N113AX
Service difficulty reports · 48
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 = 'N113AX' 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 = 'N113AX' 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 YADA2023110401Housing · erodedPILOT 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 YADA2023092101Master Cylinder · failedPILOT 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 PESDR YADA20230313001Bellcrank · crackedWHILE PERFORMING A COMPANY FLEET CAMPAIGN DISCOVERED FORWARD ELEVATOR BELLCRANK CRACKED WEB.SDR YADA202212164001Latch · out of adjustPILOT 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. MAINTENANSDR YADA20190103001Scavenge Pump · leakingAFTER 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 TSDR YADA20180118001Scavenge Pump · leakingMAINTENANCE DISCOVERED THAT THE NR 2 ENGINE OIL SCAVENGE PUMP HOUSING WAS LEAKING THROUGH THE CASTING. OIL SCAVENGE PUMP HOUSING WAS REMOVED AND REPLACED.SDR YADA20170926002Door Frame · crackedWHILE 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 YADA20170926001Door Frame · crackedWHILE 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 REPLACEDSDR YADA20160109001Gusset · crackedDURING 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 YADA20161130001Windshield · crackedLT WINDSHIELD CRACKED INFLIGHT.SDR YADA20161029001Ground Wire · disconnectedDURING 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 YADA20160815001Wire · chafedSMOKE 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 YADA20160611001Unknown · odorWITH LT BLEED AIR OPEN EXHAUST ODOR IN CABIN, MAINTENANCE COULD NOT DUPLICATE ON GROUND RUNS. ACFT GOING INTO CAMP INSPECTION.SDR YADA20160308001Frame · corrodedDURING 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 YADA20151130001Uplock Switch · shortedLANDING 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 USDR YADA20151009001Clevis Pin · missingPILOT REPORTED COPILOT RT RUDDER PEDAL DISCONNECTED FROM MASTER CYLINDER. REPLACED A MISSING CLEVIS PIN & RELATED COTTER PIN.SDR YADA20150930001Fan · failedPIREP 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 YADA20150725001Warning Light · inoperativeLANDING 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 LSDR YADA20141218001Hydraulic Line · rupturedON 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 WITSDR YADA20140516002Angle · crackedCRACK IN VERTICAL STABILIZER FWD SPAR LT ANGLE AT ATTACH BRACKET FASTENER. SEE SB 55-4114 & AD 2013-24-03.SDR YADA20140516001Angle · crackedCRACKS IN VERTICAL STABILIZER FWD SPAR RT ANGLE AT BRACKET ATTACH FASTENERS.SDR YADA20140514001Spar · crackedFOUND CRACKS IN HORIZONTAL STABILIZER AFT CENTER SPAR WEB.SDR YADA2014051700327Spar · crackedFOUND CRACKS IN VERTICAL STAB AFT CENTER SPAR WEB.SDR YADA2011F00212Line · rupturedON 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 YADA042111Relay · stuckENROUTE, 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 EXTINGUISHSDR YADA041511Landing Gear · malfunctionedPILOT 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 ACSDR 2010F00251Downlock Switch · intermittentON 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 YADA122908Pump · damagedON 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 SPRINSDR YADA112808Boot · shortedOBSERVED 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 YAD2008F00000Switch · failedPILOT 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 FAISDR ACE020508Tube · splitNOSE 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 DSDR ACE120407Tube · failedPILOT 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 TSDR ACE032707Stringer · corrodedLOCATED CORRODED STRINGER NR 14LH AT FS. 250.SDR ACE02050702Motor · failedFLAPS STOPPED AT TAKEOFF. RETRACTED TO UP ON THE GROUND. THE SMELL OF HOT ELECTRICAL WAS STRONG. REPLACED FAILED FLAP MOTOR AND GEAR BOX.SDR ACE0830061Windshield · crackedPIREP - 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 ACE0830062Windshield · crackedPIREP - 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 ACE04302006Spar Cap · corrodedMAINTENANCE 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 ACE120105Windshield · crackedPILOT REPORTED RT FORWARD WINDSHIELD CRACKED. REPLACED CRACKED WINDSHIELD.SDR ACE082605Diaphragm · rupturedPILOT 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 ACE070805Fuel Heater · crackedMAINTENANCE NOTICED OIL RESIDUE ON ENGINE COWLING. LOCATED ENGINE OIL LEAK AT OIL / FUEL HEATER. REPLACED CRACKED HEATER.SDR ACE052105Windshield · crackedPILOT REPORTED LT WINDSHIELD CRACKED ON DESCENT. REPLACED FAILED WINDSHIELD (OUTER PLY FAILED).SDR ACE08282004Stringer Clip · missingDURING 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 ACE082304Limit Switch · out of adjustPILOT 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 ACE071204Skin · corrodedMAINTENANCE 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 USSDR ACE062804Windshield · crackedPILOT REPORTED LEFT WINDSHIELD CRACKED ONE HALF HOUR INTO FLIGHT. RETURNED TO ORIGINAL AIRPORT.SDR ACE112503Warning System · malfunctionedNOSE GEAR FAILED TO SHOW DOWN AND LOCKED UNTIL GEAR WAS CYCLED TWICE. MAINTENANCE COULD NOT DUPLICATE FAULT.SDR 113AX62603Intercostal · crackedWHILE 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 ACE0531021Control Cable · brokenPILOT 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
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