N13978
Service difficulty reports · 135
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 = 'N13978' 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 = 'N13978' 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 C2XA02SH165Butt Strap · corrodedSHV- DURING C-CHECK CENTER OMEGA BEAM BUTT STRAP WAS FOUND TO HAVE CORROSION BETWEEN FRAMES 20-23. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTT STRAP IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH164Angle · corrodedSHV- DURING C-CHECK RAMP ANGLE ON CENTER OMEGA BEAM BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED DAMAGED AREA AND REPLACED AFFECTED RAMP ANGLE. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH163Structure · gougedSHV- DURING C-CHECK NUMBER TWO LOWER COWLING AFT EDGE MEMBER WAS FOUND TO BE CHAFFED. MAINTENANCE REMOVED AND PLACED AFFECTED EDGE MEMBER IAW EMB SRM 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH162Stiffener · gougedSHV- DURING C CHECK NUMBER ONE COWLING STIFFENER AT STATION 2180 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH161Structure · gougedSHV - DURING C-CHECK NUMBER 1 LOWER COWLING OUTBOARD EDGE MEMBER WAS GOUGED BETWEEN STATIONS XN=2905.0 AND XN=3167.5. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH160Stiffener · gougedSHV- DURING C CHECK NUMBER ONE LOWER COWLING AFT STIFFENER WAS FOUND GOUGED. MAINTENANCE REMOVED AND REPLACED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH159Floorbeam · corrodedSHV - DURING C-CHECK LEFT HAND OMEGA BEAM WAS FOUND TO HAVE CORROSION ON DOUBLER INBOARD AT FRAME 20. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH158Butt Strap · corrodedSHV- DURING C-CHECK BUTT STRAP AT FRAME 17 WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02SH157Doubler · corrodedSHV- DURING C CHECK TWO DOUBLERS WERE FOUND TO HAVE CORROSION ON RIGHT OMEGA BEAM BETWEEN FRAMES 20 AND 22. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED DOUBLERS IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA02IA188B-Nut · looseIAH- DURING TAKEOFF THE CREW NOTED THAT E2 ATTCS NO MARGIN, REJECTED TAKEOFF. MAINTENANCE INSPECTED THE ENGINE AND FOUND A LOOSE B-NUT ON THE START CONTROL VALVE. MAINTENANCE TIGHTENED THE B-NUT AND PERFORMED A ENGINE RUN ON THE NR 2 ENGINE. NO DEFECTS NOTSDR C2XA02IA186Hinge · wornLIT- THE CREW NOTED SEVERE VIBRATIONS IN BOTH YOKES IN FLIGHT. DECLARED EMERGENCY AND THE FLIGHT WAS DIVERTED TO LIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ELEVATOR IAW EMB145 AMM 27-30-00, OPS CHECK GOOD. THE AIRCRAFT WAS APSDR C2XA02IA187Hinge · wornLIT- THE CREW NOTED SEVERE VIBRATIONS IN BOTH YOKES IN FLIGHT. DECLARED EMERGENCY, THE FLIGHT WAS DIVERTED TO LIT, LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ELEVATOR IAW EMB145 AMM 27-30-00, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVSDR C2XA02BT025Smoke Detector · activatedEWR- CREW REPORTED, LAV SMOKE INDICATOR WITH SMELL OF SMOKE, BUT LAV SMOKE INDICATOR EXTINGUISHED AFTER ONE MINUTE AND SMOKE SMELL DISSIPATED. MAINTENANCE RAN ENGINES WITH BOTH PACKS ON, TESTED LAV SMOKE NO SMELL IN CABIN OR COCKPIT, NO FAN SMOKE FAULT IAW ESDR C2XA02IA087Smoke · detectedAMA- FLIGHT 3808 ON TAKEOFF THE CREW NOTED SMOKE IN THE LAV AND RETURNED TO AMA WITHOUT INCIDENT. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LAV FIRE DETECTION SYSTEM AND CHECKED THE LAV FOR SMOKE, NO DEFECTS NOTED. COULD NOT DUPLICATE THE PROBLEM ANDSDR C2XA01CL222Smoke Detector · dirtyCLE FLIGHT NR 3323 THE CREW REPORTED SMOKE IN CABIN AND COCKPIT ALONG WITH A LAV SMOKE INDICATION. THE CREW DECLARED A EMERGENCY AND RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CLEANED DEBRIS FROM LAV SMOKE DETECTOR. THSDR C2XA01BT172Controller · faultyCREW REPORTED ON TAXI, SMOKE IN COCKPIT ELECTRICAL BURNING SMELL IN COCKPIT ONLY. CONTRACT MAINTENANCE FOUND FAULTY AP PUSHBUTTON SWITCH ON AUTOPILOT CONTROL PANEL. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROLLER IAW EMB145 MM 22-11-01. OPS CHECK GOOD. AIRSDR C2XA01IA216Power Supply · inoperativeIAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA01TY059Skin · chafedTYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE INTERNAL SKIN AT FRAMES NR 66 AND 67 WAS FOUND CHAFED BY A BLEED LINE ADEL CLAMP. MAINTENANCE REPAIRED DAMAGED AREA BY INSTALLING A DOUBLER IAW EMB-GST-0869/01, REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL RELSDR C2XA01TY058Frame · chafedTYS DURING A SCHEDULED INSPECTION, FRAME NR 80 WAS FOUND TO BE CHAFED BY THE APU FIRE BOTTLE DISCHARGE LINE. MAINTENANCE REPAIRED FRAME NR 80 IAW EMB-GST-0872/01, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA01TY057Fairing · crackedTYS DURING A SCHEDULED INSPECTION THE APU COWLING UPPER RIGHT HAND FAIRING WAS FOUND CRACKED ALONG THE ATTACHMENT FLANGE. MAINTENANCE REMOVED AND REPLACED THE FAIRING IAW EMB GST-0835/01 AND EMB-145 CPM-51-21-06. AIRCRAFT WILL BE RELEASED UPON COMPLETION OFSDR C2XA01TY056Firewall · gougedTYS DURING A SCHEDULED INSPECTION THE APU FIRE WALL WAS FOUND GOUGED ADJACENT TO THE BYPASS VALVE. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB GST-0429/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA01TY052Fire Loop · chafedTYS DURING A SCHEDULED INSPECTION THE LEFT ENGINE FIRE LOOP WAS FOUND CHAFED, ON TOP SECTION OF ENGINE. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE FIRE LOOP IAW EMB-145 MM 26-11-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SSDR C2XA01TY055Attach Fitting · gougedTYS DURING A SCHEDULED INSPECTION THE RIGHT HAND AILERON TO PCA ATTACH FITTING WAS FOUND GOUGED AND CHAFED. MAINTENANCE REMOVED AND REPLACED THE ATTACH FITTING IAW EMB GST-0903/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OSDR C2XA01TY054Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION SEVERAL AREAS OF CORROSION WAS FOUND ON THE RIGHT HAND OMEGA BEAM BETWEEN FRAMES 19 AND 22. MAINTENANCE REPAIRED THE RIGHT HAND OMEGA BEAM IAW EMB GST-0823/01, REPAIR WAS SATISFCATORY. THE AIRCRAFT WILL BE RELEASED UPON COMSDR C2XA01TY053Floor Support · corrodedTYS DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE RIGHT HAND OMEGA BEAM TOP CAP BETWEEN FRAME 18 AND 23. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND OMEGA BEAM TOP CAP IAW EMB-145 SRM-51-40-02 AND EMB-145 CPM-51-21-06. THE REPAIR WAS SATISFACSDR C2XA01TY051Floorbeam · corrodedTYS DURING A SCHEDULED INSPECTION THE LEFT OMEGA BEAM WAS FOUND TO HAVE CORROSION UNDER THE CARBON FIBER SUPPORT RAIL AT FRAME 20. MAINTENANCE REPAIRED THE OMEGA BEAM IAW EMB-145 SRM-53-21-10, EMB-145 SRM-51-40-02 AND EMB-145 CPM-51-21-03,04. THE REPAIR WASSDR C2XA01TY049Axle · gougedTYS DURING A SCHEDULED INSPECTION THE NOSE LANDING GEAR AXLE WAS FOUND TO BE GOUGED. MAINTENANCE REPAIRED THE AXLE IAW EMB GST-0866/01 AND EMB-CPM-51-21-05, THE REPAIR WAS FOUND TO BE SATISFCATORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTIONSDR C2XA01TY048Frame · chafedTYS DURING A SCHEDULED INSPECTION, FRAME 64 LOCATED INSIDE OF CARGO BAY WAS FOUND CHAFED. MAINTENANCE REPAIRED THE DAMAGED AREA IAW EMB GST-0812/01, THE REPAIR WAS FOUND TO BE SATISFCATORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA01TY047Skin · crackedTYS DURING A SCHEDULED INSPECTION THE LEFT HAND UPPER COWLING SKIN WAS FOUND CRACKED JUST FORWARD OF THE CENTER HINGE POINT. MAINTENANCE REPAIRED THE SKIN IAW EMB GST-0821/01, THE REPAIR WAS FOUND TO BE SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLSDR C2XA01TY046Bracket · gougedTYS DURING A SCHEDULED INSPECTION THE LEFT HAND AILERON ATTACHMENT BRACKET WAS FOUND TO BE GOUGED. MAINTENANCE REPAIRED THE BRACKET IAW EMB GST-085/01, THE REPAIR WAS FOUND SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA01TY045Skin · gougedTYS DURING A SCHEDULED INSPECTION THE CARGO DOOR SKIN WAS FOUND GOUGED AT THE CUTOUT FOR THE ACTUATING HANDLE. MAINTENANCE REPAIRED THE SKIN IAW EMB GST-0815/01, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR C2XA01TY044Angle · corrodedTYS DURING A SCHEDULED INSPECTION THE RIGHT OMEGA BEAM RAMP ANGLE BETWEEN FRAMES 19 AND 20 WAS FOUND BENT AND CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-145 SRM 51-40-02, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE SDR C2XA01TY043Gusset · corrodedTYS DURING A SCHEDULED INSPECTION THE FLOOR STRUCTURE DIGITAL GUSSET LOCATED JUST AFT OF THE COCKPIT DOORWAY, WAS FOUND TO HAVE SEVERAL AREAS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE DIGITAL GUSSET IAW EMB-145 SRM 51-40-03 AND EMB-145 CMP 51-21-06, SDR C2XA01TY042Cowling · gougedTYS DURING A SCHEDULED INSPECTION THE APU COWLING UPPER PROFILE WAS FOUND TO BE BENT AND GOUGED. MAINTENANCE REMOVED AND REPLACED THE PROFILE IAW EMB-GST-0801/01, REPAIR WAS SATISFACTORY. AIRCRAFT WILL BE RELEASED FOR SERVICE UPON COMPLETION OF INSPECTION.SDR C2XAOOCL095O-Ring · wornCLE-CREW REPORTED A BLEED 2 LEAK MESSAGE ON THE EICAS. CREW FOLLOWED THE QRH AND THE MESSAGE WENT AWAY AFTER ONE AND HALF MINUTES. A/C RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MX REMOVED/REPLACED 0-RINGS ON NR 2 BLEED IN AFT UPPER CARGO BAY I
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