N231YV
Service difficulty reports · 90
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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 = 'N231YV' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'N231YV' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR GLBA20100104FSkin · crackedMAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND IN THE UPPER FUSELAGE DOME SKIN AT FAS 150. CRACK IS APPROX.3" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED THE REQUIRED RII INSPECTIONS IAW EO 09-120-53-040. MATERIALS UTLIZED ARE LISTEDSDR GLBA200912211ASwitch · deterioratedUPON APPROACH THE PILOTS REPORTED THAT THE LANDING GEAR WOULD NOT COME DOWN. THEY PERFORMED CHECKLISTS AND HAND PUMPED THE GEAR DOWN. ALL 3 GREEN ANNUNCIATORS ILLUMINATED. MX REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW MM 31-10-00-201 SECTION 5SDR GLBA200911221Indicator · inoperativeUPON APPLICATION OF TAKEOFF POWER ON RUNWAY, THE NR 2 PROP GAUGE WENT TO ZERO.SDR GLBA20091009FDisplay · failedAIR RETURN - PILOTS REPORTED THE CAPTAINS EHSI WENT OUT FOLLOWED BY SMOKE IN THE COCKPIT. TURNING THE PILOTS SIDE SCREENS OFF STOPPED THE SMOKE. IT APPEARED TO THE PILOTS THAT THE CAPTAINS SIDE MIC (HEADSET) WAS LOSING IT'S EFFECTIVENESS AS WELL. OPENSDR GLBA200910051Wire · chafedAIR RETURN - PILOTS REPORTED THE LANDING GEAR RELAY POPPED AND A MANUAL GEAR EXTENSION WAS PERFORMED. MAINTENANCE REPAIRED A BROKEN WIRE AT THE THE HYDRAULIC POWER PACK SHUTTLE VALVE IAW MM 20-13-00. MAINTENANCE PERFORMED A GEAR RETRACTION AND EXTENSION TEST SDR GLBA200908191Powerpack · failedPILOTS REPORTED THAT THE GEAR HANDLE DID NOT OPERATE THE GEAR AND WOULD NOT EXTEND. A MANUAL EXTENSION OF GEAR WAS PERFORMED. MX REMOVED AND REPLACEDTHE LANDING GEAR PWR PACK ASSY AND OPS CHECKED THROUGH SEVERAL GEAR EXTENSIONS AND RETRACTIONS IAW MM 32-30-SDR GLBA20090227AAltimeter · inoperativeFLIGHT 5096 - PILOTS REPORTED THAT THE FIRST OFFICERS ALTIMETER WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS ALTIMETER IAW MM 31-10-00. PERFORMED ENCODER CHECK WHICH OPERATIONALLY CHECKED GOOD IAW FAR 43 APPENDIX (E) (A) & (C) (A). MAISDR GLBA200812172Seat Track · crackedMAJOR REPAIR - LT CENTER SEAT TRACK SUPPORT TAB IS BROKEN OFF FROM SEAT TRACK AT F.S. 187.5 TO 190.5. MAINTENANCE REPAIRED LEFT CENTER SEAT TRACK SUPPORT TAB AT APPROXIMATELY F.S. 189 TO 191 IAW SRM 53-90. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.SDR GLBA200812171Seat Track · crackedMAJOR REPAIR - LT CENTER SEAT TRACK SUPPORT TAB IS BROKEN OFF FROM SEAT TRACK AT F.S.160 TO F.S. 164. MAINTENANCE REPAIRED THE LEFT HAND CENTER SEAT TRACK SUPPORT TAB AT F.S. 162 TO F.S. 164 IAW SRM 53-90. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.SDR GLBA200812151Skin · crackedMAJOR REPAIR - DURING CONFORMITY INSPECTIONS MX DISCOVERED THE FUSELAGE SKIN ON THE LT SIDE OF THE NR 2 COMM ANTENNA TO BE CRACKED APPROXIMATELY 2.5 " IN LENGTH AT F.S. 393.25. MAINTENANCE REPAIRED CRACK ON FUSELAGE SKIN UNDER NR 2 COMM ANTENNA IAW E.O. 03-17SDR GLBA200812113Spar · crackedMAJOR REPAIR HORIZONTAL STABILIZER SPAR WEB CRACKED APPROXIMATELY .250" IN LENGTH. MAINTENANCE REPAIRED HORIZONTAL STABILIZER MAIN SPAR WEB IAW BEECH 1900D SRM 55-91. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.SDR GUU2008F00032Unknown · odorFLIGHT 5406 PBI/FLL. DURING FLIGHT LIGHT FUEL ODOR INSIDE ACFT. INSPECTED FUEL AUX TANKS. RAN ENGS WITH BLEEDS OPEN. NO FUEL ODOR DETECTED. (S)SDR GUU2008F00029Unknown · odorFLIGHT 5406 PBI/FLL, DURING FLIGHT LIGHT FUEL ODOR INSIDE ACFT. INSPECTED FUEL AUX TANKS, RAN ENGS WITH BLEEDS OPEN. NO FUEL ODOR DETECTED. (S)SDR GUUA04260801Wire · shortedFLIGHT: 9275, DURING APPROACH LANDING GEAR WOULD NOT COME DOWN, CIRCUIT BREAKER POPPED. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. REPAIRED SHORTED WIRE G15F22 ON CABIN SIDEWALL NEAR MAIN DOOR. OPERATIONAL CHECK GOOD NO DEFECTS NOTED.SDR GUUA04250801Wire · chafedFLIGHT: 5401, AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. LANDING GEAR CIRCUIT BREAKER POPPED, UNABLE TO RESET. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. REPAIRED CHAFED WIRE G15C22 AT LT WING ROOT. OPS CHECK NORMAL.SDR GUUA04240801Control Switch · inoperativeFLIGHT: 9280, DOING A GO AROUND, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION UNLESS THE DOWN LOCK RELEASE SWITCH WAS USED, THE GEAR FAILED TO RETRACT WITH THE HANDLE IN THE UP POSITION, LANDING GEAR CIRCUIT BREAKER POPPED. REPLACED LANDING GEAR SDR GUUA04160801Longeron · crackedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED TWO INCH CRACK ON COCKPIT RIGHT UPPER LONGERON AT FS 107.0 AND WL 119.0. REMOVED DAMAGED SECTION OF LONGERON AND INSTALLED FILLER PROFILE TO MATCH REMOVED SECTION OF LONGERON. FABRICATED AND INSTALLED REINFORCESDR GUUA04040803Control Column · obstructedFLT NR 9188, ON FINAL APPROACH CONTROL COLUMN JAMMED. REQUIRED STRENGTH OF BOTH CREW MEMBERS TO OVER COME. MAINT DETERMINED THAT A WIRE BUNDLE FROM UNDER AND FWD OF THE INSTRUMENT PANEL WAS INTERFERING WITH THE CONTROL COLUMN. THE WIRE BUNDLE WAS POSITIONESDR GUUA02100801Bleed Air Sys · contaminatedFLIGHT: 5401, DURING FLIGHT, FUNKY SMOKE ODOR IN THE COCKPIT WITH BLEED OPEN. CLEANED RESIDUAL OIL, FROM OIL SERVICING.SDR GUUA01050802Hinge Bracket · corrodedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OB HINGE BRACKET.SDR GUUA01050801Hinge Bracket · corrodedDURING SCHEDULED ROUTINE INSPECTION DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOILATED. REPLACED RT ELEVATOR CTR HINGE BRACKET.SDR GUUA10240701Contact · dirtyFLIGHT: 9188, DURING LANDING NOSE LANDING GEAR ANNUNCIATOR FAILED TO ILLUMINATE. CLEANED ANNUNCIATOR CONTACTS. OPERATIONAL CHECK GOOD.SDR GUUA07090701Powerpack · defectiveFLIGHT: 9174, AFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR POWER PACK MOTOR. LANDING GEAR OPERATIONAL CHECK NORMAL.SDR GUUA06150701Wire · looseFLIGHT: 9278, DURING FLIGHT, RT DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY. CONTINUED TO DESTINATION, LANDED WITHOUT INCIDENT. SECURED LOOSE WIRE AT THE RT FIRE BOTTLE.SDR GUUA04230702Unknown · odorFLIGHT: 9308 MIA/EYW - DURING APPROACH ODOR IN COCKPIT. PERFORMED ENGINE RUN WITH CAPTAIN CHECK BLEED SYSTEM ALL ELECTRICAL ON, CHECKED OIL AND BRAKE FLUID NO ODORS AT THIS TIME.SDR GUUA08300601Acm · odorFLIGHT:9265 PBI/MHH DURING FLIGHT SMELLED BURNING IN THE AIRCRAFT. DIVERTED TO FPO LANDED WITHOUT INCIDENT. FOUND ACM BLOWING FULL HOT CAUSING AIR CONDITION DUCTS AND PLASTIC VENTS TO EMIT BURNING SMELL FROM UNDER FLOOR VENTS. REPLACED ACM OPERATIONAL CHECKSDR GUU2005F00045Connector · looseFLT - 9292 - JAX/TPA - AFTER TAKEOFF, WHILE ADJUSTING THE ELEVATOR TRIM FROM CLIMB TO LEVEL FLIGHT, THE YOKE WAS PULLED AWAY FROM THE FIRST OFFICERS HANDS. IT WAS IF THE TRIMMING CABLE SNAPPED INTO A NEW POSITION. DETERMINED BACK SHELL WIRE BUNDLE CLAMP EAR SDR 64696Wire · chafedWHILE TAXING FOR TAKEOFF CREW NOTED ARCING BY F/O'S DEFROST HANDLE AND RETURNED TO GATE. REPAIRED CHAFED WIRES AND REPOSITIONED AS NEEDED.SDR 58501Solenoid · dirtyON TAKEOFF ROLL IN TAMPA FLORIDA ON FLIGHT 5536, THE LT ENGINE POWER LEVER FULL FORWARD WOULD ONLY GO TO 2000 LBS OF TORQUE AND 1500 PROP RPM. THE CREW ABORTED THE TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE CLEANED AND LUBED THE LOW PSDR 52532Switch · out of adjustON FLIGHT 9415 FROM PANAMA CITY FLORIDA TO PENSACOLA FLORIDA, AFTER TAKEOFF FROM PANAMA CITY FLORIDA, THE STALL WARNING WENT OFF AND WOULD NOT SILENCE. THE AIRCRAFT RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE RE-ADJUSTED THE SWITCHES. NO PARTS WSDR AMWA9Spar Cap · chafedUPON A SERVICE INSPECTION MAINTENANCE FOUND THE LEFT AND RIGHT LOWER SPAR CAP BEHIND THE NACELLE INNER FEN WAS CHAFED. BLENDED, ALODINED AND PRIMED BOTH OF THE LOWER WING SPAR CAP IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. REFERENCE NUMBER JV/0215-03. NO TEARDSDR 044616Wire · failedUPON LANDING IN PITTSBURGH, THE CREW REPORTED THAT THE NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE IN GEAR DOWN POSITION. THE BULB WAS THEN CHECKED WHICH WAS FOUND TO BE OKAY. THE CREW MANUALLY LOWERED THE GEAR PER THE CHECKLIST. THEN THEY DECLARED AN EMERGENCY LSDR AMWA044616Actuator · failedUPON LANDING, FLIGHT 5533, THE CREW REPORTED THAT THE NOSE GEAR ANNUNCIATOR DID NOT ILLUMINATE IN GEAR DOWN POSITION. THE BULB WAS THEN CHECKED WHICH WAS FOUND TO BE OKAY. THE CREW MANUALLY LOWERED THE GEAR PER THE CHECKLIST. THEN DECLARED AN EMERGENCY LANDSDR AMW2002F00004Switch · dirtyDURING THE INITIAL CLIMB, THE CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CREW THEN RETURNED TO THE FIELD WITHOUT ANY FURTHER INCIDENT. NO TEARDOWN REPORT IS REQUIRED. THE CORRECTIVE ACTION WAS THAT THE DOOR SWITCH WAS CLEANED.SDR 98ZZZM894Skin · crackedOVERNIGHT MAINTENANCE IN ICT, FOUND A .5 INCH CRACK EXTENDING FROM A RIVET ON THE RT INBOARD FLAP DOVETAIL. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)SDR 97ZZZX4240Brackets · wornDURING BEECH TEMP. REV. 5-6, INSPECTION FOUND LEFT OUTBOARD FLAP ATTACHING BRACKETS WORN. REPLACED BRACKETS IAW T.O. 1900-27-00-0001 AND ADDED DOUBLER IAW T.O. 1900-27-50-0001. (X)SDR 97ZZZX4234Dovetail Blkhd · crackedDURING BEECH TEMP. REV. 5-6 INSPECTION, FOUND DOVETAIL BULKHEAD HAD 2 CRACKS. ONE CRACK IS 2 INCHES LONG, 12 INCHES FROM OUTBOARD EDGE. THE OTHER IS .50 INCH, 22 INCHES FROM OUTBOARD EDGE. STOP-DRILLED CRACKS. REPAIRED IAW AMWA TO 1900-27-00-0001. (X)SDR 97ZZZM979Bulkhead · crackedDURING BEECH TEMP REV 5-6, INSPECTION FOUND THAT THE DOVETAIL BULKHEAD WAS CRACKED, IT WAS PATCHED IAW AMWA TO 1900-27-00-0001.SDR 97ZZZM658Flap · crackedDURING ROUTINE INSPECTION, RIGHT INBOARD FLAP WAS FOUND TO HAVE A 2.2 INCH CRACK ON THE TRAILING EDGE. REPAIRED IAW SRM AND AMW. (M)SDR 97ZZZX2055Actuator Switch · failedWHEN CREW SELECTED GEAR DOWN ON APPROACH TO ICT, THE NOSE GEAR DID NOT SHOW DOWN AND LOCKED. CREW LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE INDICATION SWITCH HAD FAILED. ACTUATOR WAS REMOVED AND REPLACED. AIRCRAFT WAS RETURNED TO SERVICE.
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