N164D
Service difficulty reports not matched to an aircraft · 57
They name N164D, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N164D' AND registry_match IS NULL 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 = 'N164D' AND registry_match IS NULL 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 COMA9910073Smoke Detector · malfunctionedLAV SMOKE DETECTOR ACTIVATED. F/A AND PASSENGERS REPORTED SMOKE SMELL. REPLACED THE SMOKE DETECTOR.SDR COMA9910012Sign · fell offEMERGENCY EXIT SIGN AT ROW 5 FELL OFF. REPLACED EXIT SIGN.SDR COMA9910008Striker · out of adjustCARGO DOOR WARNING AFTER TAKEOFF. ADJUSTED CARGO DOOR SWITCH STRIKER.SDR COMA9910007Sign · brokenEMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN.SDR COMA9810290Ahrs · out of adjustAHRS INTERMITTENT DURING TAKEOFF. REORIENTED NR 1 AHRS.SDR COMA9810237Eec · failedLEFT ENGINE EEC FAILED ON TAKEOFF. REPLACED LEFT ENGINE EEC.SDR COMA9810192Doubler · crackedDOUBLER ON POST BETWEEN DIRECT VISION WINDOW AND NR 1 WINDOW IS CRACKED BELOW HANDLE. REMOVED DOUBLER AND REPLACED WITH SERVICEABLE DOUBLER. ALSO COMPLIED WITH S/B 120-53-0045 IAW EMB 120 S/B 120-53-0045.SDR COMA9810079Skin · broken offDURING LEAK CHECK OF CARGO DOOR SEAL FOUND AN AREA OF CARGO DOOR SKIN MISSING (BROKEN OFF) FROM UPPER AFT CORNER, MISSING SKIN AREA WAS 3.75 INCH LONG AND .625 IN FROM OUTER EDGE OF SKIN. NO DAMAGE TO DOOR FRAME WAS FOUND. THE CARGO DOOR SKIN WAS REPAIRED ISDR COMA9710390Battery · dischargedEMERGENCY LIGHTS AT ROW 5 WILL ONLY ILLUMINATE FOR 2 TO 3 SECONDS. REPLACED EMERGENCY LIGHTS BATTERY.SDR COMA9710317Light · inoperativeEMERGENCY LIGHTING AT GALLEY FLOOR IS INOP. REPLACED LIGHT ASSY.SDR COMA9710314Battery · dischargedCABIN EMERGENCY LIGHTS ROWS 2 TO 5 ARE INOP. REPLACED THREE EMERGENCY LIGHTING BATTERIES. S/N 439, 727 AND 794.SDR COMA970213Prox Switch · failedTHE LANDING GEAR SELECTOR LEVER WOULD NOT MOVE TO THE RETRACT POSITION. REPLACED DEFECTIVE WEIGHT ON WHEELS PROXIMITY SWITCH ON THE LT MLG.SDR COMA9710163Selector Control · malfunctionWHEN LANDING GEAR SELECTED UP, THE LEFT HAND MLG INTRANSIT LIGHTS REMAINED ON. REPLACED THE SELECTOR CONTROL ASSY.SDR COMA9710133Annunciator · malfunctionFLAP CONTROL FAULT WARNING DURING TAXI. REPLACED THE FLAP ANNUNCIATOR PANEL. PART TOTAL CYCLES, 8,700.SDR COMA9710123Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710122Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710121Beam · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT OMEGA BEAM WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710120Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710119Butt Strap · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER AERODESIGN REPORT NR 1671-1, REV A, DATED 1-28-97.SDR COMA9710118Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710117Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710116Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710115Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710114Sill · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710113Supporting Sect · corrodedON 2C CHECK, THE LT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. THE PART WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA9710112Supporting Sect · corrodedON 2C CHECK, THE RT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. THE PART WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA9710111Crossbeam · corrodedON 2C CHECK, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT CROSSBEAM WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710110Support · corrodedON 2C CHECK, THE LOWER FUSELAGE SKIN SUPPORT AT FRAME 14 WAS FOUND CORRODED. THE PART WAS REPLACED PER EMB 120 SRM STANDARD PRACTICES.SDR COMA9710109Angle · corrodedON 2C CHECK, THE ATTACHING ANGLE AT STRINGER 18L, BETWEEN FRAMES 15 AND 15A WAS FOUND CORRODED. THE PART WAS REPLACED WITH A NEW PART PER SRM STANDARD PRACTICES.SDR COMA9710108Supporting Sect · corrodedON 2C CHECK, THE RT FWD SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. THE PART WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA9710107Stringer · corrodedON 2C CHECK, THE FUSELAGE STRINGER 18L WAS FOUND TO BE CORRODED NEAR FRAME 16, THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 1990-5, REV IR, DATED 1-28-97.SDR COMA9710106Sill · gougedON 2C CHECK, THE CARGO COMPARTMENT FLOOR SUPPORT LT SILL WAS FOUND DAMGED BY INTERIOR LINING SCREWS. THE SILL WAS REPLACED PER SRM STANDARD PRACTICES.SDR COMA9710105Skin · gougedON 2C CHECK, THE CARGO DOOR OUTER SKIN WAS FOUND TO BE GOUGED ALONG THE TOP EDGE, CAUSED BY THE FUSELAGE MOUNTED DOOR STOPS. THE SKIN WAS REPAIRED PER SRM 52-30-01, PG 201 TO 203.SDR COMA9710076Prox Sensor · inoperativeGEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED LT MLG WOW PROX SENSOR.SDR COMA9710043Stringer · dentedTHE LEFT NACELLE OUTBOARD STRINGER NR 1 WAS DAMAGED BY THE FORWARD GEAR DOOR TENSIONER WHICH HAD DISCONNECTED BECAUSE THE RETAINING BOLT FELL OUT. THE LT STRINGER NR 1 HAD BEEN PREVIOUSLY REPAIRED BY INSERTION FOR THE SAME REASON. SINCE THE INSERTION REPAIR SDR COMA9710031Gear Handle · malfunctionedGEAR HANDLE IN UP POSITION VERY LOOSE. REPLACED GEAR HANDLE. OPERATIONAL CHECK GOOD. PART TOTAL CYCLES, 19,478.SDR COMA9660180Current Sensor · failedPITOT STATIC HEAT INOP. REPLACED THE CURRENT SENSOR.SDR COMA9610246Wire · failedEMERGENCY FLOOR LIGHTING IS DIM. REPAIRED FLOOR PATH LIGHTING WIRING AT FRAME 24. SYSTEM CHECK SATISFACTORY.SDR COMA9610200Battery · dischargedEMERGENCY LIGHTING AT THE CABIN MID SECTION IS DIM. REPLACED EMERGENCY BATTERY.SDR COMA9610195Skin · corrodedDURING C-1 INSPECTION, FOUND LOWER FUSELAGE SKIN AT FRAME 21 TO SHOW SIGNS OF CORROSION (SKIN BULGING). FURTHER INVESTIGATION FOUND THAT SMALL AREA BETWEEN SKIN AND TITANIUM STRAP WAS, IN FACT, CORRODED BETWEEN STRINGERS 2DL AND 2DR. REPAIR WAS DONE BY CUTTISDR COMA9610181Servo · malfunctionPILOTS STICK SHAKER IS ON CONTINUOUSLY. REPLACED THE PILOTS STICK SHAKER.SDR COMA9610230Ballscrew Servo · defectiveAD-94-22-12. WHILE PERFORMING HAMILTON STANDARD SB 14RF-9-61-A53 REV. S, FOUND THE SPLINES OF THE BALLSCREW SERVO WERE WORN BEYOND LIMITS PRIMARILY ON THE RIGHT SIDE OF THE SPLINES. ACTION TAKEN: SENT PCU OUT TO HAMILTON STANDARD FOR FURTHER EVALUATION.SDR COMA9610178Spline · defectiveWHILE PERFORMING AD-94-22-12 HAMILTON STANDARD S/B 14RF9-61-A53 REV S. FOUND THE SPLINES OF THE BALLSCREW SERVO WORN BEYOND LIMITS PRIMARILY ON THE RIGHT SIDE OF THE SPLINES. SENT PCU OUT TO HAMILTON STANDARD FOR FURTHER EVALUATION.SDR COMA9610108Prox Sensor · failedTAKEOFF TRIM AURAL WARNING SOUNDS WHEN TRIM IS CORRECTLY SET IN TAKEOFF RANGE. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSOR.SDR COMA9610102Circuit Breaker · trippedFLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER IS TRIPPED. RESET BREAKER, SYSTEM TEST NORMAL.SDR COMA9610041Actuator · defectiveFLAP ASYMMETRY WARNING AFTER LANDING. REPLACED THE RT OUTBD FLAP ACTUATOR.SDR COMA9512039Actuator · defectiveAFTER LANDING WHEN FLAPS SELECTED UP, CONTROL FAULT WARNING ACTIVATED. REPLACED THE RT INBD FLAP ACTUATOR.SDR COMA9512032Control Unit · defectiveFLAP CONTROL FAULT, ASYMMETRY, AND DISAGREEMENT WARNINGS, ZERO FLAPS LANDING. REPLACED THE FLAP CONTROL UNIT AND ANNUNCIATOR PANEL.SDR COMA9512036Actuator · defectiveFLAP CONTROL FAULT, FLAP DISAGREEMENT, AND FLAP ASYMMETRY WARNINGS WHEN FLAPS SELECTED TO 15 DEGREES FOR LANDING APPROACH. REPLACED THE LT AND RT INBD FLAP ACTUATORS.SDR COMA9512022Acm · failedDURING FLIGHT, OIL SMELL FROM BOTH COOLING PACKS. REPLACED THE RT AIR CYCLE MACHINE.
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