N14180
Service difficulty reports · 85
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 = 'N14180' 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 = 'N14180' 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 JJBA20221121016Actuator Cable · jammedMAIN CABIN DOOR WON'T OPEN, ACTUATING MECHANISM JAMMED. INSPECTED AND FOUND MAIN DOOR FORWARD LOCK JAMMING. ADJUSTED MAIN CABIN DOOR CABLE D TO FRONT LOCK BOX. FOUND AFT LOCKING-MECHANISM CAM OVER CENTER. THE LOCKING FORCE OUT OF LIMITS (ON LOW SIDE WITH FORCESDR JJBA20211027060None · noneMCD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R&R MCD EXT EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.SDR JJBA20210611019Skin · dentedLH WING INBD LEADING EDGE HAS A DENT. ACCOMPLISHED PERMANENT REPAIR TO THE LEFT HAND WING LEADING EDGE 1 BY REMOVING DAMAGE, NDT PERFORMED. FABRICATED AND INSTALLED REPAIR PARTSSDR JJBA20210607013Floor Support · corrodedCABIN FLOOR SUPPORTS IN MIDDLE SECTION (FR 23-FR 59) POSSIBLE CORROSION. EVALUATED AREA RH FLOOR SUPPORT BTW FR 23-25, FR53-57. FOUND TO BE IN LIMIT, APPLIED ALODINE AND PRIME. AREA AT RH BTW FR 25-36, FR 37-41, LH BTW FR 21-23, FR 23-25, FR 28-40, FR 29-35, FSDR JJBA20210606012Floorbeam · corrodedLAV FLOOR BEAMS BL 19L, BL 0, BL 19R SIGNS OF CORROSION. EVALUATED AND REMOVED CORROSION ON LAV FLOOR BEAMS. FOUND TO BE 100% OUT OF LIMITS. REMOVED AND INSTALLED NEW GUSSETS ON BL 0 AND BL 19. REMOVED AND FABRICATED NEW GUSSET FOR LBL19 AND INSTALLED NEW GUSSSDR JJBA20210604011Seat Track · damagedLH COCKPIT SEAT TRACK HAVE ELONGATED HOLES (LH AND RH SIDE) AND CHAFFED. EVALUATED LH COCKPIT SEAT TRACK. FOUND TO BE OUT OF LIMITS. COUNTER SIDE EXCEEDS THE MINIMUM REQUIREMENT. REMOVED AND REPLACED SEAT TRACK LH.SDR JJBA20210602007Floor Support · corrodedCABIN FLOOR SUPPORTS IN FWD SECTION (FWD OF FR 23) POSSIBLE CORROSION. REMOVED CORROSION ON GUSSET AND BEAM ASTER EVAL. FOUND BOTH PARTS TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW GUSSET AND BEAM AT FR 16 TO FR 24 BL-O AND FR 20 BL-O. TREATED, PRIMED, TOP SDR JJBA20210522026Seat Track · damagedRH COCKPIT SEAT TRACK HAVE ELONGATED HOLES (LH SIDE AND RH SIDE) AND CHAFED. REMOVED AND REPLACED 2 EA TRACKS AT RH COCKPIT (LH SIDE AND RH SIDE).SDR JJBA20210519021Reinforcement · corrodedPAX DOOR THRESHOLD REINFORCING STRUCTURE HAS CORROSION THREE DIFFERENT BRACKETS. REMOVED AND REPLACED 2 NEW BRACKETS ON PAX DOOR OUTBD BRACKETS PAINT DAMAGE ONLY.SDR JJBA20210518019Hinge · wornPAX DOOR, UPPER SIDE HINGE ATTACHMENT FITTING HAS WEAR MARKS AND GAUGING. BLENDED OUT DAMAGE.SDR JJBA20210518018Hinge · crackedPAX DOOR, LWR SIDE HINGE ATTACHMENT FITTING HAS CRACK MARK. BLENDED OUT DAMAGE.SDR JJBA20210518017Floorbeam · corrodedFRM 23, 15R, RBL 0.0'-27.0" FLOOR BOARD SUPPORT BEAM HAS CORROSION (FLOOR STRUCTURE). REMOVED AND REPLACED ANGLE (SUPPORT).SDR ASOA2020031184003Light · overheatedIAH - FLIGHT 4328, THE CREW REPORTED CEILING LIGHT SMOKE SMELL 1A & 2A. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE AFFECTED CEILING LIGHT ON MEL 33-20-00-2, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR ASOA2019041065049Ground Stud · damagedCREW REPORTED ROW 18 EMERGENCY LIGHTS WILL NOT ILLUMINATE FACING A/C FRONT BACK SIDE WORKS. MX INSPECTED AND FOUND W192-8819-22N (GROUND STUD GS8517DC) DAMAGED REPAIRED ITEMS OPERATIONAL CHECKS GOOD IAW EMB 145 XRJ AMM 33-50-50 (20-13-05) A/C WAS APPROVED FOR SDR ASOA201807095161Inverter · inoperativeDURING MX INSPECTION THE LOWER EMERGENCY LIGHT ON THE SERVICE DOOR WAS INOP. MX REMOVED AND REPLACED THE NR 2 INVERTER WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA201806267116Fitting · crackedTYS A/C CAME IN FOR A 2A INSPECTION WHEN INSPECTION FOUND THE LEFT ENGINE LOWER FWD AFT FITTING CRACKED AND VERIFIED BY NDT METHODS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW EA 26-2014-063. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AFTER ALL WORK IS CSDR ASOA201702020046Skin · crackedDURING C-CK. FUSELAGE SKIN CRACK AT FR 75 BTW STR 2L-3L. REPAIRED FUSELAGE SKIN IAW SRM 53-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160912046Computer · faultedCREW REPORTED THE ACFT GOES INTO R/O AND G/A MODE DURING TAKEOFF AND ON APPROACH AND UNABLE TO SWITCH OUT OF IT. MAINTENANCE R & R IC-600 NR 2 WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160912049CComputer · malfunctionedTHE CREW REPORTED THE AIRCRAFT GOES INTO A ROLL AND GA MODE DURING TAKOFF AND ON APPROACH AND UNABLE TO SWITCH OUT OF IT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 IC600 COMPUTER. OPS CHECKED GOOD.SDR ASOA20150815045Yoke · crackedDURING MAINTENANCE THE NR 2 ENGINE FORWARD LOWER YOKE FITTING WAS FOUND CRACKED. MAINTENANCE REPLACED THE NR 2 ENGINE YOKE FITTING IAW STS EA 26-2014-063.SDR ASOA20150620059Inverter · inoperativeDURING PREFLIGHT THE EXIT ROW EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150318019Controller · failedTHE CREW REPORTED WINDSHIELD HEAT NR 1 FAIL RESULTING IN ELECTRICAL OVERHEAT SMELL. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD HEAT TEMP CONTROLLER, OPS CHECKS WERE GOOD.SDR ASOA20141016114RInverter · inoperativeDURING MAINTENANCE INSPECTION, THE FWD EMERGENCY EXIT ROW AISLE LIGHT WOULD NOT ILLUMINATE. MX R & R THE NR 6 EMERGENCY LIGHT SYSTEM INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140930083Light · inoperativeTHE CREW REPORTED OVERHEAD EMERGENCY EXIT LIGHT AT ROW 12 DID NOT ILLUMINATE DURING TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT AT ROW 12. OPS CHECKED GOOD.SDR ASOA20140705092Light · inoperativeDURING PREFLIGHT THE CREW REPORTED THAT THE EMERGENCY LIGHT WAS INOPERATIVE OVER SEAT 18C ON THE FORWARD SIDE. MAINTENANCE R & R THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR V0XD201405250122Skin · dentedDENT ON REAR FUSELAGE SKIN, FRAME 78 STRINGER 6L. REPAIRED DENT IAW EC 5330-02473.SDR V0XD2014052518021Structure · corrodedWASTE DRAIN VALVE COMPARTMENT CORRODED. R & R WASTE DRAIN VALVE COMPARTMENT IAW SRM 51-40-02.SDR V0XD2014052518020Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT FRAMES 41-48. R & R RT FLOOR SUPPORT IAW SRM 51-40-02, 51-40-04, 51-40-06.SDR V0XD2014052518019Channel · corrodedSERVICE DOOR FRAME CHANNEL CORRODED AT THREE NUT PLATE LOCATIONS. R & R SERVICE DOOR FRAME CHANNEL IAW SRM 51-40-02, 51-20-03.SDR V0XD2014052518018Support · corrodedCORROSION ON LT SUPPORT AT FRAME 64 S15L. BLENDED CORROSION MATERIAL LOSS WAS .003" WITHIN LIMITS IAW SRM 53-31-10.SDR V0XD2014052518017Beam · corrodedLAV LT BEAM CAP CORRODED. BLENDED CORROSION, REMOVED .005" OF MATERIAL LOSS. FOUND TO BE WITHIN LIMITS IAW SRM 53-24-10, WO 80225, WC 1184.SDR V0XD2014052518016Cap · corrodedLEFT NLG TRUNNION CAP HAS PITTING. REMOVED MINOR PITTING ON LT NLG TRUNNION CAP IAW SRM 53-11-08, WO 80225, W/C 1177.SDR V0XD2014052518015Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT AFT OF FRAME 50. R & R RT FLOOR SUPPORT FROM FRAMES 48-52 IAW SRM 51-40-02, 51-20-03.SDR V0XD2014052518014Floorbeam · corrodedRT FLOORBEAM ANGLE CORRODED AT FRAME 23. R & R RT FLOORBEAM ANGLE IAW SRM 51-40-02, WO 80225, WC 1183.SDR V0XD2014052518013Floor Support · corrodedCORROSION ON LT FLOOR SUPPORT. R & R LT FLOOR SUPPORT FROM FRAMES 18 - 24 IAW SRM 51-40-02, 51-40-09, 51-20-03.SDR V0XD2014052518012Floorbeam · corrodedCORROSION UNDER LAV FLOOR PANEL 261DF ON FLOORBEAM. R & R FLOORBEAM ANGLE IAW SRM 51-40-02.SDR V0XD2014052518011Floor Support · corrodedCORROSION ON LT FLOOR SUPPORT AT FRAME 49. BLENDED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-23-10. NDT PERFORMED.SDR V0XD2014052318010Floor Support · corrodedAFT CARGO BAY FLOOR SUPPORT CORRODED AT FRAME 65. BLENDED CORROSION IAW SRM 53-31-10, FOUND TO BE WITH IN LIMITS IAW SRM 53-31-10, SWPM 20-21-00, AND CPM 51-21-04, 51-21-05. NDT PERFORMED, NO DEFECTS NOTED.SDR V0XD2014052318009Splice · corrodedFLOOR SUPPORT CONNECTION SPLICE CORRODED AT FRAME 35 UNDER FLOORBOARD 252AF. BLENDED CORRODED AREA IAW SRM 53-23-10, AREA LESS THAN 10 PERCENT MATERIAL LOSS, FOUND TO BE WITH IN LIMITS.SDR V0XD2014052318008Floor Support · corrodedRIGHT FLOOR SUPPORT FROM FRAMES 24-36 IS CORRODED. REMOVED CORRODED FLOOR SUPPORT AND INSTALLED NEW IAW SRM 51-4-02, AND SWPM 20-21-00.SDR V0XD2014052318007Floor Support · corrodedCORROSION ON FLOOR SUPPORT FWD OF FRAME 26 LT SIDE. REMOVED CORRODED FLOOR SUPPORT AND INSTALLED NEW IAW SRM 51-40-02, 51-20-03, 51-40-06, AND SWPM 20-22-00.SDR V0XD2014052318006Floorbeam · corrodedCORROSION ON FLOORBEAM. R & R FLOORBEAM IAW SRM 51-40-02, 51-20-03 AND, 51-40-02.SDR V0XD2014052318005Window Frame · corrodedRIGHT WINDSHIELD ASSY FRAME IS CORRODED IN MULTIPLE AREAS. BLENDED CORRODED AREAS IAW ACMM 56-10-01, FOUND TO BE WITHIN LIMITS IAW MM 56-10-01. NDT PERFORMED, NO DEFECTS NOTED.SDR V0XD2014052318004Window Frame · corrodedLEFT WINDSHIELD ASSY FRAME IS CORRODED IN MULTIPLE AREAS. BLENDED CORRODED AREAS IAW ACMM 56-10-01, FOUND TO BE WITHIN LIMITS IAW ACMM 56-10-01. NDT PERFORMED, NO DEFECTS NOTED.SDR ASOA20130305020RWire · damagedCREW REPORTED THE F/O'S FLASHLIGHT WAS NOT CHARGING. MX REPAIRED THE WIRE ON THE F/O'S FLASHLIGHT CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121009131Light · malfunctionedDURING POST FLIGHT INSPECTION, CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT SHUTOFF. SWITCHES WERE CYCLED ON AND OFF AND THE LIGHTS EXTINGUISED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120711051Sign · inoperativeFWD FACING CEILING EMERGENCY SIGN OVERWING FOUND INOPERATIVE. MX R & R EMERGENCY EXIT CEILING SIGN WITH OPS CHECK SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20120604051Engine · leakingCREW REPORTED SMOKE IN THE LAVATORY. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. ENGINE LEAKING, MX REPLACED THE NR 2 ENGINE. OPS CHECKED GOOD.SDR ASOA20120508095Shear Tie · crackedSHEAR TIE CRACKED AT FR 73, BETWEEN STR 8BR AND 9BR. MX R & R THE SHEAR TIE IAW SRM 51-10-03 AND 51-40-02.SDR ASOA20120508094Floor Support · crackedSPLICE BRACKET CRACKED AT THE LT OMEGA BEAM BETWEEN FR 16 AND 17. MX R & R THE SPLICE BRACKET IAW SRM 51-20-03 AND 51-40-02. ACFT WILL BE RELEASED AT THE END OF THE CHECK.
Back to N14180