# Service difficulty reports: N113AX

A list on [N113AX](https://openairdocs.org/aircraft/N113AX.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR YADA2023110401](https://openairdocs.org/sdr/YADA2023110401.md): Housing · eroded · Nov 4, 2023 · N113AX · Beech 1900C · Turbine Engine Oil System
  > PILOT REPORTED SEEING OIL ON RH WING DURING PREFLIGHT. MAINTENANCE IDENTIFIED A LEAK FROM A HOLE IN THE RH ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED SAME. THIS IS A COMON ISSUE WITH THESE PUMP HOUSINGS.
- [SDR YADA2023092101](https://openairdocs.org/sdr/YADA2023092101.md): Master Cylinder · failed · Sep 21, 2023 · N113AX · Beech 1900C · Master Cylinder/Brake Valve
  > PILOT REPORTED AFTER LANDING AND DURING TAXI "PILOT SIDE LEFT BRAKE GOES FLAT". MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND THAT THE PILOTS LEFT PEDAL BRAKE MASTER CYLINDER WAS FULLY COMPRESSING CAUSING PEDAL TO GO ALL THE WAY TO THE FLOOR. PILOTS LEFT PE
- [SDR YADA20230313001](https://openairdocs.org/sdr/YADA20230313001.md): Bellcrank · cracked · Mar 11, 2023 · N113AX · Beech 1900C · Elevator Control System
  > WHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.
- [SDR YADA202212164001](https://openairdocs.org/sdr/YADA202212164001.md): Latch · out of adjust · Dec 14, 2022 · N113AX · Beech 1900C · Fuselage Main, Structure
  > PILOT REPORTED SMOKE FROM RT CIRCUIT BREAKER PANEL, NR 2 AVIONICS BREAKER MELTED, COMM 2 AND ADF 1 BREAKERS ALSO SMOKED. AIRCRAFT RETURNED TO AIRPORT OF ORIGIN. PILOT ALSO REPORTED THAT SMOKE ABATED AFTER NR 2 AVIONICS BREAKER PLUNGER POPPED OUT. MAINTENAN
- [SDR YADA20190103001](https://openairdocs.org/sdr/YADA20190103001.md): Scavenge Pump · leaking · Jan 3, 2019 · N113AX · Beech 1900C · Turbine Engine Oil System
  > AFTER LANDING, CREW NOTICED ENGINE OIL ON LT WING. MAINTENANCE LOCATED OIL LEAK AT NR 1 ENGINE OIL SCAVENGE PUMP HOUSING AND REPLACED SAME. REMOVED HOUSING VERIFIED TO HAVE CAVITATION CAVITY THROUGH WALL OF SCAVENGE PUMP BODY THAT WAS ALLOWING OIL TO ESCAPE T
- [SDR YADA20180118001](https://openairdocs.org/sdr/YADA20180118001.md): Scavenge Pump · leaking · Jan 18, 2018 · N113AX · Beech 1900C · Turbine Engine Oil System
  > MAINTENANCE DISCOVERED THAT THE NR 2 ENGINE OIL SCAVENGE PUMP HOUSING WAS LEAKING THROUGH THE CASTING. OIL SCAVENGE PUMP HOUSING WAS REMOVED AND REPLACED.
- [SDR YADA20170926002](https://openairdocs.org/sdr/YADA20170926002.md): Door Frame · cracked · Sep 26, 2017 · N113AX · Beech 1900C · Fuselage Main, Structure
  > WHILE PERFORMING MAINTENANCE INSPECTION DURING A,B,C CHECK FOUND CRACK ON CARGO DOOR FRAME P/N:114-430125-5 AT F.S.: 509.50. CRACK IS 1.6 INCHES LONG AND BEYOND LIMITS. FRAME SECTION WILL BE REPLACED AND DOUBLER INSTALLED.
- [SDR YADA20170926001](https://openairdocs.org/sdr/YADA20170926001.md): Door Frame · cracked · Sep 26, 2017 · N113AX · Beech 1900C · Fuselage Main, Structure
  > WHILE PERFORMING MAINTENANCE INSPECTION DURING A,B,C CHECK FOUND MULTIPLE CRACKS AT AIRSTAIR DOOR FRAME. ONE LOCATED ON FRAME P/N:114-420041-37 AND ONE LOCATED ON AIRSTAIR DOOR CHANNEL P/N:114-420041-41. BOTH CRACKS ARE BEYOND LIMITS AND PARTS WILL BE REPLACED
- [SDR YADA20160109001](https://openairdocs.org/sdr/YADA20160109001.md): Gusset · cracked · Jan 9, 2017 · N113AX · Beech 1900C · Fuselage Miscellaneous Structure
  > DURING MAINTENANCE A,B,C STRUCTURAL INSPECTION, FOUND LT INTERCOSTAL GUSSET CRACKED AT FUSELAGE STATION 107. PART HAS BEEN REMOVED AND REPLACED IAW STRUCTURAL REPAIR MANUAL.
- [SDR YADA20161130001](https://openairdocs.org/sdr/YADA20161130001.md): Windshield · cracked · Nov 29, 2016 · N113AX · Beech 1900C · Flight Compartment Windows
  > LT WINDSHIELD CRACKED INFLIGHT.
- [SDR YADA20161029001](https://openairdocs.org/sdr/YADA20161029001.md): Ground Wire · disconnected · Oct 29, 2016 · N113AX · Beech 1900C · Electrical Power System Wiring
  > DURING DEPARTURE, RECIEVED A BATTERY CHARGE LIGHT THAT DID NOT EXTINGUISH. RETURNED TO DEPARTURE. RECONNECTED BATTERY GROUND TERMINAL AND PERFORMED OPS CHECKED OF BATTERY PASSED.
- [SDR YADA20160815001](https://openairdocs.org/sdr/YADA20160815001.md): Wire · chafed · Aug 15, 2016 · N113AX · Beech 1900C · Fuel System Wiring
  > SMOKE COMING FROM RIGHT WING TIP IN VICINITY OF FUEL VENT, FUEL FOUND ON UNDERSIDE OF WING NEAR HEATED FUEL VENT. MAINTENANCE REPLACED FUEL VENT ON RT WING DUE TO CHAFFING AND SHORTING WIRE ON OLD FUEL VENT.
- [SDR YADA20160611001](https://openairdocs.org/sdr/YADA20160611001.md): Unknown · odor · Jun 11, 2016 · N113AX · Beech 1900C · Air Distribution System
  > WITH LT BLEED AIR OPEN EXHAUST ODOR IN CABIN, MAINTENANCE COULD NOT DUPLICATE ON GROUND RUNS. ACFT GOING INTO CAMP INSPECTION.
- [SDR YADA20160308001](https://openairdocs.org/sdr/YADA20160308001.md): Frame · corroded · Mar 8, 2016 · N113AX · Beech 1900C · Fuselage Main, Frame
  > DURING STRUCTURAL INSPECTION, CORROSION WAS FOUND ON TOP FLANGE OF FUSELAGE FRAME AT FS 468.25. SUSPECT CORROSION WAS CAUSED BY CARGO SPILLAGE. FRAME WAS REPAIRED IAW SRM.
- [SDR YADA20151130001](https://openairdocs.org/sdr/YADA20151130001.md): Uplock Switch · shorted · Nov 30, 2015 · N113AX · Beech 1900C · Landing Gear Position and Warning
  > LANDING GEAR UNSAFE INDICATION, AFTER RETRACTION, RED LIGHT IN HANDLE. ACFT LANDED UNEVENTFULLY AT AIRPORT OF ORIGIN. IDENTIFIED & REPLACED A FAULTY NOSE GEAR UPLOCK INDICATION SWITCH, SWITCH WAS FOUND TO HAVE CONTAMINATION & CORROSION ON TERMINAL CONTACTS U
- [SDR YADA20151009001](https://openairdocs.org/sdr/YADA20151009001.md): Clevis Pin · missing · Oct 9, 2015 · N113AX · Beech 1900C · Landing Gear Brake System
  > PILOT REPORTED COPILOT RT RUDDER PEDAL DISCONNECTED FROM MASTER CYLINDER. REPLACED A MISSING CLEVIS PIN & RELATED COTTER PIN.
- [SDR YADA20150930001](https://openairdocs.org/sdr/YADA20150930001.md): Fan · failed · Sep 30, 2015 · N113AX · Beech 1900C · Air Distribution Fan
  > PIREP SMELL OF ELEC BURNING IN FLIGHT. CREW ELECTED TO RETURN TO DEPARTURE AIRPORT & LANDED WITHOUT INCIDENT. MX VERIFIED THE RECIRCULATION FAN HAD INTERMITTENT GRINDING SOUND & SEIZING, DEFERRED. ACFT RETURNED TO BASE WITHOUT INCIDENT. FAN TO BE REPLACED.
- [SDR YADA20150725001](https://openairdocs.org/sdr/YADA20150725001.md): Warning Light · inoperative · Jul 25, 2015 · N113AX · Beech 1900C · Landing Gear Position and Warning
  > LANDING UNSAFE LIGHT & LANDING POSITION LIGHT INOPERATIVE DURING LANDING. PERFORMED FLYBY & EMERGENCY GEAR EXTENSION IAW QRH. AN UNEVENTFUL LANDING WAS PERFORMED & NO EMERGENCY WAS DECLARED. ALL GEAR DOWN & LOCKED GREEN LIGHTS ILLUMINATED ON ROLLOUT AFTER L
- [SDR YADA20141218001](https://openairdocs.org/sdr/YADA20141218001.md): Hydraulic Line · ruptured · Dec 18, 2014 · N113AX · Beech 1900C · Hydraulic System, Main
  > ON APPROACH FLIGHT CREW SELECTED LANDING GEAR DOWN. THE NOSE GEAR FAILED TO COMPLETELY EXTEND & LOCK, LANDING GEAR PUMP CONTINUED TO RUN. THE PILOT PULLED THE LG CB & THEN THE HYD LOW LEVEL ANNUNCIATOR ILLUMINATED. THE PILOT COMPLETED THE GEAR EXTENSION WIT
- [SDR YADA20140516002](https://openairdocs.org/sdr/YADA20140516002.md): Angle · cracked · May 16, 2014 · N113AX · Beech 1900C · Vertical Stabilizer Miscellaneous Structure
  > CRACK IN VERTICAL STABILIZER FWD SPAR LT ANGLE AT ATTACH BRACKET FASTENER. SEE SB 55-4114 & AD 2013-24-03.
- [SDR YADA20140516001](https://openairdocs.org/sdr/YADA20140516001.md): Angle · cracked · May 16, 2014 · N113AX · Beech 1900C · Vertical Stabilizer Miscellaneous Structure
  > CRACKS IN VERTICAL STABILIZER FWD SPAR RT ANGLE AT BRACKET ATTACH FASTENERS.
- [SDR YADA20140514001](https://openairdocs.org/sdr/YADA20140514001.md): Spar · cracked · May 14, 2014 · N113AX · Beech 1900C · Horizontal Stabilizer, Spar/Rib
  > FOUND CRACKS IN HORIZONTAL STABILIZER AFT CENTER SPAR WEB.
- [SDR YADA2014051700327](https://openairdocs.org/sdr/YADA2014051700327.md): Spar · cracked · May 14, 2014 · N113AX · Beech 1900C · Horizontal Stabilizer, Spar/Rib
  > FOUND CRACKS IN VERTICAL STAB AFT CENTER SPAR WEB.
- [SDR YADA2011F00212](https://openairdocs.org/sdr/YADA2011F00212.md): Line · ruptured · Oct 13, 2011 · N113AX · Beech 1900C · Hydraulic System, Main
  > ON A PREFLIGHT WALK AROUND INSPECTION OF THE ACFT, THE FLIGHT CREW NOTICED A PUDDLE OF HYD FLUID ON THE GROUND AROUND THE RT MLG. HYD FLUID WAS ALSO NOTED ON THE GEAR AND IN THE WHEEL WELL. ARRANGEMENTS WERE MADE AND A FERRY PERMIT ISSUED FOR A FERRY FLIGHT
- [SDR YADA042111](https://openairdocs.org/sdr/YADA042111.md): Relay · stuck · Apr 21, 2011 · N113AX · Beech 1900C · Landing Gear Retraction/Extension System
  > ENROUTE, THE PILOT NOTICED THE LANDING GEAR RELAY CIRCUT BREAKER WAS POPPED. THE FLIGHT CREW ALSO THOUGHT THEY COULD HEAR THE LANDING GEAR PUMP RUNNING BUT WERE UNSURE. AT ONE POINT IN THE FLIGHT THE HYD RESERVOIR LOW LEVEL LIGHT CAME ON BUT LATER EXTINGUISH
- [SDR YADA041511](https://openairdocs.org/sdr/YADA041511.md): Landing Gear · malfunctioned · Apr 15, 2011 · N113AX · Beech 1900C · Landing Gear Retraction/Extension System
  > PILOT REPORTED THAT IN CRUISE, NOTICED THE LANDING GEAR RELAY CIRCUT BREAKER WAS POPPED. SEVERAL ATTEMPTS TO RESET THE CIRCUT BREAKER WERE UNSUCCESSFUL. ON ARRIVAL THE CREW HAD TO MANUALLY EXTEND THE LANDING GEAR. MECHANIC WAS CONTACTED AND INSPECTED THE AC
- [SDR 2010F00251](https://openairdocs.org/sdr/2010F00251.md): Downlock Switch · intermittent · Dec 11, 2010 · N113AX · Beech 1900C · Landing Gear Position and Warning
  > ON APPROACH TO THE AIRPORT, THE GEAR WAS SELECTED DOWN BUT THERE WAS NO INDICATION THE NOSE GEAR WAS DOWN AND LOCKED. THE GEAR WAS CYCLED SEVERAL TIMES AND CYCLED MANUALLY ONCE BUT THERE WAS STILL NO NOSE GEAR DOWN INDICATION. THE ACFT RETURNED TO BASE. ON
- [SDR YADA122908](https://openairdocs.org/sdr/YADA122908.md): Pump · damaged · Dec 29, 2008 · N113AX · Beech 1900C · Fuel Boost Pump
  > ON AN OPS CHECK FLIGHT, PILOT REPORTED LOW PRESSURE FUEL LIGHT ON THE NR 1 ENG, LIGHT WENT OUT WITH AUX PUMP ON. REPLACED PUMP. TEARDOWN OF REMOVED PUMP REVEALED THAT THE PRESSURE CONTROL DIAPHRAGM HAD FAILED POSSIBLY DUE TO AN IMPROPERLY MFG PN RA5361 SPRIN
- [SDR YADA112808](https://openairdocs.org/sdr/YADA112808.md): Boot · shorted · Nov 28, 2008 · N113AX · Beech 1900C · Propeller/Rotor Anti-Ice/De-Ice System
  > OBSERVED SPARKS FROM RT PROP INFLIGHT, SPARKS STOPPED WHEN PROP DEICE WAS TURNED OFF. A/C LANDED UNEVENTFULLY. MAINT REPLACED PROP DUE TO SHORTED DEICE BOOT.
- [SDR YAD2008F00000](https://openairdocs.org/sdr/YAD2008F00000.md): Switch · failed · Jul 11, 2008 · N113AX · Beech 1900C · Landing Gear Position and Warning
  > PILOT REPORTED NOSE GEAR UNSAFE WARNING AFTER VARIOUS ATTEMPTS AT GEAR EXTENSION. GREEN LIGHT CAME ON AT TOUCHDOWN. VERIFIED NOSE GEAR DRAG BRACE SWITCH PLUNGER WAS "STICKY" AND WAS DEFLECTING STRIKER PLATE INSTEAD OF DEPRESSING SWITCH PLUNGER. REPLACED FAI
- [SDR ACE020508](https://openairdocs.org/sdr/ACE020508.md): Tube · split · Feb 5, 2008 · N113AX · Beech 1900C · Tire Tube
  > NOSE TIRE LOOSING AIR AFTER LANDING (BET) REPLACED NOSE TIRE ASSY (FOUND INNER TUBE SPLIT ON SEAM 1/8). THIS IS THE LATEST IN A STRING OF INNER TUBE FAILURES FOR UNDETERMINED REASONS. THIS WAS A CANADIAN MANUFACTURED TUBE AND THE FAILURE SEEMS TO BE AT A D
- [SDR ACE120407](https://openairdocs.org/sdr/ACE120407.md): Tube · failed · Dec 4, 2007 · N113AX · Beech 1900C · Tire Tube
  > PILOT STOPPED AIRCRAFT ON TAXIWAY DUE VIBRATION FROM NOSE TIRE. MAINTENANCE REPLACED FLAT TIRE. INSPECTION OF TIRE AND TUBE IDENTIFIED A NAIL IN TIRE (UNDETERMINED IF THIS WAS CAUSE OF FAILURE) ADDITIONAL INSPECTION OF TUBE INDICATED POSSIBLE PROBLEM WITH T
- [SDR ACE032707](https://openairdocs.org/sdr/ACE032707.md): Stringer · corroded · Mar 25, 2007 · N113AX · Beech 1900C · Fuselage Main, Longeron/Stringer
  > LOCATED CORRODED STRINGER NR 14LH AT FS. 250.
- [SDR ACE02050702](https://openairdocs.org/sdr/ACE02050702.md): Motor · failed · Feb 5, 2007 · N113AX · Beech 1900C · Trailing Edge Flap Control System
  > FLAPS STOPPED AT TAKEOFF. RETRACTED TO UP ON THE GROUND. THE SMELL OF HOT ELECTRICAL WAS STRONG. REPLACED FAILED FLAP MOTOR AND GEAR BOX.
- [SDR ACE0830061](https://openairdocs.org/sdr/ACE0830061.md): Windshield · cracked · Aug 30, 2006 · N113AX · Beech 1900C · Flight Compartment Windows
  > PIREP - ON CLIMBOUT ONE WINDSHIELD SHATTERED AND THEN, FIVE MINUTES LATER, THE OTHER WINDSHIELD SHATTERED. UNEVENTFUL LANDING MADE, CREW VERIFIED ONLY OUTER PLYS WERE CRACKED AND AIRCRAFT RETURNED TO MAINTENANCE BASE FOR WINDSHIELD REPLACEMENTS.
- [SDR ACE0830062](https://openairdocs.org/sdr/ACE0830062.md): Windshield · cracked · Aug 30, 2006 · N113AX · Beech 1900C · Flight Compartment Windows
  > PIREP - ON CLIMBOUT ONE WINDSHIELD SHATTERED AND THEN, FIVE MINUTES LATER, THE OTHER WINDSHIELD SHATTERED. UNEVENTFUL LANDING MADE, CREW VERIFIED ONLY OUTER PLYS WERE CRACKED AND AIRCRAFT RETURNED TO MAINTENANCE BASE FOR WINDSHIELD REPLACEMENTS.
- [SDR ACE04302006](https://openairdocs.org/sdr/ACE04302006.md): Spar Cap · corroded · Apr 30, 2006 · N113AX · Beech 1900C · Wing Spar
  > MAINTENANCE FOUND CORROSION ON FORWARD SPAR LOWER CAP FORWARD FLANGE, IN THE CENTER FUSELAGE BAY, UNDER ORIGINAL SEALANT. REPAIR REQUIRED REMOVAL OF CORROSION AND STRAP DOUBLER PER FR-CO FACTORY REPAIR DESIGN.
- [SDR ACE120105](https://openairdocs.org/sdr/ACE120105.md): Windshield · cracked · Dec 1, 2005 · N113AX · Beech 1900C · Flight Compartment Windows
  > PILOT REPORTED RT FORWARD WINDSHIELD CRACKED. REPLACED CRACKED WINDSHIELD.
- [SDR ACE082605](https://openairdocs.org/sdr/ACE082605.md): Diaphragm · ruptured · Aug 26, 2005 · N113AX · Beech 1900C · Fuel Boost Pump
  > PILOT REPORTED LOW FUEL PRESSURE WARNING LIGHT CAME ON IN FLIGHT. MAINTENANCE REPLACED LEAKING LOW PSI BOOST PUMP. VERIFIED DIAPHRAGM HAD FAILED. FUEL WAS OBSERVED IN AGB AREA.
- [SDR ACE070805](https://openairdocs.org/sdr/ACE070805.md): Fuel Heater · cracked · Jul 8, 2005 · N113AX · Beech 1900C · Fuel Heater
  > MAINTENANCE NOTICED OIL RESIDUE ON ENGINE COWLING. LOCATED ENGINE OIL LEAK AT OIL / FUEL HEATER. REPLACED CRACKED HEATER.
- [SDR ACE052105](https://openairdocs.org/sdr/ACE052105.md): Windshield · cracked · May 21, 2005 · N113AX · Beech 1900C · Flight Compartment Windows
  > PILOT REPORTED LT WINDSHIELD CRACKED ON DESCENT. REPLACED FAILED WINDSHIELD (OUTER PLY FAILED).
- [SDR ACE08282004](https://openairdocs.org/sdr/ACE08282004.md): Stringer Clip · missing · Aug 28, 2004 · N113AX · Beech 1900C · Fuselage Main, Attach Fittings
  > DURING SCHEDULED STRUCTURAL INSPECTION OF THE AREA, FOUND STRINGER CLIP PN. 114-430066-5 NEVER INSTALLED AND THE BULKHEAD AT FS 363.25 HAD CRACKS IN THE FLANGE ABOVE AND BELOW THE MISSING CLIP LOCATION.
- [SDR ACE082304](https://openairdocs.org/sdr/ACE082304.md): Limit Switch · out of adjust · Aug 23, 2004 · N113AX · Beech 1900C · Landing Gear Position and Warning
  > PILOT REPORTED LANDING GEAR HANDLE WARNING LIGHTS REMAINED ON AFTER GEAR WAS RETRACTED. CREW RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING. MAINTENANCE ADJUSTED THE NOSE LANDING GEAR UP LIMIT SWITCH FOR PROPER OPERATION.
- [SDR ACE071204](https://openairdocs.org/sdr/ACE071204.md): Skin · corroded · Jul 12, 2004 · N113AX · Beech 1900C · Fuselage Main, Plate/Skin
  > MAINTENANCE OBSERVED DEFORMATION OF FUSELAGE SKIN AT LAP JOINTS AT STATIONS 348.25 & 430.75 UNDER STRINGER 16. REPAIRS MADE INCLUDED REMOVAL OF EXFOLIATED SHIMS AND FAILED BONDING AGENT. PREVIOUS REPAIRS OF THIS TYPE AND ON THIS MODEL HAVE DISCLOSED PRIOR US
- [SDR ACE062804](https://openairdocs.org/sdr/ACE062804.md): Windshield · cracked · Jun 28, 2004 · N113AX · Beech 1900C · Flight Compartment Windows
  > PILOT REPORTED LEFT WINDSHIELD CRACKED ONE HALF HOUR INTO FLIGHT. RETURNED TO ORIGINAL AIRPORT.
- [SDR ACE112503](https://openairdocs.org/sdr/ACE112503.md): Warning System · malfunctioned · Nov 25, 2003 · N113AX · Beech 1900C · Landing Gear Position and Warning
  > NOSE GEAR FAILED TO SHOW DOWN AND LOCKED UNTIL GEAR WAS CYCLED TWICE. MAINTENANCE COULD NOT DUPLICATE FAULT.
- [SDR 113AX62603](https://openairdocs.org/sdr/113AX62603.md): Intercostal · cracked · Jun 26, 2003 · N113AX · Beech 1900C · Fuselage Miscellaneous Structure
  > WHILE C/W STRUCTURAL INSPECTION 53-10-02, FOUND.5 INCH CRACK IN OUTER FLANGE RADIUS OF INTERCOSTAL PN 114-430116-7 AT STATION NR 498.25 AND ADJACENT TO THE CARGO DOOR AFT UPPER GAS STRUT ATTACH BRACKET MOUNTED TO THE DOOR FRAME.
- [SDR ACE0531021](https://openairdocs.org/sdr/ACE0531021.md): Control Cable · broken · Jun 3, 2002 · N113AX · Beech 1900C · Elevator Control System
  > PILOT ATTEMPTED TO ADJUST ELEVATOR TRIM TO REDUCE CONTROL FORCES AND NOTICED THAT TRIM SYS DID NOT FEEL LIKE IT WAS WORKING NORMAL. AFTER UNEVENTFUL LANDING, PILOT ATTEMPTED TO ADJUST ELEVATOR TRIM, NOTED THAT TRIM WHEEL STARTED TO BIND. BROKEN UPPER ELEVAT

## 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 n_number = 'N113AX' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N113AX/reports

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