPENED, NO ENGINE LIGHT OFF OCCURED. OPENED ENGINE COWL TO INVESTIGATE, NOTICED FUEL DRIPPING FROM AROUND START DE-RICHMENT ADJUSTMENT OF FCU, ONTO THE STARTER GENERATOR. CONTACTED MAINTENANCE PERSONNEL TO INVESTIGATE. FUEL C

Next page: https://openairdocs.org/model/bell-206l/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 = '206L'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/bell-206l/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.