N13988
Service difficulty reports · 127
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 = 'N13988' 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 = 'N13988' 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 ASOA20130304284TSkin · corrodedSERVICE DOOR CUT-OUT HAS CORROSION BEYOND LIMITS AFTER BLEND-OUT. R & R REINFORCEMENT STRUCTURE.SDR ASOA20130304283TFloor Support · corrodedOMEGA BEAM AT FRM 20 HAS AREAS OF CORROSION BEYOND LIMITS AFTER BLEND-OUT. CUT-OUT DAMAGE, FABRICATED AND INSTALLED.SDR ASOA20130304282Gusset · corrodedCORROSION BEYOND LIMITS AFTER BLEND-OUT AT SCREW HOLES IN CENTER OMEGA BEAM GUSSET. R & R GUSSET.SDR ASOA20130304281Sill · corrodedLOWER CORNER OF SERVICE DOOR CUT-OUT REINFORCMENT STRUCTURE IS CORRODED BEYOND LIMITS AFTER BLEND-OUT. R & R SERVICE DOOR SILL.SDR ASOA20130302280Floor Support · corrodedACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND IN A FLOOR SUPPORT ANGLE BETWEEN FRAMES 23 AND 24. MX R & R THE FLOOR SUPPORT ANGLE REF SRM 51-40-02; 51-40-03 AND CPM 51-23-04. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20130302279TCrossbeam · corrodedACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND IN THE CROSS-MEMBER AT FRAME 20. MX REMOVED THE CORROSION AND INSTALLED A NEW PART AT FRAME 20 SRM 51-40-02 AND 51-40-03. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20130302278Frame · corrodedACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND UNDER THE LWR FWD CHAFED PLATE AT CARGO DOOR FRAME 65,STRINGER 17L. MX CUT OUT DAMAGE AREA AND INSTALL A NEW REPAIR ON THE FRAME REF SRM 53-31-04. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CSDR ASOA20130302277Frame · corrodedACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE INTERNAL SIDE OF THE MAIN PAX DOOR ALONG LOWER FRAME AT STR 14L. MX R & R THE AFT AND FWD FRAMES WITH NEW FRAMES REF SRM 51-40-02. ALL WORK COMPLIED WITH AND WILL BE RELEASED AT END OF THE CHECK.SDR ASOA20130301276Sill · corrodedACFT IN IN FOR A C-CHECK WHEN CORROSION WAS FOUND IN THE LT SILL AT SCREW HOLES AT FRAMES 19 AND 20. MX REMOVED THE DAMAGED PART, DRILLED AND INSTALL A NEW SILL RE SRM 51-40-02 AND 51-40-03. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20130301275Structure · corrodedACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE LAV DUMP HOUSING EXTERNAL SIDE AT DUMP CHUTE. MX R & R THE LAV DUMP CHUTE IAW SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20130301274TGusset · corrodedACFT IS IN FOR A C-CHECK WHEN CORROSION WAS FOUND IN THE GUSSET AT THE CENTER OMEGA BEAM AT FRAME 59 THRU 61. MX R & R THE CENTER OMEGA BEAM GUSSET AT FRAME 59 THRU 61 IN REF SRM 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20130301273TFloor Support · corrodedACFT IS IN FOR A C-CHECK THE CENTER OMEGA BEAM AT FRAME 18 TO FRAME 23 WAS FOUND CORRODED AND OUT OF LIMITS. MX R & R A NEW OMEGA BEAM REFERENCING SRM 51-40-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA20120824134Inverter · inoperativeCABIN EMERGENCY EXIT LIGHTS FOR AISLE INOPERATIVE AT ROW 12 AND AFT. R & R EMERGENCY LIGHT INVERTER NR 6 AND R & R FLOOR PROXIMITY LIGHT NR 8. OPS CHECKED GOOD ACFT RELEASED AND RETURNED TO SERVICE.SDR ASOA20120629121TBleed Air Sys · multiple failACFT DIVERTED WITH A BLEED LEAK ISSUE. MX RETORQUED NR 2 ENGINE BLEED VALVE AND THE Y DUCT. RETORQUED SEVERAL NR 2 SYSTEMS PACT DUCTS. OPS AND LEAK CHECKED GOOD IAW CHRONIC WORKSHEET,CONTROL NR 594620. BLEED LEAK TASK CARD 6836001 ON NR 2 SIDE ONLY. ACFT WASDR ASOA20120323034Latch · faultyDURING ROUTINE MX, OXYGEN MASK WOULD NOT DEPLOY AT SEAT 16BC. MX INSPECTED AND REPLACED THE OXYGEN DOOR ELECTRICAL LATCH. OPS CHECKED GOOD.SDR C2XA11RI174Structure · damagedFLT 5864 PWM CREW REPORTED A BIRD STRIKE ON TAKEOFF AND PERFORMED AN AIR RETURN BACK TO PWM WITHOUT INCIDENT. NORTHEAST AVIATION MX PERFORMED BIRD STRIKE INSPECTION IAW EMB145 AMM 05-50-08 WITH DAMAGE NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11IA196Control Unit · inoperativeIAH - FLIGHT 2688, THE CREW REPORTED THAT THE MAIN AND BACKUP PITCH TRIMS WERE INOPERATIVE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT (HSCU), OPERATIONALLY TESTED WITH NO DEFECTS, AND TSDR C2XA11RI134Processor · inoperativeFLIGHT 3065 - EWR - FLIGHT CREW REPORTED CAPT AIR SPEED INOP IN FLIGHT DURING CLIMBING. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVES AND REPLACED AIR DATA PROCESSOR UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TOSDR C2XA11SH048Door Frame · corrodedSHV - DURING C-CHECK SERVICE DOOR LOWER AFT CUTOUT HAS CORROSION AT STR 12R. REPAIRED SERVICE DOOR LOWER AFT CUTOUT IAW EC5310-01373. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA11SH047Support · corrodedSHV - DURING C-CHECK CARGO DOOR LOWER SUPPORT CORRODED. REPLACED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 53-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10SH438Controller · malfunctionedPRESSURIZATION FAILED IN FLIGHT AT FL290. REMOVED AND REPLACED DIGITAL PRESURIZATION CONTROLLER IAW EMB 145 AMM 21-31-01. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA10RI0151Unknown · odorFLIGHT 2736 - EWR - FLIGHT CREW REPORTED ELECTRICAL BURNING ODOR IN GALLEY WHEN COFFEE POTS TURNED ON. EWR MX PERFORMED OPERATIONAL CHECK AND COULD NOT DUPLICATE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA10IA193Battery · overtempIAH - FLIGHT 2751, THE CREW REPORTED A BATT TWO OVERTEMP INDICATION. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA09RI079Warning System · malfunctionedFLIGHT 2331 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. EWR MX RESET AIR GROUND CIRCUIT BREAKERS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09SH067Bushing · migratedSHV - DURING C-CHECK LT AILERON TO PCA FITTING HAS MIGRATED I/B & O/B HAT BUSHINGS O/B SIDE. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177 REV B. PERFORMED BACKLASHES IAW EMB-145 AMM 27-11-00 AND DEFLECTIONS IAW EMB-145 AMM 27-10-0SDR C2XA09SH066Bushing · migratedSHV - DURING C-CHECK HYD SYSTEM 2 RUDDER ACTUATOR UPPER HAT BUSHING AT RUDDER 1 ATTACHMENT MIGRATED. MAINTENANCE INSTALLED NEW RUDDER 1 IAW EMB-145 AMM 27-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09SH065Bushing · migratedSHV - DURING C-CHECK HYDRAULIC SYSTEM 1 RUDDER ACTUATOR UPPER HAT BUSHING AT RUDDER ATTACHMENT MIGRATED. MAINTENANCE INSTALLED NEW RUDDER 1 IAW EMB-145 AMM 27-20-03. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09SH064Fitting · wornSHV - DURING C-CHECK LT AILERON TO PCA FITTING HAS MIGRATED I/B & O/B HAT BUSHINGS O/B SIDE. MAINTENANCE REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177 AND COMPLETED OPS CHECKS IAW EMB 145 AMM 27-11-00 AND AMM 27-10-00-700-801-A. THE AIRCRAFT WSDR C2XA09SH063Inlet · corrodedSHV - DURING C-CHECK LT ENG INLET HAS CORRODED BOLT HOLE. MAINTENANCE REPAIRED LT ENGINE INLET MOUNTING ATTACHMENT FLANGE BOLT HOLE IAW EC5420-01158. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09SH062Sill · corrodedSHV - DURING C-CHECK SERVICE DOOR CENTER SILL HAS CORROSION. MAINTENANCE INSTALLED NEW SERVICE DOOR CENTER SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA09SH061Fitting · corrodedSHV - DURING C-CHECK FRM 65 SHEAR CLIP CORRODED AT LWR BEAM. MAINTENANCE REPAIRED FRM 65 SHEAR CLIP AT LOWER BEAM IAW EC5330-01458. ALODINE, PRIMED AND PAINTED IAW EMB 145 CPM 51-21-06. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA08RI147Controller · inoperativeFLIGHT CREW REPORTED AUTO PRESSURIZATION FAILED DURING TAXI OUT. MX REMOVED AND REPLACED PRESSURIZATION MANUAL CONTROLLER AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K)SDR C2X2008F00033Bulb · inoperativeDURING ROUTINE MAINTENANCE, MX FOUND SEAT 12 BC OVERHEAD SQUARE EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE. (K)SDR C2XA08IA196Ballast · inoperativeIAH FLIGHT 2312 DURING POST FLIGHT INSPECTION THE GALLEY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R&R THE GALLEY EMERGENCY LIGHT BALLAST, OPS CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA07SH031Floorbeam · corrodedSHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20 IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA07SH030Door Frame · corrodedSHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER FRAME HAS CORROSION. MX REMOVED AND REPLACED LOWER FRAME OF CARGO DOOR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR C2XA07IA105Strut · lowIAH - FLIGHT 2887, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE MESSAGE ON TAKEOFF. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE SERVICED THE NOSE LANDING GEAR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RSDR C2XA07RI014Charger · inoperativeDURING ROUTINE MAINTENANCE, MX FOUND LT FWD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED NR 1 EMERGENCY BATTERY CHARGER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO FLIGHT.SDR C2XA07RI007Inverter · inoperativeRIC - MX DURING SCHEDULE ROUTINE MAINTENANACE, MX FOUND 02 EMERGENCY AISLE LIGHTS INOP. MX REMOVED AND REPLACED NR 4 EMERGENCY LIGHT INVERTER. MX PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.SDR C2XA07BT030Battery · inoperativeEWR LOG SQUAWK FLT 2325 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IAW EMB145 AMM 33-50-04. OPS CHECK GOOD.SDR C2XA07IA055Battery · dischargedMAF - FLIGHT 2760, DURING PREFLIGHT THE CREW REPORTED THE AFT THREE EMERGENCY LIGHT STRIPS TO BE INOPERATIVE. THE CREW CHARGED THE EMERGENCY LIGHTS SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA07IA022Light · malfunctionedIAH - FLIGHT 2642, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE AFT EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE RESET THE AFT EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA07CL013Smoke Detector · malfunctionedCLE FLIGHT 2913 THE CREW REPORTED A LAV SMOKE INDICATION INFLIGHT. NO FIRE OR SMOKE WAS PRESENT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONAL CHECKS WERE GOOD.SDR C2XA07CL009Roller · seizedCLE FLIGHT NR 2816, THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND REPLACED THE AFT UPPER ROLLER. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06IA199Battery Pack · dischargedDURING A POST FLIGHT INSPECTION THE AFT EMERGENCY LIGHT AISLE PATH LIGHTING STRIP WAS INOPERATIVE. THE NR 4 EMERGENCY BATTERY PACK WAS REPLACED, THE LIGHTING SYSTEM TESTED AND THE DISCREPANCY CLEARED.SDR C2XA06SD017Power Supply · inoperativeSDF - LT FWD FAIRING EMERGENCY LIGHT, AISLE 1 EMERGENCY LIGHT, AND COCKPIT FLOOD EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 1 EMERGENCY POWER SUPPLY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD.SDR C2XA06TY059Fuse · blownEMERGENCY LIGHT AT TOP OF COCKPIT CEILING INOP. REPLACED FUSE AT NR 1 EMERGENCY BATTERY CRADLE IAW EMB 145 VCMM 25-60-03. OPS CK GOOD AIRCRAFT RETURNED TO SERVICE.SDR C2XA06TY058Fuse · inoperativeFWD EMERGENCY LIGHT LT SIDE INOP. REPLACED FUSE AT NR 1 EMERGENCY LIGHT BATTERY CRADLE IAW EMB-145 VCMM 25-60-03. OPS CK GOOD AIRCRAFT RETURNED TO SERVICE.SDR C2XA06CL069Fuse · blownCLE FLIGHT 2098 THE CREW REPORTED THE OUTER LOWER LEFT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FUSE ON THE NR 1 BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06BT030Charger · inoperativeDURING POSTFLIGHT, CREW REPORTED LEFT FAIRING EMERGENCY LIGHT NOT OPERATING. MAINTENANCE REMOVED AND REPLACED NR 1 EMERGENCY BATTERY CHARGER IAW EMB145 AMM NR 33-50-04, OPS CHECKED GOOD.
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