# Service difficulty reports: Bell Helicopter Textron 206B

A list on [Bell Helicopter Textron 206B](https://openairdocs.org/model/bell-helicopter-textron-206b.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 32 · 1,564 reports

- [SDR 2022FA0000610](https://openairdocs.org/sdr/2022FA0000610.md): None · none · Dec 15, 2021 · N249WW · Bell 206B · Fuselage Structure (General)
  > SEVERAL CRACK-LIKE INDICATIONS WERE FOUND ON THE GEAR TEETH IN THE MAIN ROTOR TRUNNION. THESE INDICATIONS MEASURED ~3/8" LONG IN THE AREA OF INTEREST. CRACKS WERE FOUND WITH FLUORESCENT MAGNETIC PARTICLE TESTING. INSPECTION WAS PERFORMED PER ASTM E1444 AS REQU
- [SDR R73A20210315001](https://openairdocs.org/sdr/R73A20210315001.md): Engine · making metal · Mar 8, 2021 · N134VG · Bell 206B · Engine (Turbine/Turboprop)
  > DURING CRUISE FLIGHT THE PILOT OBSERVED THE "ENGINE CHIP" CAUTION LIGHT ILLUMINATED. PIC LANDED SAFELY IN A NEARBY FOOTBALL FIELD. FOUND (1) SMALL METAL SLIVER ON THE ENGINE'S LOWER MAGNETIC PLUG.
- [SDR 2021FA0000078](https://openairdocs.org/sdr/2021FA0000078.md): Fuel Control · failed · Feb 16, 2021 · N719CB · Bell 206B · Fuel Control/Reciprocating Engines
  > AIRCRAFT ENGINE WOULD NOT START. FUEL CONTROL REMOVED AND REPLACED DISCREPANCY CORRECTED. THIS IS THE FINDINGS OF THE REPAIR STATION THE FUEL CONTROL WAS SENT TO. THIS IS NOT THE SAME REPAIR STATION THAT THE FUEL CONTROL WAS OVERHAULED AT. THE FUEL CONTROL BEL
- [SDR 2021FA0000047](https://openairdocs.org/sdr/2021FA0000047.md): Fuel Control · failed · Feb 16, 2021 · N719CB · Bell 206B · Fuel Control/Turbine Engines
  > FIRST FUEL CONTROL UNABLE TO ADJUST START, SECOND FUEL CONTROL WAS UNABLE TO START AT ALL, REPLACED FUEL CONTROL DISCREPANCY WAS FIXED. THIS WAS ALL IN A YEARS TIME. ON AIRCRAFT 748 THE FUEL CONTROL WAS CHANGED DUE TO THE THROTTLE ARM WAS DIFFICULTY TO ROTATE
- [SDR CA190726010](https://openairdocs.org/sdr/CA190726010.md): Indicator · malfunctioned · Jul 22, 2019 · Bell 206B · Tail Rotor Gearbox
  > (CAN) INDICATOR FOUND TO BE ROTATED IN TAIL ROTOR GEARBOX HOUSING. SIGHT GLASS REMOVED AND INDICATOR FOUND INSTALLED UPSIDE DOWN. UPSIDE DOWN INSTALLATION OCCURRED AT OVERHAUL OF TAIL ROTOR GEARBOX. UPSIDE DOWN INSTALLATION OF INDICATOR NEGATES THE LOCKING MEC
- [SDR CA190716006](https://openairdocs.org/sdr/CA190716006.md): Governor · faulty · Jul 10, 2019 · Bell 206B · Turbine Governor
  > (CAN) AIRCRAFT WAS IN FLIGHT AND PILOT NOTICED A DROP IN ENGINE RPM FROM 100% TO 90%. STARTED DECENT ON A BUSH ROAD. GOVERNOR WAS REPLACED WITH A SERVICEABLE UNIT. NO DAMAGE OR INJURY (TC# 20190716006)
- [SDR CA190712013](https://openairdocs.org/sdr/CA190712013.md): Rod End · loose · Jul 9, 2019 · Bell 206B · Rotorcraft Flight Control
  > (CAN) UPON ROUTINE INSPECTION THE COLLECTIVE TUBE ASSEMBLY WAS FOUND TO HAVE LOOSE ROD ENDS. THIS PART HAS A 4800HR FINITE LIFE, CURRENTLY APPROXIMATELY 1/3 OF ITS LIFE USED. THE ROD ENDS ARE NOT ADJUSTABLE, AND ARE BONDED/STAKED INTO POSITION. THE BONDING HAS
- [SDR CA190716009](https://openairdocs.org/sdr/CA190716009.md): Gyro · faulty · Jun 29, 2019 · Bell 206B · Directional Gyro and Indicating System
  > (CAN) IT WAS REPORTED TO BELL:SHORTLY AFTER TAKEOFF, SMOKE STARTED TO FILL THE COCKPIT. THE PILOT TURNED OFF THE BATTERY, OPENED THE SIDE WINDOW, AND MADE AN EMERGENCY LANDING BACK AT THE POINT OF DEPARTURE. ONCE ALL ELECTRICAL POWER HAD BEEN TURNED OFF, INCLU
- [SDR CA190410019](https://openairdocs.org/sdr/CA190410019.md): Blade · debonded · Apr 9, 2019 · Bell 206B · Main Rotor Blades
  > (CAN) ON MARCH 25 2019, DURING AN ENGINEER WALK AROUND, WE FOUND BOTH VAN HORN MAIN ROTOR BLADE TRIM TABS DEBONDED, THE DEBONDS WERE FOUND ON THE LOWER PORTION OF THE BLADES AND EXTENDING 1.5 INCHES FROM THE INBOARD EDGE OF THE TABS. THERE IS NO INSPECTION OR
- [SDR CA190409008](https://openairdocs.org/sdr/CA190409008.md): Blade · mismanufactured · Mar 26, 2019 · Bell 206B · Main Rotor Blades
  > (CAN) UPON INSTALLATION OF A SET OF NEW MAIN ROTOR BLADES IT WAS DISCOVERED THE ALIGNMENT PIN WAS MISSING FROM ONE OF THE NEW BLADES. PART NUMBER 206-010-200-151 AND COULD NOT BE INSTALLED ONTO THE AIRCRAFT. AFTER CONTACTING THE BELL TECHNICAL REP. HE THEN DIR
- [SDR 2020FA0000049](https://openairdocs.org/sdr/2020FA0000049.md): Rotor · cracked · Mar 12, 2019 · N220GP · Bell 206B · Main Rotor System
  > A CRACK INDICATION WAS INDICATED 7/16 INCHES LONG, 10 INCHES FROM UPPER END OF MAST. CRACK WAS FOUND WITH FLORESCENT MAGNETIC PARTICLE. INSPECTION WAS DONE PER TASK, AS REQUESTED BY CLIENT.
- [SDR LSSA2018F00000](https://openairdocs.org/sdr/LSSA2018F00000.md): Drive Bearing · failed · Sep 20, 2018 · N16726 · Bell 206B · Fuel Control/Turbine Engines
  > THE AIRCRAFT SUFFERED AN INFLIGHT ENGINE OVERSPEED AND SUBSEQUENT ENGINE FAILURE. THE PILOT PERFORMED A SUCCESSFUL AUTOROTATION TO THE GROUND WITH NO DAMAGE TO THE AIRFRAME AND NO INJURIES TO THE OCCUPANTS. AFTER RECOVERY OF THE ACFT AND REMOVAL. INSPECTION
- [SDR CA190110019](https://openairdocs.org/sdr/CA190110019.md): Safety Valve · failed · Sep 19, 2018 · Bell 206B · Turbine Engine Compressor Section
  > (CAN) IT WAS REPORTED TO BELL: ENROUTE WITH A PASSENGER AND SUSTAINED A SUDDEN POWER LOSS. PILOT AUTOROTATED TO AN OPEN FIELD AND THE LANDING GEAR WAS DAMAGED DURING LANDING BUT AIRCRAFT REMAINED UPRIGHT. INVESTIGATION FOUND THE PC SAFETY VALVE HAD FAILED. NO
- [SDR CA180723016](https://openairdocs.org/sdr/CA180723016.md): Monitor · cracked · Jul 19, 2018 · Bell 206B · Main Rotor Gearbox
  > (CAN) DURING SCHEDULED MAINTENANCE, THE TRANSMISSION OIL MONITOR HOUSING WAS REMOVED TO INSPECT THE SCREEN FOR CONTAMINATION. UPON REMOVAL OF THE O-RING FROM THE TRANSMISSION OIL MONITOR IT WAS DISCOVERED THAT THERE WAS CRACKING AROUND THE MOUNTING FLANGE OF
- [SDR CA180117008](https://openairdocs.org/sdr/CA180117008.md): Drive Shaft · worn · Jan 8, 2018 · Bell 206B · Tail Rotor Drive Shaft
  > (CAN) NOTED A KNOCKING NOISE NEAR TAIL ROTOR GEARBOX AFTER AIRCRAFT LANDED FOR MAINTENANCE. FOUND EXCESSIVE PLAY BETWEEN AFT TAIL ROTOR DRIVESHAFT SEGMENT AND HANGER BEARING. DISASSEMBLED AFT SEGMENT AND FOUND WEAR ON BEARING MATING SURFACE OF THE SHAFT, AS
- [SDR TLLA2016040100002](https://openairdocs.org/sdr/TLLA2016040100002.md): Stiffener · cracked · Mar 16, 2016 · N5373U · Bell 206B · Fuselage Main, Structure
  > DURING DAILY INSPECTION, FOUND CRACKS IN THE AFT CROSSTUBE SUPPORT LOWER CORNERS AND STIFFENERS. THE CRACKS ARE COMMON IN THIS MODEL ACFT AND THE REPAIR PROCEDURES ARE DETAILED IN THE SRM BHT-206 SRM-1, REPAIR 5-2-1. ACFT MAY HAVE HAD A HISTORY OF FLIGHT TRA
- [SDR TLLA2016040100001](https://openairdocs.org/sdr/TLLA2016040100001.md): Support · cracked · Mar 16, 2016 · N5373U · Bell 206B · Fuselage Main, Structure
  > DURING DAILY INSPECTION, FOUND CRACKS IN THE ARFT CROSSTUBE SUPPORT STRUCTURE LOWER CORNERS AND STIFFENERS. THE CRACKS ARE COMMON IN THIS MODEL ACFT AND THE REPAIR PROCEDURES ARE DETAILED IN THE SRM BHT 206, SRM-1, REPAIR 5-2-1. THIS ACFT MAY HAVE HAD A HIST
- [SDR 2016FA0000154](https://openairdocs.org/sdr/2016FA0000154.md): Governor · inoperative · Mar 9, 2016 · N211CS · Bell 206B · Engine (Turbine/Turboprop)
  > EPOXY CAME LOOSE FROM END OF DRIVE SHAFT. CLIP CAME LOOSE ALLOWING DRIVE SHAFT SPLINES TO WEAR AND CAUSE UNSTABLE GOVERNOR CONTROL.
- [SDR 2016FA0000153](https://openairdocs.org/sdr/2016FA0000153.md): Governor · inoperative · Mar 9, 2016 · N59548 · Bell 206B · Main Rotor System
  > EPOXY CAME LOOSE FROM END OF DRIVE SHAFT. CLIP CAME LOOSE ALLOWING DRIVE SHAFT SPLINES TO WEAR AND CAUSE EXCESSIVE DROOPING DURING ENGINE POWER CHANGES.
- [SDR CA160215022](https://openairdocs.org/sdr/CA160215022.md): Coupling · broken · Feb 15, 2016 · Bell 206B · Tail Rotor Drive Shaft
  > (CAN) DURING A SCHEDULED 100/300 HR INSPECTION, THE OUTER DISC OF A 10 DISC PACK WAS DISCOVERED BROKEN THE EDGE RUB INDICATES THAT THE DISC HAS PROBABLY BEEN BROKEN FOR SOME TIME THE ACFT TT IS 9444.3. THE BROKEN PART IS UNKNOWN TIME IN SERVICE THE APPEARANCE
- [SDR 2016FA0000047](https://openairdocs.org/sdr/2016FA0000047.md): Structure · cracked · Feb 3, 2016 · N206NU · Bell 206B · Fuselage Main, Structure
  > DURING A ROUTINE 12 MONTH INSPECTION THE HAT-RACK, LOCATED ABOVE AND BEHIND THE FORWARD FACING CABIN SEATS, WAS REMOVED TO INSPECT THE STRUCTURE IN THE AREA OF THE ENGINE PAN. 4 CRACKS IN PRIMARY STRUCTURE WERE DISCOVERED. 1 WAS ON THE EDGE OF AN INSPECTION
- [SDR CA160203023](https://openairdocs.org/sdr/CA160203023.md): Burner Can · cracked · Feb 2, 2016 · Bell 206B · Turbine Engine Combustion Section
  > (CAN) PILOT NOTED HIGHER THEN NORMAL TOT TEMPERATURES IN FLIGHT, PILOT LANDED AT THE HANGER AND UPON FURTHER INVESTIGATION FOUND RT BURNER CAN ARMPIT CRACKED.
- [SDR TLLA201602020001](https://openairdocs.org/sdr/TLLA201602020001.md): Web · cracked · Jan 22, 2016 · N5373U · Bell 206B · Fuselage Main, Structure
  > DURING SCHEDULED ANNUAL INSPECTION, FOUND A CRACK EMANATING FROM ACCESS HOLE IN LOWER WEB OF ROOF BEAM AT BS 119.0. THIS AREA INSPECTION IS DETAILED IN MM1-5-29, 300 HR INSPECTION. THIS ACFT HAS A CARGO HOOK, BUT HAS NO HISTORY OF UNUSUAL FLIGHT PARAMETERS:
- [SDR CA150918003](https://openairdocs.org/sdr/CA150918003.md): Governor · malfunctioned · Sep 14, 2015 · Bell 206B · Turbine Governor
  > (CAN) DURING ACFT RUN UP AND PRE TAKEOFF CHECKS THE PILOT WAS UNABLE TO OBTAIN FULL MAIN ROTOR RPM. THE ACFT WAS SHUTDOWN AND MAINTENANCE CONTACTED. THE AME FOUND THE ENGINE GOVERNOR ARM TO BE SEIZED. THE ENGINE GOVERNOR ASSEMBLY WAS REPLACED AND THE ACFT RET
- [SDR NKVR20150908002](https://openairdocs.org/sdr/NKVR20150908002.md): Stiffener · cracked · Sep 8, 2015 · N206PL · Bell 206B · Fuselage Miscellaneous Structure
  > DURING INSPECTION, STIFFENER NEAR TAIL BOOM ATTACH INSPECTION PANEL FOUND TO BE CRACKED.
- [SDR NKVR20150908001](https://openairdocs.org/sdr/NKVR20150908001.md): Stiffener · cracked · Sep 8, 2015 · N206PL · Bell 206B · Fuselage Miscellaneous Structure
  > DURING INSPECTION, STIFFENER FOUND TO BE CRACKED NEAR TAIL BOOM ATTACH INSPECTION PANEL.
- [SDR NKVR20150817002](https://openairdocs.org/sdr/NKVR20150817002.md): Support · cracked · Sep 8, 2015 · N206PL · Bell 206B · Fuselage Miscellaneous Structure
  > DURING INSPECTION, RT LG TUNNEL SUPPORT FOUND TO BE CRACKED.
- [SDR NKVR20150817001](https://openairdocs.org/sdr/NKVR20150817001.md): Support · cracked · Sep 8, 2015 · N206PL · Bell 206B · Fuselage Miscellaneous Structure
  > DURING INSPECTION, FOUND RT LG TUNNEL CRACKED, STATION 125, WL 21, RBL 13.5 & LBL 13.5, UPON FURTHER INSPECTION A CRACK IN THE SAME LOCATION WAS FOUND ON THE LT SIDE AS WELL. STOP DRILLED & FABRICATED REPAIR PARTS FROM NEW PART & INSTALLED IAW SRM 1 CHAPTER 5
- [SDR CA150910011](https://openairdocs.org/sdr/CA150910011.md): Vane · missing · Sep 6, 2015 · Bell 206B · Turbine Engine Compressor Section
  > (CAN) A ENGINEER WAS CALLED TO THE HELICOPTER DUE TO A DEFECT OF LACK OF POWER IN THE POWER ASSURANCE CHECK. THE ENGINEER CARRIED OUT A COMPRESSOR WASH STILL LACK OF POWER. THE ENGINEER REMOVED THE COMBUSTION CASE AND FOUND PART OF THE COMPRESSOR CASE HALF ST
- [SDR CA150827011](https://openairdocs.org/sdr/CA150827011.md): Bearing · failed · Aug 24, 2015 · Bell 206B · Main Rotor Gearbox
  > (CAN) ACFT WARNING SYSTEM INDICATED METAL CHIP GENERATION INSIDE MAIN TRANSMISSION. TRANSMISSION REMOVED FROM ACFT AND INVESTIGATION FOUND DUPLEX BEARING DETERIORATION.
- [SDR CA150812004](https://openairdocs.org/sdr/CA150812004.md): Horn · failed · Aug 7, 2015 · Bell 206B · Main Rotor Indicating System
  > (CAN) LOW ROTOR HORN FAILED, REMAINED QUIET AT SHUTDOWN.
- [SDR CA151117023](https://openairdocs.org/sdr/CA151117023.md): Discharge Tube · cracked · Aug 1, 2015 · Bell 206B · Engine Temperature Indicating System
  > (CAN) PILOT NOTICED ON LANDING A HIGHER THEN NORMAL TOT. INVESTIGATION FOUND THAT THERE WAS A CRACK FOUND IN THE DISCHARGE TUBE.
- [SDR 2017FA0000127](https://openairdocs.org/sdr/2017FA0000127.md): Longeron · cracked · Jul 17, 2015 · N16206 · Bell 206B · Fuselage Main, Longeron/Stringer
  > THE RT UPPER AFT LONGERON WAS FOUND CRACKED. THE CRACK EXTENDED DOWNWARD FROM THE UPPER FLANGES FREE EDGE AT BS 117. THE LONGERON WAS REPLACED.
- [SDR CA150804004](https://openairdocs.org/sdr/CA150804004.md): Spring · broken · Jul 3, 2015 · Bell 206B · Fuel Control/Turbine Engines
  > (CAN) FOLLOWING THE SECOND GROUND RUN AND TEST FLIGHT FOLLOWING A TURBINE CHANGE THE PILOT MENTIONED TO THE AME ONBOARD THAT THE THROTTLE FELT A LITTLE STIFF WHEN ROLLING DOWN FROM 100%. THE AME THEN GOT OUT TO CHECK AND NOTICED THE SPRING WAS IN A DIFFERENT P
- [SDR CA150617020](https://openairdocs.org/sdr/CA150617020.md): Blade · damaged · May 22, 2015 · Bell 206B · Main Rotor Blades
  > (CAN) PILOT WAS ON APPROACH BACK TO FORESTRY BASE, 1.5 MILES WHEN HE AND HIS PASSENGER HEARD A LOUD POP. THEY LOOKED AROUND THE CABIN BUT FOUND AND FELT NOTHING. UPON LANDING AND SHUTDOWN, A WHISTLING SOUND WAS HEARD FROM THE BLADES. AN INVESTIGATION BY THE PI
- [SDR CA150519023](https://openairdocs.org/sdr/CA150519023.md): Gear · damaged · May 19, 2015 · Bell 206B · Tail Rotor Gearbox
  > (CAN) UPON INSPECTION OF THE GEAR DURING O/H OF THE GEARBOX, IT WAS FOUND THAT 1 OF THE ATTACHMENT BOLT HOLES HAD NO CHAMFER WHERE THE BOLT HEAD MEETS THE GEAR FACE. THIS RESULTED IN DAMAGE TO THE SHANK AREA UNDERNEATH THE BOLT HEAD.
- [SDR CA150511010](https://openairdocs.org/sdr/CA150511010.md): Bearing · failed · May 9, 2015 · Bell 206B · Turbine Governor
  > (CAN) ROTOR RPM WANDERING. REMOVED GOVERNOR, FOUND BEARING PIECES IN CAVITY.
- [SDR CA150504003](https://openairdocs.org/sdr/CA150504003.md): Gear · cracked · May 1, 2015 · Bell 206B · Turbine Engine Reduction Gear
  > (CAN) AN EXCESSIVE OIL LEAK AT TURBINE/GEARBOX JOINT WAS DISCOVERED DURING A DAILY INSPECTION. FURTHER INVESTIGATION SHOWED THE GEARBOX FLANGE APPEARS TO BE CRACKED. THE ENGINE GEARBOX WAS REPLACED AND SENT FOR REPAIRS. THE GEARBOX TSO 4552.9 AND TSN 11,440.5
- [SDR CA150327010](https://openairdocs.org/sdr/CA150327010.md): Skid · cracked · Mar 26, 2015 · Bell 206B · Wheel/Ski/Float
  > (CAN) DURING REMOVAL OF GROUND HANDLING WHEELS THE RT SKID TUBE WAS FOUND TO BE CRACKED AROUND THE COMPLETE CIRCUMFERENCE OF THE SKID TUBE AT THE FORWARD GROUND HANDLING WHEEL ATTACHMENT.
- [SDR CA150327013](https://openairdocs.org/sdr/CA150327013.md): Nut · cracked · Mar 24, 2015 · Bell 206B · Tail Rotor Head
  > (CAN) DURING A SCHEDULED TAIL ROTOR REMOVAL AME WENT TO REMOVE THE TAIL ROTOR CROSSHEAD, 206-011-857-001. RETAINING NUT AND THERE WAS NO TORQUE, AND THOUGH STRANGE, IT WAS CRACKED RIGHT AT THE SLOT.
- [SDR CA150318009](https://openairdocs.org/sdr/CA150318009.md): Lock Nut · cracked · Mar 6, 2015 · Bell 206B · Tail Rotor Gearbox
  > (CAN) AT LAST 100 HRS INSPECTION OF HELICOPTER, TT 3276,5 HOURS, INSPECTED THE TAIL ROTOR SELF LOCKING NUT AND FOUNDED IT CRACKED AT HALF, REPLACED IT FOR A NEW NUT.
- [SDR CA141224005](https://openairdocs.org/sdr/CA141224005.md): Engine · malfunctioned · Dec 23, 2014 · Bell 206B · Engine (Turbine/Turboprop)
  > (CAN) HELICOPTER WAS STARTED FOR A GROUND RUN. IT WAS NOTED THAT DURING THE GROUND RUN, MAIN ROTOR BLADES STARTED TO TURN. THEN THE MAIN ROTOR BLADES STARTED TO DEACCELERATE WITH NO THROTTLE ADJUSTMENT. WE ARE TROUBLESHOOTING THE OBSERVATION DEFECT.
- [SDR CA141212009](https://openairdocs.org/sdr/CA141212009.md): Clutch · worn · Dec 10, 2014 · Bell 206B · Engine/Transmission Coupling
  > (CAN) DURING TRAINING, IT WAS NOTICED THAT THE TACH NEEDLES DID NOT SEPARATE WHEN THE THROTTLE WAS ROLLED BACK TO IDLE. FREEWHEEL ASSY WAS REMOVED AND SENT TO O/H SHOP FOR INSPECTION. DURING INSPECTION CLUTCH ASSY WAS DEEMED UNSATISFACTORY.
- [SDR CA150122007](https://openairdocs.org/sdr/CA150122007.md): Turbine Wheel · cracked · Oct 14, 2014 · Bell 206B · Turbine Section
  > (CAN) THE PILOT HAD REPORTED N2 LOCKUP. DURING MAINTENANCE THE ENGINE WAS DISASSEMBLED TO HAVE THE ENGINE GEARBOX REPAIRED AND TO SEND THE TURBINE FOR INSPECTION TO DETERMINE THE CAUSE OF THE N2 LOCKUP. THE TURBINE WAS SENT FOR INSPECTION. DURING THE INSPEC
- [SDR CA140918010](https://openairdocs.org/sdr/CA140918010.md): Window · detached · Sep 16, 2014 · Bell 206B · Flight Compartment Windows
  > (CAN) WHILE DOING A 15 MIN COMMERCIAL TOUR, AIRCRAFT`S PILOT SIDE LOWER CHIN POP OUT. BUBBLE WINDOW SEPARATED FROM THE AIRFRAME AT APPROXIMATELY 300 FT AGL ON APPROACH TO THE BASE FACILITY. AN INSPECTION OF THE WINDOW FRAME REVEALED THAT THERE MAY HAVE BEEN
- [SDR CA141024021](https://openairdocs.org/sdr/CA141024021.md): Blade · damaged · Sep 2, 2014 · Bell 206B · Main Rotor Blades
  > (CAN) LOSS OF M/R BLADE TELL-TALE WEIGHT CAUSED LATERAL VIBRATIONS. PILOT FOUND THE TIP CAP YIELDED FROM MOUNTING, BUT STILL ATTACHED BY LOWER FORWARD SCREW.
- [SDR CA140826026](https://openairdocs.org/sdr/CA140826026.md): Rib · cracked · Aug 11, 2014 · Bell 206B · Rotorcraft Tail Boom
  > (CAN) WHEN CARRYING OUT A 300 HR INSPECTION ON THE ACFT, A CRACK WAS FOUND ON THE LT STABILIZER ATTACHMENT FITTING OF THE INBD RIB. THERE WERE NO DEFECTS FOUND ON THE ADJACENT TAILBOOM AREA. THIS ATTACHMENT FITTING ALLOWS FOR FASTENING THE STABILIZER TO THE
- [SDR CA140811005](https://openairdocs.org/sdr/CA140811005.md): Turbine · making metal · Jul 30, 2014 · Bell 206B · Turbine Section
  > (CAN) DURING POST INSTALLATION GROUND RUNS AFTER A SCHEDULED TURBINE CHANGE THERE WERE THREE ENGINE CHIP INDICATIONS ON BOTH THE UPPER AND LOWER CHIP DETECTOR. FIRST CHIP INDICATION WAS BURNED, CHIP RETURNED IN 10 SECONDS, ENGINE SHUT DOWN, FOUND TWO SMALL HAI
- [SDR IGAL2014FA0000404](https://openairdocs.org/sdr/IGAL2014FA0000404.md): Support Bracket · defective · Jun 13, 2014 · N49643 · Bell 206B · Rotorcraft Tail Boom
  > DURING SCHEDULED 100 HOUR INSPECTION AND COMPIANCE WITH ASB206-12-129, REV C DATED 09 JUNE 2014 FOR INSPECTION ONLY, WHICH IS DIRECTLY APPLICABLE TO THE PART THAT WAS FOUND DEFECTIVE, THE SUPPORT BRACKET WAS FOUND BOTH CRACKED AND BROKEN. MFG WAS NOTIFIED AT
- [SDR CA140220004](https://openairdocs.org/sdr/CA140220004.md): Motor · inoperative · Feb 14, 2014 · Bell 206B · Air Distribution Fan
  > (CAN) DURING 600 HR/END OF SEASON SHROUD HEATER ANNUAL INSPECTION THE BLOWER MOTOR WAS FOUND TO BE INOPERATIVE. BLOWER MOTOR REPLACED.

Next page: https://openairdocs.org/model/bell-helicopter-textron-206b/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 = '206B'
ORDER BY difficulty_date DESC
```

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

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