# Service difficulty reports: Bell 214ST

A list on [Bell 214ST](https://openairdocs.org/model/bell-214st.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 31 · 1,513 reports

- [SDR 9EKA20210602](https://openairdocs.org/sdr/9EKA20210602.md): Nut · loose · May 29, 2021 · N823H · Bell 214ST · Main Rotor Gearbox
  > DURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT FRETTING WAS OCCURRING BETWEEN THE RING GEAR CASE AND THE UPPER CASE OF MAIN GEAR BOX. C/W TORQUE CHECK OF STUDS AND FOUND NUTS HAVE LOST TORQUE.
- [SDR 9EKA202004241002](https://openairdocs.org/sdr/9EKA202004241002.md): Panel · corroded · Apr 21, 2020 · N746H · Bell 214ST · Fuselage Miscellaneous Structure
  > DURING A CORROSION INSPECTION, MULTIPLE LOCATIONS OF CORROSION FOUND ON THIS PANEL.
- [SDR 9EKA20200409001](https://openairdocs.org/sdr/9EKA20200409001.md): Tube · broken · Apr 9, 2020 · N787SR · Bell 214ST · Engine (Turbine/Turboprop)
  > WHILE CONDUCTING AN APPROACH ENGINE NO.1 POWER ROLLED BACK. OBSERVATIONS AND ACTIONS WERE: 1. SOUND OF ENGINE SPOOL DOWN 2. ENG.1 OUT LIGHT, FOLLOWED BY MASTER CAUTION LIGHT. 3. TQ SPLIT SHOWING ENG.1 DECREASING TOWARDS ZERO. 4. CONFIRMED ENG.1 GAUGES
- [SDR 9EKA201906075003](https://openairdocs.org/sdr/9EKA201906075003.md): Blade · eroded · Jun 5, 2019 · N746H · Bell 214ST · Main Rotor Blades
  > DURING CRUISE, HEAVY VIBRATION FELT ON AIRCRAFT. THE AIRCRAFT MADE A PRECAUTIONARY LANDING OFF FIELD. ON INSPECTION, TIP CAP OF MAIN ROTOR BLADE SPLIT AND PEELED BACK. THERE APPEARED TO BE EROSION IN THE SANDY ENVIRONMENT.
- [SDR 9EKA20190526005](https://openairdocs.org/sdr/9EKA20190526005.md): Hydraulic Line · worn · May 26, 2019 · N746H · Bell 214ST · Hydraulic System, Auxiliary
  > DURING CRUISE FLIGHT, OIL COOLER LIGHT ILLUMINATED. EMERGENCY PROCEDURES CARRIED OUT, SWITCHING THE FAN TO THE SECONDARY BLEED AIR FAN. OIL TEMP REMAINED IN THE GREEN AND THE AIRCRAFT LANDED SAFELY AT BASE. UPON ARRIVAL, IT WAS DETERMINED THAT A LEAK IN THE
- [SDR 9EKA20190125001](https://openairdocs.org/sdr/9EKA20190125001.md): Sensor · inoperative · Jan 25, 2019 · N823H · Bell 214ST · Attitude Gyro and Indicating System
  > ROLL SCAS KICKED OFF IN FLIGHT AND WOULD NOT RE-ENGAGE.
- [SDR 9EKA20181207005](https://openairdocs.org/sdr/9EKA20181207005.md): Mast · cracked · Dec 6, 2018 · N512EV · Bell 214ST · Main Rotor Mast/Swashplate
  > DURING WEEKLY INSPECTION, FOUND 1 EACH BROKEN MAST TO TRANSMISSION MOUNT STUD BROKEN. NOT STILL ATTACHED TO BROKEN STUD AND THE TORQUE STRIPE NOT AFFECTED AND HOLDING BROKEN STUD WITH NUT IN PLACE. FURTHER INSPECTION OF THE AREA FOUND MULTIPLE CRACKS TO THE MA
- [SDR 9EKA2018110810003](https://openairdocs.org/sdr/9EKA2018110810003.md): Support · cracked · Oct 30, 2018 · N825H · Bell 214ST · Fuselage Miscellaneous Structure
  > PN 214-031-240-173 SUPPORT FOUND CRACKED DURING AIRFRAME INSPECTION.
- [SDR 9EKA20170527002](https://openairdocs.org/sdr/9EKA20170527002.md): Erosion Shield · debonded · May 26, 2017 · N825H · Bell 214ST · Main Rotor Blades
  > DURING PREVENTATIVE TOUCH UP PAINT ON MAIN ROTOR BLADE, DISCOVERED LOWER BLADE EROSION PLATE DEBONDED AT BOND LINE
- [SDR 9EKA20160808010](https://openairdocs.org/sdr/9EKA20160808010.md): Support · cracked · Aug 7, 2016 · N825H · Bell 214ST · Fuselage Miscellaneous Structure
  > DURING POST FLIGHT DISCOVERED A 4" SKIN CRACK IN FUSELAGE AFT OF RT PILOT DOOR. DURING HIDDEN DAMAGE INSPECTION, FOUND CRACKED BULKHEAD DOOR POST SUPPORT AT STA 142.50, WL 22.00, BL 40.0.
- [SDR 2017FA0000421](https://openairdocs.org/sdr/2017FA0000421.md): Panel · cracked · Jul 2, 2016 · N390AL · Bell 214ST · Fuselage Main, Plate/Skin
  > FUSELAGE LOWER PANEL BELOW LEFT FUEL BLADDER HAS A 30 INCHES LONGITUDINAL CRACK.
- [SDR 9EKA20160702009](https://openairdocs.org/sdr/9EKA20160702009.md): Skin Panel · cracked · Jul 2, 2016 · N390AL · Bell 214ST · Fuselage Main, Plate/Skin
  > DURING A POST FLIGHT INSPECTION, FUSELAGE LOWER PANEL, BELOW LT FUEL BLADDER FOUND TO HAVE A 30" LONGITUDINAL CRACK.
- [SDR 9EKA20160512006](https://openairdocs.org/sdr/9EKA20160512006.md): Ecu · faulty · May 12, 2016 · N390AL · Bell 214ST · Fuel Control/Turbine Engines
  > ENGINE 1 INDICATED EXCESSIVE TORQUE SPLIT WITH YAW MOTION OF THE ACFT. ENG 1 THROTTLE WAS MANUALLY BROUGHT DOWN TO 10% BELOW NR 2 & SAFELY RETURNED TO BASE.
- [SDR JYDR20160225 053](https://openairdocs.org/sdr/JYDR20160225%20053.md): Ring Gear · cracked · Feb 24, 2016 · N214EB · Bell 214ST · Main Rotor Gearbox
  > MGB REMOVED FOR OIL LEAKING FROM CRACK IN RING GEAR CASE. UPON DISASSEMBLY AT REPAIR STATION DISCOVERED A SECTION OF 13 SPLINE TEETH ON THE UPPER RING FRACTURED. 7 TEETH WERE COMPLETELY SEPARATED FROM THE CASE BUT HELD IN PLACE BY THE INNER RING GEAR ASSY.
- [SDR 9EKA20160224002](https://openairdocs.org/sdr/9EKA20160224002.md): Blade · cracked · Feb 24, 2016 · N511EV · Bell 214ST · Main Rotor Blades
  > MAIN ROTOR BLADE HAS A 2 INCH CRACK IN THE CHORD DIRECTION OF THE TIP SHOE, CAUSED FROM EROSION, AS A RESULT FROM UNIMPROVED LANDING ZONES.
- [SDR 9EKA20160219001](https://openairdocs.org/sdr/9EKA20160219001.md): Stud · sheared · Feb 19, 2016 · N214EB · Bell 214ST · Main Rotor Mast/Swashplate
  > TWO MAIN ROTOR TRANSMISSION MAST STUDS FOUND SHEARED OFF DURING 25 HOUR INSPECTION.
- [SDR 9EKA20151201026](https://openairdocs.org/sdr/9EKA20151201026.md): Chip Detector · activated · Dec 1, 2015 · N214EB · Bell 214ST · Tail Rotor Drive Indicating System
  > PILOT REPORTED MOMENTARY TAIL ROTOR GEAR BOX CHIP LIGHT ON MASTER CAUTION PANEL.
- [SDR 9EKA20151124025](https://openairdocs.org/sdr/9EKA20151124025.md): Fuel Filter · dirty · Nov 24, 2015 · N214EB · Bell 214ST · Engine Fuel Distribution
  > NUMBER 1 ENG FUEL FILTER MASTER CAUTION LIGHT CAME ON, INDICATING FUEL FLOW RESTRICTION.
- [SDR 9EKA20150916024](https://openairdocs.org/sdr/9EKA20150916024.md): Engine · failed · Sep 16, 2015 · N214EB · Bell 214ST · Engine (Turbine/Turboprop)
  > DURING CRUISE FLIGHT IN A SHALLOW RIGHT HAND TURN, NR 2 ENG EXPERIENCED HIGH SIDE FAILURE IMMEDIATELY, FOLLOWED BY UNCOMMANDED SHUTDOWN. ACFT RECOVERED 26 MILES BACK TO BASE IN SINGLE ENG CONFIGURATION.
- [SDR 9EKA2015FA0000414](https://openairdocs.org/sdr/9EKA2015FA0000414.md): Chip Detector · damaged · Aug 28, 2015 · N511EV · Bell 214ST · Turbine Engine Oil System
  > ON RETURN TO BASE, NR 2 ENGINE CHIP DETECTOR CAUTION LIGHT ILLUMINATED AND STAYED ON, EMERGENCY PROCEDURES IAW THE RFM WERE C/W BY THE PIC, CONDUCTED TROUBLESHOOTING AND FOUND ELECTRICAL CHIP DETECTOR HOUSING DAMAGED CAUSING FALSE CAUTION LIGHT, REPLACED WITH
- [SDR 9EKA2015052720](https://openairdocs.org/sdr/9EKA2015052720.md): Case · cracked · May 23, 2015 · N511EV · Bell 214ST · Tail Rotor Gearbox
  > 90 DEGREE TAIL ROTOR GEAR BOX LOWER LT CASE AROUND MOUNTING STUD BROKEN.
- [SDR 9EKA2015052019](https://openairdocs.org/sdr/9EKA2015052019.md): Fuel Filter · restricted · May 17, 2015 · N393AL · Bell 214ST · Engine Fuel Distribution
  > NUMBER 2 ENG FUEL FILTER MASTER CAUTION LIGHT CAME ON WHEN THE ENG WAS AT 60 % TQ, INDICATING A FUEL FLOW RESTRICTION.
- [SDR 9EKA0514201518](https://openairdocs.org/sdr/9EKA0514201518.md): Structure · delaminated · May 12, 2015 · N511EV · Bell 214ST · Fuselage Miscellaneous Structure
  > RIGHT ENG SERVICE DECK HONEYCOMB PANEL HAS DELAMINATION OF APPROX 3" DIAMETER, STATION 298, BL 25, WL 65.
- [SDR 9EKA2015050517](https://openairdocs.org/sdr/9EKA2015050517.md): Bulkhead · cracked · May 5, 2015 · N511EV · Bell 214ST · Nacelle/Pylon, Bulkhead/Firewall
  > CRACK 2.75 INCHES FOUND ON AFT LT PYLON BULKHEAD AREA, PREVIOUS HELICOPTER REPAIR COMPLETED.
- [SDR 9EKA2015040314](https://openairdocs.org/sdr/9EKA2015040314.md): Plate · torn · Apr 1, 2015 · N393AL · Bell 214ST · Main Rotor System
  > DURING CRUISE FLIGHT, PILOT REPORTED UNUSUAL VIBRATIONS. DURING INSPECTION, NODAL BEAM PLATES & HELPER SPRING FOUND TO HAVE TORN ELASTOMERIC RUBBER.
- [SDR 9EKA2015033013](https://openairdocs.org/sdr/9EKA2015033013.md): Case · cracked · Mar 27, 2015 · N214EB · Bell 214ST · Main Rotor Gearbox
  > DURING PREFLIGHT OIL WAS NOTICED ON THE UPPER TRANSMISSION CASE. UPON FURTHER INVESTIGATION, PAINT WAS BUBBLED ON RING GEAR CASE. CLEANED PAINT & DYE PENETRANT WAS USED REVEALING A SUSPECTED CRACK. ACFT WAS RUN AT 100% NR & OIL WAS NOTICED COMING FROM A CRA
- [SDR 9EKA02162015003](https://openairdocs.org/sdr/9EKA02162015003.md): Turbine · cracked · Feb 13, 2015 · N512EV · Bell 214ST · Turbine Engine Compressor Section
  > DURING 25 HR SCHEDULED INSPECTION, CRACK WAS FOUND IN EXHAUST AREA OF NR 1 POWER TURBINE. MM WAS REFERENCED & NO CRACKS ARE ALLOWED, AWAITING PT CHANGE.
- [SDR 9EKA02162015002](https://openairdocs.org/sdr/9EKA02162015002.md): Hose · chafed · Jan 30, 2015 · N511EV · Bell 214ST · Main Rotor Gearbox
  > WHILE IN STEADY STATE CRUISE FLIGHT AT 70% TQ, MAIN TRANSMISSION OIL CAUTION LIGHT ILLUMINATED & THE OIL PRESS GAUGE FOR THE TRANSMISSION WAS OBSERVED DECREASING RAPIDLY. PRECAUTIONARY EMER LANDING WAS MADE IN LESS THAN 1 MIN & THE ACFT SAFELY TOUCHED DOWN.
- [SDR 9EKA02162015001](https://openairdocs.org/sdr/9EKA02162015001.md): Skin · debonded · Dec 25, 2014 · N214EB · Bell 214ST · Rotorcraft Tail Boom
  > TAIL BOOM, EMPENNAGE METALLIC SKIN, HONEYCOMB STRUCTURE ON RT SIDE JUST AFT OF THE FWD VOR ANTENNA MOUNT WL 74, BS 294 HAS DISBONDED. INSPECTION WAS PERFORMED IAW BHT ALL SRM 2-13. TAIL BOOM IS BEING REPLACED WITH REPAIRED SERVICE TAIL BOOM. DAMAGED TAIL BO
- [SDR 9EKA201411190134](https://openairdocs.org/sdr/9EKA201411190134.md): Panel · cracked · Nov 19, 2014 · N787SR · Bell 214ST · Fuselage Miscellaneous Structure
  > WHILE PERFORMING THE 25HR 7 DAY A CHECK, AIRFRAME & ENG 1 & 2 INSPECTION, A SIGNIFICANT SERIES OF CRACKS WERE DISCOVERED IN THE AFT LT BAGGAGE COMPARTMENT.
- [SDR 9EKA201411190133](https://openairdocs.org/sdr/9EKA201411190133.md): Support · damaged · Nov 19, 2014 · N787SR · Bell 214ST · Fuselage Miscellaneous Structure
  > WHILE PERFORMING THE 25HR 7 DAY A CHECK, AIRFRAME & ENG 1 & 2 INSPECTION, A SIGNIFICANT SERIES OF CRACKS WERE DISCOVERED IN THE AFT LT BAGGAGE COMPARTMENT.
- [SDR 9EKA201411190132](https://openairdocs.org/sdr/9EKA201411190132.md): Panel · cracked · Nov 19, 2014 · N787SR · Bell 214ST · Fuselage Miscellaneous Structure
  > WHILE PERFORMING THE 25HR 7 DAY A CHECK, AIRFRAME & ENG 1 & 2 INSPECTION, A SIGNIFICANT SERIES OF CRACKS WERE DISCOVERED IN THE AFT LT BAGGAGE COMPARTMENT.
- [SDR 9EKA201411190131](https://openairdocs.org/sdr/9EKA201411190131.md): Cap · cracked · Nov 19, 2014 · N787SR · Bell 214ST · Fuselage Miscellaneous Structure
  > WHILE PERFORMING THE 25HR 7 DAY A CHECK, AIRFRAME & ENG 1 & 2 INSPECTION, A SIGNIFICANT SERIES OF CRACKS WERE DISCOVERED IN THE AFT LT BAGGAGE COMPARTMENT.
- [SDR 9EKA20141119013](https://openairdocs.org/sdr/9EKA20141119013.md): Cap · cracked · Nov 19, 2014 · N787SR · Bell 214ST · Fuselage Miscellaneous Structure
  > WHILE PERFORMING THE 25HR 7 DAY A CHECK, AIRFRAME & ENG 1 & 2 INSPECTION, A SIGNIFICANT SERIES OF CRACKS WERE DISCOVERED IN THE AFT LT BAGGAGE COMPARTMENT.
- [SDR 9EKA20141119013A](https://openairdocs.org/sdr/9EKA20141119013A.md): Cap · cracked · Nov 19, 2014 · N787SR · Bell 214ST · Fuselage Miscellaneous Structure
  > WHILE PERFORMING THE 25HR 7 DAY A CHECK, AIRFRAME & ENG 1 & 2 INSPECTION, A SIGNIFICANT SERIES OF CRACKS WERE DISCOVERED IN THE AFT LT BAGGAGE COMPARTMENT.
- [SDR 9EKA20141114012](https://openairdocs.org/sdr/9EKA20141114012.md): Pump · failed · Nov 14, 2014 · N214EB · Bell 214ST · Hydraulic Pump (Electric/Engine), Main
  > ON APPROACH, CREW NOTICED LOW PRESS ON NR 2 HYD SYS & THE MASTER CAUTION LIGHT, CONSULTED THE EMER CHECKLIST & SHUTOFF NR 2 HYD SYS. LANDED THE ACFT AT ANOTHER LOCATION.
- [SDR 2014FA0000643](https://openairdocs.org/sdr/2014FA0000643.md): Access Panel · missing · Oct 26, 2014 · N214EB · Bell 214ST · Fuselage Main, Plate/Skin
  > AFTER A ROUTINE MISSION AN ACCESS PANEL LOCATED ON THE AFT PYLON FAIRING ON THE RT SIDE, WAS FOUND NOT INSTALLED ON THE ACFT. THE PANEL IS SECURED AT THE TOP BY A HINGE TO THE AFT PYLON FAIRING. THE HINGE CONSISTS OF 8 SECTIONS ATTACHED TO THE FAIRING AND HAS
- [SDR 9EKA20140809009](https://openairdocs.org/sdr/9EKA20140809009.md): Hydraulic Line · ruptured · Aug 9, 2014 · N214EB · Bell 214ST · Hydraulic System, Main
  > INFLIGHT CREW NOTED NR 1 HYD SYS FAIL LIGHT ILLUMINATED & PROCEEDED TO SHUT DOWN NR 1 SYS. EXECUTED UNEVENTFUL LANDING. VISUALLY FOUND NR 1 HYD SYS PRESSURE LINE PN 70-060T000Y4B4 TO LT CYCLIC SERVO RUPTURED.
- [SDR 9EKA20140516004](https://openairdocs.org/sdr/9EKA20140516004.md): Skin · cracked · May 16, 2014 · N390AL · Bell 214ST · Elevator, Plate/Skin
  > FOUND CRACK IN SKIN OF RT ELEVATOR. CRACK IS LOCATED AT THE AFT INBD BOTTOM SIDE OF THE ELEVATOR, JUST FWD OF THE RIVETS ATTACHING THE TAB.
- [SDR 2013FA0000625](https://openairdocs.org/sdr/2013FA0000625.md): Case · cracked · Nov 1, 2013 · N825H · Bell 214ST · Main Rotor Gearbox
  > DURING INVESTIGATION OF AN OIL LEAK, A CRACK WAS FOUND IN THE MAIN TRANSMISSION UPPER LEFT HAND RING GEAR CASE.
- [SDR 9EKA2013082300003](https://openairdocs.org/sdr/9EKA2013082300003.md): Tab · missing · Aug 23, 2013 · N214EB · Bell 214ST · Main Rotor Blades
  > WHILE CONDUCTING A "POST FLIGHT" INSPECTION, MECHANICS NOTICED THAT ONE OF THE MAIN ROTOR BLADES WAS MISSING A TRIM TAB.
- [SDR 9EKA2013082200002](https://openairdocs.org/sdr/9EKA2013082200002.md): Fitting · cracked · Aug 21, 2013 · N390AL · Bell 214ST · Rotorcraft Tail Boom
  > CRACK ON THE VERTICAL SPAR OF THE TAIL IT IS LOCATED IN THE COLD WORK AREA JUST ABOVE THE OUTPUT QUILL OF THE 42 DEG GEARBOX. LOCATED ON THE LEFT SIDE AT BS 569.689, WL 95 ON FIN STATION 32. CRACK IS.040 DEEP AND 1.1 INCHES LONG.
- [SDR LCFA20130429001](https://openairdocs.org/sdr/LCFA20130429001.md): Tail Boom · cracked · Apr 29, 2013 · N822H · Bell 214ST · Rotorcraft Tail Boom
  > LEFT SIDE OF THE TAIL BOOM CRACKED IMMEDIATELY FORWARD AND BELOW THE FORWARD MOUNT OF THE LEFT VOR ANTENNA. LENGTH OF CRACK IS APPROXIMATELY 20/64" LONG AND EXTENDS FROM THE ANTENNA BASE TOWARD A RIVET NEAR THE AFT EDGE OF A SPLICE BETWEEN THE MAIN TAIL BOOM
- [SDR LCFA2012F00259](https://openairdocs.org/sdr/LCFA2012F00259.md): Bearing Support · broken · Nov 16, 2012 · N787SR · Bell 214ST · Standard Practices/Structures
  > ROD END BEARING, FOUND BROKEN AFTER COMPLETION OF FLIGHT, ON POST INSPECTION.
- [SDR P4YA0713201200001](https://openairdocs.org/sdr/P4YA0713201200001.md): Wire · damaged · Jul 13, 2012 · N391AL · Bell 214ST · Tail Rotor Drive System Wiring
  > 42 DEGREE GEARBOX LIGHT CAME ON AT A TEMP OF 35 DEGREE C AND STAYED ON. MX REPLACED TEMP PROBE AND PRESSURE SWITCH WIRE FROM THE 42 DEGREE GEARBOX TO THE TAILBOOM CONNECTOR AT A/F TO FUSELAGE ATTACH STATION.
- [SDR LCFA2012F00073](https://openairdocs.org/sdr/LCFA2012F00073.md): Attach Fitting · cracked · Apr 11, 2012 · N214EB · Bell 214ST · Rotorcraft Tail Boom
  > WHILE PERFORMING AN URELATED MX WALK-AROUND INSPECTION, NOTED A CRACK ON THE UPPER LT MAIN FUSELAGE TO TAILBOOM ATTACHMENT FITTING. THIS IS A KNOWN ISSUE.
- [SDR 3S8R201108230001](https://openairdocs.org/sdr/3S8R201108230001.md): Frame · cracked · Aug 23, 2011 · N28014 · Bell 214ST · Fuselage Main, Frame
  > MAIN GEAR BOX FRAME HAS A CRACK ON THE LT SIDE RADIUS, STA 227.10, WL 65.00.
- [SDR LCFA20110709001](https://openairdocs.org/sdr/LCFA20110709001.md): Spindle · broken · Jul 9, 2011 · N214EB · Bell 214ST · Main Rotor Gearbox
  > THE TRANSMISSION WAS LIFTED TO FACILITATE CHANGING THE LT TRANSMISSION STOP FITTING. IT WAS NOTICED THAT THE LT NODAL BEAM WAS FREE TO ROTATE ON THE TRANSMISSION SPINDLE. IT WAS DISCOVERED THAT IT WAS NOT THE ELASTOMERIC, BUT THAT THE SPINDLE ASSY HAD CRACK
- [SDR P4YA2011050900001](https://openairdocs.org/sdr/P4YA2011050900001.md): Drive Shaft · cracked · May 9, 2011 · N5748M · Bell 214ST · Tail Rotor Drive Shaft
  > DURING A 25HR CHECK, THE NR 6 TAIL ROTOR DRIVESHAFT MOUNTING FLANGE WAS DISCOVERED CRACKED ON THE OUTPUT SIDE OF THE IGB COUPLING. THE CRACKS ARE AROUND THE BOLT HOLES. THE TRDS IS ON-CONDITION.
- [SDR P4Y2008F00000](https://openairdocs.org/sdr/P4Y2008F00000.md): Skin · cracked · Jun 7, 2008 · N5748M · Bell 214ST · Fuselage Main, Plate/Skin
  > STRUCTURAL DAMAGE TO AC LT SIDE TRANSMISSION AREA CAUSED BY CONTACT WITH FORKLIFT BASE DURING CARGO LOADING OPERATIONS. (K)

Next page: https://openairdocs.org/model/bell-214st/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 = '214ST'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/bell-214st/reports

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