N14125
Service difficulty reports · 100
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 = 'N14125' 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 = 'N14125' 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 RAIA201707220001Warning Light · false activationCARGO DOOR OPEN INDIDCATION DURING FLIGHT. PERFORMED OPS CHECK OF THE CARGO DOOR WARNING SYSTEM, OPS CHECKED GOOD.SDR RAIA201704070001Battery Pack · inoperativeLT AND RT OVERWING EMERGENCY LIGHTS NR 5 & 6, INOPERATIVE. R & R THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPS CHECKED GOOD.SDR RAIA201702160001Switch · failedON ROTATION, LOST MFD1, PFD2, NR 2 FMS DISPLAY, AND NR 2 COMMS. AFTER RUNNING THE CHECKLIST, FOUND THE NR 2 AVIONICS MASTER SWITCH HAD TRIPPED. R & R THE NR 2 AVIONIC MASTER SWITCH. OPS CHECKED GOOD.SDR RAIA201608260002Anti-Ice Valve · inoperativeANTI-ICE INOPERATIVE IN ICING CONDITIONS, FOLLOWED BY SPS/ICE SPEEDS. INSPECTED AND FOUND NR 2 ENG ANTI-ICE VALVE TO BE INTERNALLY DAMAGED NOT ALLOWING PROPER FLOW OF AIR INTO BLEED SYS. REMOVED AND REPLACED ANIT-ICE VALVE OPS CHECK GOOD.SDR RAIA201606260001Warning System · activatedENGINE 2 REVISED FAIL EICAS MSG, NO THRUST ON ENGINE NR 2, IDLE POWER ONLY, SINGLE ENGINE APPROACH AND LANDING. DEFERRED IAW MEL 78-30-00 CAT C.SDR RAIA201606160001Door Seal · out of adjustBAG DOOR OPEN INDICATION IN FLIGHT. CLEANED AND ADJUSTED DOOR VENT DOOR SEAL AND CLEANED MICROSWITCHES. OPS CHECK GOOD.SDR RAIA201605110003Warning Light · activatedBAGGAGE DOOR OPEN INDICATION IN FLIGHT.SDR RAIA201604220001Switch · inoperativeENGINE 2 REVERSER FAIL ON EICAS. R & R THRUST REVERSER TRANSIT SWITCHES. OPS CHECK GOOD.SDR RAIA201603240001Fadec · malfunctionedENGINE THRUST REVERSER FAIL EICAS MSG DURING CRUISE, EMERGENCY LANDING. R & R FADEC 2A. OPS CHECK GOOD.SDR ASOA20150723025Lamp · burnedACFT WAS CRUISING, WHEN A BURNING ODOR OCCURRED ABOVE SEAT 11A. ACFT LANDED WITHOUT INCIDENT AFER ALL OVERHEAD LIGHTS WERE TURNED OFF. ACFT WAS THEN FERRIED, WHERE MAINTENANCE RELAMPED SIDEWALL LIGHT AT SEAT 11A IAW AMM 33-21-06 AND OPS CHECKED GOOD AND NO OSDR ASOA20150714150Yoke · crackedDURING C-CHECK, THE RT ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01160. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150714149Frame · crackedDURING C-CHECK, THE RT FRAME 10 WAS FOUND TO BE CRACKED BETWEEN STR 9R-10R. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150714148Frame · crackedDURING C-CHECK, THE LT FRAME 10 WAS FOUND TO BE CRACKED BETWEEN STRINGERS 9-10L. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20141215101Ballast · faultyTHE CREW REPORTED ELECTRICAL ODOR FROM ROWS 4 AND 5. MAINTENANCE INSPECTED AND REPLACED THE LIGHT BALLASTS. OPS CHECKED GOOD.SDR ASOA20141214100CWire Harness · faultyTHE CREW REPORTED, AN ODOR AROUND SEAT 4A AND 5A. MAINTENANCE INSPECTED AND REPLACED THE SIDE WALL LIGHT HARNESS ASSEMBLY. OPS CHECKS WERE GOOD.SDR ASOA20140414044Target · out of adjustLANDING GEAR AIR/GROUND FAILED AND TRUST REVERSER DISAGREE AFTER TAKEOFF. ADJUSTED NLG WOW SWITCH TARGET IAW AMM 32-63-05. OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20130801059Connector · looseDURING ROUTINE MX, THE EMERGENCY EXIT ROW SIGNS WERE FOUND INOPERATIVE. MX RECONNECTED THE NR 3 EMERGENCY LIGHT BATTERY CHARGER CONNECTOR P8031. OPS CHECKED GOOD.SDR ASOA20130702182Fitting · damagedDURING C-CHECK. LT AILERON PCA ATTACHMENT BRACKET HAS MIGRATED HAT BUSHING. R & R LT AILERON PCA FITTING IAW EC5750-01177. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130702181Beam · corrodedDURING C-CHECK, CARGO DOOR LOWER BEAM CORRODED. R & R CARGO DOOR LOWER BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130630180VFloor Support · corrodedDURING C-CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MX R & R THE OMEGA BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130630179Sill · corrodedDURING C-CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED AT FRAMES 20-22 AND STRINGERS 15-16R. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130630178Fitting · corrodedDURING C-CHECK THE FRAME 75 FITTING AT STRINGER 1R (12:00 POSITION) WAS FOUND TO HAVE FRETTING CORROSION BETWEEN THE FITTING AND SKIN. MX REMOVED THE CORROSION AND PERFORMED THE REPAIR IAW EC5310-01317, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130409034Cradle · damagedCREW REPORTED FORWARD CABIN FLASHLIGHT NOT CHARGING. R & R THE FORWARD CABIN FLASHLIGHT CRADLE ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130213015HEngine · smokeAFTER TAKEOFF THE CREW REPORTED A LAVATORY SMOKE INDICATION IN FLIGHT. THE ACFT RETURNED AND LANDED WHERE MX DETERMINED THE SOURCE OF THE SMOKE TO BE THE NR 2 ENGINE. THE ACFT WAS FLOWN UNDER A SPECIAL FLIGHT PERMIT TO WHERE THE NR 2 ENGINE WAS REPLACED, ENGSDR ASOA20130103001Inverter · inoperativeDURING ROUTINE MX, THE LT EMERGENCY EXIT SHROUD LIGHT AND OVERWING EMERGENCY CEILING EXIT SIGN WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.SDR ASOA20121001129Unknown · odorCREW REPORTED A BURNING ODOR IN THE COCKPIT AND CABIN AFTER TAKEOFF. THE ACFT LANDED WITHOUT INCIDENT, MX INSPECTED THE ACFT, COMPLIED WITH FIM, ALL WITH NO DEFECTS NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120410056Engine · leakingAFTER TAKEOFF THE CREW REPORTED SMOKE BEGAN TO FILL CABIN AFTER SELECTING ENGINE BLEED AIR ON TAKEOFF. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND R & R THE NR 1 ENGINE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS SDR C2XA11SH097Warning System · malfunctionedSHV - ABORTED TAKEOFF AT 60 KTS DUE TO FO DV WINDOW YELLOW TAB SHOWING UNLOCKED. PERFORMED OPERATIONAL CHECK OF F/O DV WINDOW IAW EMB 145 AMM 56-11-00. OPS CHECK GOOD. DV WINDOW VERIFIED CLOSED AND LOCKED.SDR C2XA11RI046Valve · inoperativeFLIGHT 3009 - EWR - FLIGHT CREW REPORTED THAT AFTER T/O FUEL INDICATOR ON NR 2 SIDE DECREASING AT HIGH RATE. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED RT WING FLAP VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFTSDR C2XA10CL159Duct · leakingCLE FLT 2197 THE CREW REPORTED A NR 2 BLEED LEAK MESSAGE ON THE EICAS CLIMBING THRU 17000. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED DUCT FROM THE PRE-COOLER TO BLEED VALVE. OPERATIONAL CHECKS WERSDR C2XA10IA167Proximity Sensor · inoperativeIAH - FLIGHT 2857, THE CREW REPORTED A AN SPS ADVANCE WARNING INDICATION DURING ALL PHASES OF FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT DOWNLOCK PROXIMITY SWITCH, OPERATIONALLY TESTED WITSDR C2XA09SH430Skin · crackedSHV - DURING C-CHECK (ZONE - 311) EXTERNAL SKIN AT FRAME 80, HAS (2) SKIN CRACKS AT RIVETS (.031" & .046"). MAINTENANCE REPAIRED (ZONE-311) EXTERNAL SKIN @ FRAME 80 (2) IAW EC5330-02012. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH429Skin · crackedSHV - DURING C-CHECK (ZONE - 311) EXTERNAL SKIN AT FRAME 79, HAS (5) SKIN CRACKS AT RIVETS (.059", .074", .061", .046" AND .017'). MAINTENANCE PERFORMED REPAIR ON ZONE 311 EXTERNAL SKIN AT FRAME 79 (5) PLACES IAW EC 5330-02012. THE AIRCRAFT WAS APPROVED FOR SDR C2XA09SH428Skin · crackedSHV - DURING C-CHECK (ZONE-311) SKIN AT FRAME 78, HAS CRACKED SKIN AT RIVET (.054"). MAINTENANCE PERFORMED REPAIR ON ZONE-311 FUSELAGE EXTERNAL SKIN AT FRAME 78 IAW EC5330-02012. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH427Skin · crackedSHV - DURING C-CHECK (ZONE-311) EXTERNAL SKIN AT FRAME 77, HAS (2) SKIN CRACKS AT RIVETS (.081" & .043"). MAINTENANCE PERFORMED REPAIR OF ON ZONE-311 FUSELAGE EXTERNAL SKIN FRAME 77 IAW EC5330-02012. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH426Sill · corrodedSHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORROSION (LEVEL 1 LOCAL). MAINTENANCE REPAIRED CENTER SERVICE DOOR FLOOR SILL IAW EMB-145XR SRM 53-21-02 AND CPM 51-21-04/05/06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09SH425Floor Support · corrodedSHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION (LEVEL 3 LOCAL) AT LIGHTENING HOLES BETWEEN FRAMES 49-50. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM BETWEEN FRAMES 49-50 IAW EMB-145XR EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09IA256Battery · overtempIAH - FLIGHT 2160, THE CREW REPORTED A BATTERY ONE OVERTEMP PEAKING AT 83 DEGREES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCSDR C2XA09IA142Garlock Seal · leakingVPS - FLIGHT 2408 - DURING CRUISE THE CREW REPORTED AN E1 LOW OIL PRESSURE MESSAGE. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION, AND DIVERTED TO VPS WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND SDR C2XA09IA139Controller · malfunctionedIAH - FLIGHT 2916 - THE CREW REPORTED A RAPID DECOMPRESSION AT FL360, AND THAT THE CABIN ALT REACHED 13000FT, THE AIRCRAFT LANDED AT TUL WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND THE AIRCRAFT WAS FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDSDR C2XA09IA138Outflow Valve · malfunctionedFLIGHT 2916 - THE CREW REPORTED A RAPID DECOMPRESSION AT FL360, AND THAT THE CABIN ALT REACHED 13000FT. THE AIRCRAFT LANDED AT TUL WITHOUT INCIDENT WHERE MX INSPECTED ACFT, R & R THE PNEUMATIC OUTFLOW VALVE, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RSDR C2XA09TY103Outflow Valve · defectiveTYS - AIRCRAFT EN ROUTE FROM CLT TO IAH WHEN THE AUTO PRESSURE SYSTEM FAIL INFLIGHT. AIRCRAFT DIVERTED BACK TO CLT AND WAS MEL (169978). IAH - MAINTENANCE REMOVED AND REPLACED THE ELECTRO PNEUMATIC OUTFLOW VALVE IAW EMB 145XR MM 21-31-03. OPS CHECK GOOD ANDSDR C2XA09IA112Unknown · odorIAH - FLIGHT 3133, THE CREW REPORTED A BURNING SMELL INTERMITTENTLY EN ROUTE, AND ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT CABIN AND COCKPIT FOR A BURNING SMELL WITH NO DEFECTS NOTED. THE AIRCRAFT WAS SDR C2XA09IA041Bleed Valve · inoperativeIAH - FLIGHT 2099, THE CREW REPORTED THAT THE APU BLEED VALVE WAS STUCK OPEN DURING CLIMB. THE ACFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MX R&R THE APU BLEED VALVE, OPS TESTED WITH NO DEFECTS. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA07IA021Unknown · smokeIAH - DURING POST-FLIGHT INSPECTION THE CREW REPORTED A SMOKE/BURNING SMELL NEAR ROWS 16-18. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DISCREPANCIES NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06TY053Bracket · chafedTYS DURING A 2C INSPECTION THE RIGHT AILERON PCA ATTACHMENT BRACKET HAS DAMAGE WHERE THE HAT BUSHINGS WERE GOUGED. MAINTENANCE REMOVED AND REPLACED THE PCA BRACKET IAW EC 5750-01177. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.SDR C2XA06TY052Sill · corrodedTYS DURING A 2C INSPECTION THE FWD L ANGLE IN THE CARGO DOORWAY WAS FOUND WITH CORROSION. MAINTENANCE REMOVED THE CARGO DOOR SILL AND THE CORROSION; FR 68 SHEAR CLIP, REPAIRED CARGO DOOR SILL, ALODINED, PRIMED, PAINTED AND SEALED EC 5330-01458. ALL WORK WASSDR C2XA06TY051Tank · corrodedTYS DURING A 2C INSPECTION CORROSION WAS FOUND BENEATH A FUEL LINE SUPPORT BRACKET ON THE VENTRAL TANK. MAINTENANCE CUT OUT THE CORRODED AREA, FAB A DOUBLER IAW EC2810-01017, SRM 57-10-03, APPLIED FUEL TANK SEALANT AND FUEL VAPOR COATING IAW EMB XR SRM 51-40SDR C2XA06CL008Valve · leakingCLE FLIGHT 3260 - THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT WHEN APU STARTING. MAINTENANCE REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.SDR C2XA05IA056Charger · inoperativeCRP - DURING MAINTENANCE INSPECTION THE NUMBER TWO EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO
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