N16149
Service difficulty reports · 158
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 = 'N16149' 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 = 'N16149' 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 JJBA20210510011Strut · inoperativeLH MLG SIDE STRUT LOWER BEARING FLANGE HAS MISSING ARROWS. REMOVED AND REPLACED LH MLG LOWER SIDE BRACE. OPS CHECK GOOD.SDR JJBA20210401006Armrest · crackedFOUND CRACK UNDER ARMREST 7A MIDWAY UP. REMOVED AND REPLACED SEAT 7A.SDR JJBA20212140008Seat Frame · crackedPASSENGER SEATS 2A AND 18A HAVE CRACKED SUPPORTS BELOW AISLE ARMREST. SEATS 3A, 6A, AND 7A HAVE CRACKED SUPPORTS. R&R PASSENGER SEATS. NO OTHER DEFECTS NOTED AT THIS TIME.SDR JJBA20210123024Engine · failedENGINE 2 FAILED AND SHUT DOWN ON CLIMB OUT. INSTALLED REPLACEMENT NR 2 ENGINE. OPERATIONS AND LEAK CHECK SATISFACTORY.SDR JJBA20201209009Lamp · inoperativeSERVICE DOOR LOWER EMERGENCY LIGHT INOPERATIVE. R & R SERVICE DOOR LOWER EMERGENCY LIGHT LAMP. OPERATIONS CHECK SATISFACTORY, NO FURTHER DEFECTS NOTED.SDR JJBA20201102002Bolt · damagedMAIN CABIN DOOR DOES NOT OPEN FROM INSIDE. OPENS WITH OUTSIDE HANDLE. FOUND SECURING BOLT FOR HANDLE SPLINE TO BE LOOSE AND STRIPPED. REMOVED AND REPLACED BOLT AND NUT. OPERATIONS CHECK SATISFACTORY.SDR JJBA20201011009Gearbox · overpressuredE2 BLEED CAUSES OIL SMELL IN AIR COND. PERFORMED OIL-RELATED SMOKE/ABNORMAL SMELL IN CABIN/COCKPIT FIM TASK. FOUND ENGINE NR 1 EMITTING OIL SMELL THROUGH PACK SYSTEM WITH BLEED NR 1 ON, APU SHUT OFF AND ENGINE NR 2 OFF. NO INDICATION OF LEAKAGE OR PUDDLING SDR JJBA20201009008Strip · looseEMERGENCY REFLECTIVE STRIP LOOSE BY 1A. SECURED LOOSE PROX STRIP BY SEAT 1A.SDR JJBA20200923005Battery Pack · inoperativeMULTIPLE INTERNAL AND ONE EXTERNAL EMERGENCY LIGHTS INOPERATIVE. R&R NR 2 EMERGENCY LIGHT BATTERY, OPS CHECK SAT.SDR JJBA2020082514013Skin · crackedCRACK FOUND EXTENDED OUT FROM VORTILON NUMBER 1 ON LEADING EDGE. REMOVED AND REPLACED LEADING EDGE 111. OPERATIONS CHECK SATISFACTORY.SDR JJBA2020052010006O-Ring · damagedSMELL OF HYD OR FUEL DURING TAKE OFF. SMELL WENT AWAY AFTER APU SHUTDOWN AND BLEEDS TRANSFERRED TO ENGINES. PERFORMED T/O POWER RUNS IN THESE SCENARIOS - APU OFF, BOTH ENGINES AT T/O POWER, BLEED 2 OPEN, BLEED 1 CLOSED AND PACK 1 ON. ONLY SMELL FROM THIS SET SDR JJBA2020051108002Pump · contaminatedINVESTIGATE SOURCE OF FIBROUS DEBRIS IN RH ENGINE FUEL FILTER. FOUND PIECE OF CLOTH STUCK IN EJECTOR PUMP, NO OTHER DEBRIS. REMOVED, CLEANED AND REINSTALLED PUMP.SDR JJBA202005205005Unknown · odorSTRONG FUEL SMELL ON TAKE-OFF WITH APU RUNNING. INSPECTED ALL FUEL NOZZLES, FUEL NOZZLE GASKETS, NOZZLE MANIFOLD, FUEL CONTROL, FUEL LINES, FUEL HOSES, AND COMBUSTOR DRAIN LINE WITH APU RUNNING. OBSERVED NO LEAKAGE OR EVIDENCE OF LEAKAGE BEFORE, DURING, OR AFTSDR JJBA202005203004Fuel Control · malfunctionedSMELL OF FUEL ON TAKE OFF WITH APU RUNNING. R&R APU FUEL CONTROL. HIGH POWER ENGINE RUNS OPS CHECK SAT. NO FUEL SMELL NOTED AT THIS TIME.SDR JJBA20191101001Snap Ring · out of positionMAIN CABIN DOOR WILL NOT OPEN. MAIN CABIN DOOR INTERNAL HANDLE INTERMEDIATE TORQUE TUBE ON RT SIDE END HAS A SNAP RING OUT OF PLACE, CAUSING TORQUE TUBE TO SHIFT AND INTERFERE WITH OPENING. REMOVED AND REINSTALLED TORQUE TUBE WITH NEW SLIP RING. PERFORMED INTESDR JJBA20190914002Light · unsecureEMERGENCY LIGHT STRIP BY SEAT 1A NOT SECURED. RE SECURED EMERGENCY FLOOR LIGHTING NEAR SEAT 1A.SDR ASOA2019061964030Skin · corrodedDURING MX INSPECTION, CORROSION WAS DISCOVERED ON THE AFT EXTERNAL FUSELAGE SKIN COMING FROM UNDER THE AIRCRAFT DATA PLATE. MX CUT OUT THE DAMAGED AREA AND PERFORMED A FILLER/DOUBLER REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICESDR ASOA201811073068Bracket · crackedDURING C CHECK INSPECTION MAIN CABIN DOOR FORWARD UPPER ROLLER BRACKET HAD A DAMAGED NUTPLATE. MAINTENANCE REMOVED ROLLER BRACKET ASSEMBLY AND FOUND BRACKET TO BE CRACKED. THE CRACKED HOLE WAS DRILLED OVERSIZED TO .375" TO REMOVE CRACK. THE HOLE WAS REAMED ANDSDR ASOA201810123065Frame · crackedDURING C CHECK FOUND CRACK ON FRAME 10 RHS INNER FLANGE AT TOP FORWARD RIVET AT ATTACHMENT TO WINDOW SILL STRUCTURE. MAINTENANCE REPLACED FRAME 10 RHS INNER FLANGE IAW SRM 51-40-02.SDR ASOA201810113066Fitting · crackedSHEAR CLIP CRACKED AT FRAME 80 BETWEEN STRINGER 5L AND 7L. MAINTENANCE REPLACED SHEAR CLIP AT FRAME 80 STRINGER 5L AND 7L.SDR ASOA201810093061Floor Support · corrodedDURING C CHECK CORROSION WAS FOUND ON OMEGA BEAM BETWEEN FRAME 22 AND FRAME 23 JUST AFT OF THE SERVICE DOOR. MAINTENANCE REPAIRED OMEGA BEAM IAW SRM 53-21-10.SDR ASOA2018102623063Rib · crackedDURING C CHECK INSPECTION FOUND RIGHT WING RIB WEB CRACKED BETWEEN RIB 20-21. MAINTENANCE REPAIRED WING RIB WEB BETWEEN RIB 20-21 IAW ETD2018-145-105347 AND SRM 57-20-07SDR ASOA201810023062Rib · crackedDURING C CHECK INSPECTION FOUND LEFT WING WEB CRACKED BETWEEN RIB 20-21. VERIFIED BY EDDY CURRENT. MAINTENANCE REPAIRED LEFT WING RIB 21 WEB IAW SRM 57-20-07.SDR ASOA2018101693059Fitting · crackedDURING C CHECK FOUND RIGHT ENGINE FORWARD LOWER PYLON YOKE FITTING CRACKED. MAINTENANCE REPLACED FORWARD YOKE FITTING.SDR ASOA2018101783060Skin · dentedDURING C CHECK FOUND DENT BELOW PANEL 113EZ. GPU SERVICE PANEL. BETWEEN FR 07 AND FRAME 08. MAINTENANCE REPAIRED IAW SRM 53-12-01SDR ASOA201704194020Light · inoperativeTHE CREW REPORTED THAT THE EMERGENCY LIGHT STRIP AT THE GALLEY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPS TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160929053Fadec · inoperativeNR 1 ENGINE LOSS 20 PERCENT N1, FADEC INOPERATIVE. MX REMOVED AND REPLACED THE FADEC 1A AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160530037Inverter · inoperativeTHE CREW REPORTED EMERGENCY LIGHT ABOVE THE F/A SEAT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.SDR ASOA20160416020Door Sill · corrodedDURING C-CHECK, THE SERVICE DOOR CUTOUT CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160416019Frame · crackedDURING C-CHECK THE FRAME 10 SEGMENT JUST BELOW THE PILOT'S DV WINDOW WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FRAME IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160217012Skin · dentedGROUND DAMAGE WAS DISCOVERED ON THE AFT FUSELAGE BETWEEN FRAMES 65-66, STRINGERS 20L-21L. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A FILLER AND DOUBLER REPAIR. LEAK CHECKS WERE PERFORMED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVSDR ASOA20150426020RBattery Pack · inoperativeCREW REPORTED THE EMERGENCY LIGHT OVER EXIT ROW NOT WORKING. MAINTENANCE R & R NR 4 EMERGENCY BATTERY PACK WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150306025HLight · inoperativeDURING PRE-FLIGHT, THE CREW REPORTED THAT THE EXIT LIGHT AT THE FRONT OF THE CABIN WAS INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140123013Fairing · damagedDURING C-CHECK, LEFT OTBD FLAP INBD FAIRING FLANGE HAS MULTIPLE DRILL HOLES. MAINTENANCE REPAIRED IAW EC5750-01566. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20140123012Support · corrodedDURING C-CHECK, DUMP VALVE EXTERNAL HOUSING CORRODED, LOCAL LEVEL 2, AT SEVERAL AREAS. MAINTENANCE R & R WASTE DRAIN DUMP SUPPORT ASSY IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140123011Skin · crackedDURING C-CHECK, VISUAL INDICATION OF CRACKS ON FUSELAGE BETWEEN FRAMES 77-80, S3-6L. MAINTENANCE REPAIRED SKIN IAW EC5330-01849. MAJOR REPAIR IAW EC5330-02849. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20140123009Support · corrodedDURING C-CHECK, WASTE DRAIN VALVE SUPPORT CORRODED. MAINTENANCE R & R WASTE DRAIN DUMP SUPPORT ASSY IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11RI059Display · faultyFLIGHT 2370 - MSP - FLIGHT CREW REPORTED BURNING SMELL AND LIGHT SMOKE IN COCKPIT COMING FROM FO MFD. CREW DECLARED EMERGENCY AND PERFORMED EMERGENCY DESCENT AND LANDED UNEVENTFULLY. CLE MX REMOVED AND REPLACED FO MFD AND PERFORMED OPERATIONAL CHECK SUCCESSFSDR C2XA11CL109Display · faultyTHE CREW REPORTED THE F/O MFD WENT BLANK WITH A BURNING SMELL AND LIGHT SMOKE. MX INSPECTED AND REPLACED THE F/O DISPLAY UNIT. OPS CHECKS WERE GOOD.SDR C2XA11SH085Pump · failedDURING FLIGHT, THE AIRCREW RECEIVED AN EICAS MESSAGE THAT THE E1 HYD PUMP FAILED. THE FLIGHT WAS DIVERTED AND THE ACFT LANDED WITHOUT INCIDENT. AN EMERGENCY WAS NOT DECLARED. MX R & R THE DEFECTIVE PUMP IAW AMM 29-10-03. THE ACFT WAS APPROVED FOR RETURN TSDR C2XA11TY040Skin · damagedTYS - A/C WAS ON SENT TO TYS FOR A LIGHTNING STRIKE DAMAGE BETWEEN STR 20/21R NEAR FR 72. MAINTENANCE INSTALLED A SMALL DAMAGE REPAIR TO FUSELAGE SKIN AT FR72 AND STR 20/21R IAW ETD 2011-145/00377. A/C WAS RELEASE AFTER PRESSURE CHECKS TO SERVICE. DMI WAS TSDR C2XA10RI0149Warning System · false activationFLIGHT 2224 - EWR - FLIGHT CREW REPORTED ENGINE 1 ANTI ICE FAIL - UNABLE TO CONTINUE DUE TO WEATHER. EWR MX PERFORMED OPERATIONAL CHECK OF ANTI ICE SYSTEM AND COULD NOT DUPLICATE INDICATION. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA10RI0141Warning System · false activationFLIGHT 2224 - EWR - FLIGHT CREW REPORTED ENG 1 ANTI ICE VALVE FAIL MESSAGE ON EICAS. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX PERFORMED OPERATIONAL AND FUNCTIONAL CHECK OF THE BLEED SYSTEM AND COULD NOT DUPLICATE MESSAGE. ACFT WAS APPROVED SDR C2XA10IA290Switch · failedFLIGHT 2769 DURING CLIMB THE CREW REPORTED AN ENGINE ONE ANTI-ICE FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE ANTI-ICE ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE SUBSEQUESDR C2XA10TY165Sign · inoperativeLT EMERGENCY LIGHT EXIT SIGN AT ROW 12A INOP. REMOVED AND REPLACED EXIT IDENTIFIER IAW EMB 145 AMM 330-50-15, OPS CHECK GOOD.SDR C2XA10RI131Light · inoperativeFLIGHT 3009 - EWR - FLIGHT CREW REPORTED EMERGENCY LIGHT STRIP INOP. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA10IA231Relay · inoperativeIAH - FLIGHT 2604, THE CREW REPORTED THAT AFTER DEPARTURE THE LANDING GEAR LEVER WOULD NOT RETRACT WITHOUT SEVERAL ATTEMPTS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RELAY K0024, OPERATIONALLY TESTED WITH NO DEFECTS. AIRSDR C2XA10RI105Control Module · inoperativeFLIGHT CREW REPORTED THAT AFTER T/O, LANDING GEAR WOULD NOT RETRACT WITHOUT PRESSING THE DOWNLOCK RELEASE BUTTON. MX R & R LANDING GEAR CONTROL LEVER MODULE AND PREFORMED EXT/RET OF LANDING GEAR CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09IA308Smoke Detector · malfunctionedIAH - FLIGHT 2081, THE CREW REPORTED INTERMITTENT LAV SMOKE WARNINGS ON EICAS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURSDR C2XA09IA149Control Panel · defectiveIAH - FLIGHT 2240, DURING CLIMB THE CREW REPORTED ELEC EMERGENCY ABNORMAL, BUT NO SYSTEM PROBLEMS NOTED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BATTERY CONTROL PANEL, OPERATIONALLY TESTED WITH NO D
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