N12567, cancelled Oct 20, 2020
Service difficulty reports · 60
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 = 'N12567' AND deregistration_id = 'N12567-2020-10-20' 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 = 'N12567' AND deregistration_id = 'N12567-2020-10-20' 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 ASOA201901214003Skin · damagedIAH - DURING MAINTENANCE INSPECTION A PREVIOUS REPAIR ON THE CARGO DOOR LOWER FORWARD CORNER WAS FOUND TO HAVE A CREASE ON THE SKIN. MAINTENANCE REMOVED THE DOUBLER, CUT OUT THE AFFECTED SKIN AND INSTALLED A NEW DOUBLER. PRESSURIZATION CHECKS WERE PERFORMED SASDR ASOA201804167062Wire · brokenINSPECTION FOUND A BROKEN WIRE ON THE EMERGENCY LIGHT STRIP. MAINTENANCE REPLACED THE LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.SDR ASOA201804167061Skin · damagedFOUND THE RT HORIZONTAL STAB LEADING EDGE DAMAGE AT THE LOWER SIDE SCREW HOLES. MAINTENANCE REPAIRED THE LOWER HORIZONTAL STAB LEADING EDGE IAW ETD 2018-145-037750.SDR ASOA201804137060Skin · damagedRIGHT HORIZONTAL STAB LEADING EDGE HAS DAMAGE AT THE SCREW HOLES ON LOWER SIDE. CONTOURED THE AREA BY COLD FORMING. INSTALLED DIMPLED WASHER IAW ETD2018-145-037750.SDR ASOA201804057052Door Frame · corrodedDOOR FRAME HAS CORROSION ON AFT LOWEST DOOR STOP ON SERVICE DOOR. REMOVED DAMAGED SECTION OF THE DOOR FRAME 22. DRILLED AND FABRICATED A DOUBLER SECTION OF THE FRAME AND INSTALLED.SDR ASOA201804057051Skin · crackedCRACKED SKIN AT FRAME 75. CUT OUT A 2 X 2 INCH SECTION OF THE SKIN AND INSTALLED FILLER AND DOUBLER.SDR ASOA201803247036Yoke · cracked#1 ENGINE PYLON LOWER FORWARD YOKE CRACKED. REMOVED AND REPLACED FORWARD YOKE. AIRCRAFT STILL IN C CHECK.SDR ASOA201706055083Control Unit · faultyPILOT REPORTED RIGHT BRAKE PEDAL WHEN COMMANDED RESULTS IN ALMOST NO BRAKING ACTION. ADDITIONALLY THE RIGHT IB BRAKE TEMP ALWAYS STAYED AT ZERO DESPITE THE RIGHT OB BRAKE TEMP GOING INTO THE AMBER INDICATION AFTER MODERATE BRAKING. MX REMOVED AND REPLACED BRAKSDR ASOA201612225092Light · inoperativeCREW REPORTED MOST AFT CABIN EMERGENCY LIGHTS ARE INOPERATIVE. MX REMOVED AND REPLACED THE LIGHT AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20160611028Control Module · odorHEAVY ELECTRICAL SMOKE ODOR REPORTED FROM MAIN CABIN DOOR AREA SPREAD TO THE GALLEY. R & R CABIN LIGHT CONTROL MODULE WITH OPS CHECK GOOD. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20150626033Charger · inoperativeDURING MAINTENANCE INSPECTION, THE LT FWD FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE R & R NR 4 EMERGENCY LIGHT BATTERY CHARGER AND REPAIRED WIRE NR W192-8593-20 WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20150520029Charger · faultyDURING ROUTINE MAINTENANCE THE LT FWD EXTERNAL EMERGENCY LIGHT AND AISLE CEILING LIGHT WOULD NOT TEST. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD.SDR ASOA20150304023Charger · inoperativeDURING A-CK INSPECTION, THE LT WING FWD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 1 BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20130806350TBearing · wornACFT LT AND RT HORIZONTAL STABILIZER SPHERICAL BEARINGS HAD PLAY IN THE HOUSING. MX REAMED BOTH HOUSINGS AND REPAIRED AND INSTALLED SPHERICAL BEARINGS IAW SRM 55-30-02. COMPLIED WITH BACKLASHES IAW AMM 27-40-00; ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERSDR ASOA20130702069Transducer · faultyPILOT REPORTED DURING BRAKE APPLICATION (RT ONLY) CLUNKING NOISE COMES FROM FWD OF COCKPIT UNTIL HARD BRAKE APPLICATION. BRAKING ACTION REDUCED UNTIL HARD APPLICATION. MX R & R NR 3 WHEEL SPEED TRANDUCER AND HARNESS WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVSDR ASOA20130412035Light · inoperativeDURING MX INSPECTION THE EMERGENCY LIGHT PROXIMITY STRIP BETWEEN ROW 4 AND 7 WAS FOUND INOPERATIVE. MX RESET SYS AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20121010081Duct · disconnectedTHE CREW REPORTED ODOR OF SMOKE AT SEATS 6-7. MX INSPECTED AND FOUND DUCT AT NR 2 RECIRCULATION FAN OFF UNDER FLOOR. MX REINSTALLED DUCT AT NR 2 RECIRCULATION FAN AND OPS CHECKED GOOD.SDR ASOA20120812109Battery Pack · dischargedDURING PREFLIGHT INSP THE CREW REPORTED TAHT THE FIRST 3 AISLE PATH EMERGENCY LIGHTS WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS AND THEN GO IFF, AND THAT THE EMERGENCY EXIT SIGN IN THE GALLEY WOULD ALSO NOT STAY ILLUMINATED. MX R & R THE NR 1 AND NR 2 EMERGENSDR ASOA20120812108Battery Pack · dischargedDURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST 3 AISLE PATH EMERGENCY LIGHTS WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS AND THEN GO OFF, AND THAT THE EMERGENCY EXIT SIGN IN THE GALLEY WOULD ALSO NOT STAY ILLUMINATED. MX R & R THE NR 1 AND NR 2 SDR ASOA20120525108Sill · corrodedCORROSION ON REPAIR DOUBLER RT SILL FRAME 20. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED, PAINTED.SDR ASOA20120519106TShear Tie · crackedSHEAR CLIP FOUND CRACKED AT FRAME 61 BETWEEN STR 6L AND 7L. MX R & R THE SHEAR CLIP IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20120519105Shear Tie · crackedSHEAR CLIP CRACKED AT FRAME 80 AT THE APU FIRE BOTTLE. MX R & R THE SHEAR CLIP IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20120519104Crossbeam · corrodedCORROSION WAS FOUND IN THE ISLE AT FRAME 20 CROSS-MEMBER THAT WAS BLENDED OUT OF LIMITS. MX R & R THE CROSS-MEMBER IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20120519103Floor Support · crackedTHE RT OTBD OMEGA BEAM SUPPORT WAS FOUND CRACKED AT FRAME 47 TO 48. MX R & R THE SUPPORT IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20120519102Skin · canningDENT ON THE CARGO DOOR. MX RECONTOURED DENT, SKIN HAD A OIL CAN, SO THEY CUT OUT DAMAGE, FABRICATED A FILLER AND DOUBLER, THEN INSTALL FILLER AND DOUBLER IAW SRM 53-20-01 AND ETD 2011-145-102644. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CSDR ASOA20120519101Seat Track · corrodedTHE LEFT OTBD SEAT TRACK WAS FOUND CORRODED BEYOND LIMITS AT FRAME 50. MX R & R THE SUPPORT AT FRAME 50 IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20120525110Floor Support · corrodedCORROSION IN GUSSET CENTER OMEGA BEAM FRAME 20. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED AND PAINTED.SDR ASOA20120525109Bracket · corrodedCORROSION ON BRACKET AT PAX DOOR ENTRANCE BELOW FLOOR. BLENDED CORROSION, WITHIN LIMITS. TREATED, PRIMED AND PAINTED.SDR C2XA11CL064Smoke Warning · false activationICT FLT 6056 THE CREW REPORTED A LAV SMOKE EICAS MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND PERFORMED LAV SMOKE SYSTEM OPERATIONAL CHECKS. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR C2XA10SH248Skin · crackedSHV - DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 2-10L. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC5330-02080 AND EC5330-02188. THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR C2XA10SH247Skin · crackedSHV - DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 78-79 AND STRINGERS 2-10R. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC 5330-02080 AND EC5330-02188. THE AIRCRAFT WAS APPROVED FOR RETURN TO SSDR C2XA10SH246Frame · crackedSHV - DURING C-CHECK FRAME 10 AT STRINGER 10L (RIGHT BELOW THE LT DV WINDOW) WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH245Frame · crackedSHV - DURING C-CHECK FRAME 10 AT STRINGER 10R (RIGHT BELOW THE RT DV WINDOW) WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE CRACKED FRAME SEGMENT IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10TY022Fuse · blownTYS - A/C IN FOR A 3A CHECK WHEN INSPECTION FOUND THE LT FWD OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE FUSE IN BATTERY TRAY 1. OPS CHECK GOOD IAW EMB 135/145 VCMM 33-21-20 AND EMB 145 AMM 33-50-00. RELEASED TO SERVICE.SDR C2XA10IA003Light · inoperativeIAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE LEFT FORWARD EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09IA332Line · contaminatedIAH - FLIGHT 2263, THE CREW REPORTED AN ALTITUDE AND IAS ERROR WITH A BURNING SMELL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE DRAINED THE WATER FROM THE PITOT STATIC SYSTEM. INSPECTED THE COCKPIT, CURRENT RELAY SENSORS WITH NO DEFECTS NOSDR C2XA09IA069Charger · inoperativeLCH - DURING MAINTENANCE INSPECTION THE COCKPIT CEILING AND NR 1 AISLE PATH, CEILING, AND WING TO FUSELAGE FRONT FAIRING LEFT EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY CHARGER, OPERASDR C2XA09TY035Skin · dentedAIRCRAFT HAD TWO DENTS BETWEEN FRM 20/21 AND STR14L/16L. REPAIRED DENTED AREA BY FABRICATING L-ANGLE IAW IC2009-145/01434A. RE-CONTOURED SKIN, PERFORMED NDT, INSTALLED L-ANGLE AND RESTORED ORIGINAL FINISH IAW IC 2009-145/01434A. AIRCRAFT RELEASED AND RETURNSDR C2XA09TY024Battery Pack · failedACFT WAS FOUND WITH THE AFT CEILING EMERGENCY LIGHT INOP. MX R&R THE NR 4 EMERGENCY LIGHT POWER SUPPLY IAW AMM 145 33-50-04. OPS CHECK GOOD AND WAS RELEASED TO SERVICE.SDR C2XA08RI065Light · inoperativeFLIGHT 2648 - EWR - FLIGHT CREW REPORTED BAG SMOKE DETECT WOULD NOT ILLUMINATED ON TEST. EWR MX RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA08RI017Proximity Switch · intermittentFLIGHT 2761 - EWR - CREW REPORTED THAT AFTER ROTATION, LDG/AIR GRD FAIL MESSAGE AND REV DISAGREE MESSAGE APPEARED ON EICAS. MESSAGES CLEARED UPON GEAR EXTENSION NEAR EWR. EWR MX REMOVED AND REPLACED NLG AIR/GRD PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECSDR C2XA07RI100Control Lever · defectiveFLT 2490 - EWR - CREW REPORTED THAT LANDING GEAR WILL NOT RETRACT AFTER TAKEOFF. CREW PROCEEDED WITH AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED LANDING GEAR CONTROL LEVER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TSDR C2XA07IA075Inverter · inoperativeMCI - DURING MAINTENANCE INSPECTION AISLE PATH LIGHTS 6, 7 & 8 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06BT056Socket · looseBTV 2A CHECK FOUND RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP BASE IAW EMB145 AMM 33-50-10. OPS CHECK GOOD.SDR C2XA06IA110Battery · dischargedIAH - FLIGHT 3225, DURING PREFLIGHT INSPECTION, THE CREW REPORTED EMERGENCY AISLE PATH LIGHT WAS INOPERATIVE. MAINTENANCE RECHARGED THE AISLE PATH LIGHTING, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06IA101Inverter · inoperativeSTL - DURING MAINTENANCE INSPECTION, THE FORWARD EMERGENCY FLOOR LIGHT STRIPS 2 & 3 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOSDR C2XA06SH047Door Frame · corrodedSHV - DURING C-CHECK THE AFT LOWER SERVICE DOOR CUTOUT FRAME WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC5310-01373. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA06SH046Skin · gougedSHV - DURING C-CHECK THE FUSELAGE SKIN AT FRAME 7 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A PATCH REPAIR IAW EMB 145 SRM 53-11-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04CL119Contactor · failedCREW REPORTED A BURNING ODOR AND CRACKING SOUND BEHIND THE CAPTAINS SEAT AFTER THE APU FAILED. REPLACED THE APU LINE CONTACTOR. AIRCRAFT RETURNED TO SERVICE.SDR C2XA04TY085Sill · corrodedDURING A SCHEDULED 1C INSPECTION THE SERVICE DOOR SILL WAS FOUND CORRODED. MAINT. REMOVED THE REPLACED THE SERVICE DOOR SILL IAW EMB 135/145 SRM 51-40-02 AND IC-2004145/2152. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.
Back to N12567, cancelled Oct 20, 2020