N952U, cancelled Feb 28, 2017
Service difficulty reports · 39
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 = 'N952U' AND deregistration_id = 'N952U-2017-02-28' 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 = 'N952U' AND deregistration_id = 'N952U-2017-02-28' 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 ZW0A0212602Power Supply · dischargedTHE TAIL COMPARTMENT EMERGENCY WHITE LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY.SDR ZW0A0212601Power Supply · dischargedTHE CEILING EMERGENCY LIGHTS WERE INOPERATIVE FROM THE GALLEYS TO THE AFT LAVS, ROW 12 THROUGH 22, AND ABOVE THE AFT FLIGHT ATTENDANT POSITION. REPLACED THE POWER SUPPLY FOR EACH OF THE LOCATIONS.SDR ZW0A0210602Control Cable · brokenDURING OVERNIGHT MAINTENANCE CHECKS THE NUMBER 5 L/E SLAT RETRACT CABLE WAS FOUND BROKEN. REPLACED THE CABLE.SDR ZW0A0101203Light · inoperativeTHE TAIL CONE SLIDE LIGHT AND TAIL CONE EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE LAMPS. CHECK-C 3-12-01 STL.SDR TWAA0104901Regulator Valve · malfunctionedWITH WING ANTI-ICE ON, HOT SMOKEY SMELL FILLED THE CABIN. REPLACED THE RIGHT ANTI-ICE PRESSURE REGULATING VALVE. CHECK-C 3-3-01 STL.SDR TWAA0101002Battery · dischargedTHE FIRST CLASS OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED TWO BATTERIES IN POWER SUPPLY. CHECK-C 3-3-00 MCI.SDR TWAA0020002Turbine · failedIN CLIMB THE NR 1 ENGINE SHUT DOWN. FLIGHT RETURNED TO STL. FOUND TURBINE FAILURE. CHANGED THE ENGINE. CHECK-C 3-3-00 MCI.SDR TWAA0003602Seal · leakingDURING TAKEOFF, LOUD NOISE FROM AFT STAIR DOOR. LUBRICATED AFT STAIR DOOR SEAL AND PRESSURIZED AIRCRAFT WITH NO NOISE NOTED. AC05 2-17-00 MCI.SDR TWAA0003205Skin · corrodedDURING CHECK-C MAINT, FOUND CORROSION BETWEEN SKIN PANELS AT LOWER EDGE OF FWD CARGO DOOR CUTOUT, STA 389 AND 408, AROUND RIVET AT STA 391, AND SCRATCHES. REMOVED CORROSION AND BLENDED SCRATCHES AND INSTALLED REPAIR PER ARA 16536A.SDR TWAA0002906Skin · damagedDURING CHECK-C MAINT, THE FWD LT ENTRY DOOR, BOTTOM EDGE OF THE DOOR THE ENTIRE LENGTH SKIN WAS PUSHED .25 IN FWD, AND .33 OF THE AREA INCLUDED PREVIOUS REPAIR. REPAIRED PER ARA 16528 AND SRM 53-04, FIG 12B.SDR TWAA0003015Skin · bentDURING CHECK-C MAINT, FOUND SKIN DAMAGED/BENT AT TOP OF RUDDER SPAR CAP, RT SIDE. ACCOMP HIGH FREQ EDDY CURRENT AND CHECKED AREA. RECONTOURED AREA RECHECKED WITH HFEC PER ARA 16525.SDR TWAA0002607Frame · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON THE AFT BULKHEAD ATTACH FRAME AT 3 NUT PLATE HOLES, LEFT OF CENTER STA 1338 AT LBL 15. REMOVED AND REPLACED ATTACH FRAME.SDR TWAA0002311Skin · corrodedDURING CHECK-C MAINTENANCE, FOUND CORROSION ON FUSELAGE SKIN AT STA 769 TO 807, AT RUB STRIP FOR LOWER RT FUSELAGE FAIRING. REMOVED CORROSION AND REPAIRED AREA PER SRM 53-04, FIG 53.SDR TWAA0002310Skin · corrodedDURING CHECK-C MAINTENANCE, FOUND CORROSION ON LOWER FUSELAGE SKIN AT RUB STRIP FOR RT WING TO FUSELAGE FAIRING AT STA 764, 771, 775, AND 777. REMOVED CORROSION PER SPM 6-80-01. ALODINED AND PRIMED AND INSTALLED DOUBLER PER SRM 53-04, PAGE 321.SDR TWAA0002309Skin · damagedDURING CHECK-C MAINTENANCE, THE RT OTBD TE FLAP TE WAS DAMAGED 46 IN FROM INBD END. CUT OUT AREA AND SPLICED IN REPAIR SECTION PER SRM 57-03 PAGE 12.SDR TWAA0002308Door Sill · corrodedDURING CHECK-C MAINTENANCE, THE FORWARD SERVICE DOOR SILL PANEL WAS CORRODED. REPLACED DOOR SILL PANEL WITH NEW PANEL.SDR TWAA0002207Skin · damagedDURING MSG24 MAINTENANCE, FOUND FUSELAGE SKIN DAMAGED AT THE FORWARD EDGE OF THE MID CARGO DOOR OPENING APPROXIMATELY 3 FASTNERS BELOW THE NUMBER 3 STOP. INSTALLED SKIN REPAIR PER DAC PRINT SRO9530108 VIEW 1003 PER ENGINEER TASK 004.SDR TWAA0002206Floorbeam · corrodedDURING MSG24 MAINTENANCE, FOUND CORROSION ON CABIN FLOOR SUPPORT AT STA 150-200, RBL6. REMOVED CORROSION PER SRM 51-10-3.. REPLACED WITH NEW PART PER SRM 51-10 PG 1 PAR C, SRM 6-70-02. INSTALLED FASTNERS PER SRM 51-30-PG1 PART NUMBER 07-91.SDR TWAA0002205Floorbeam · corrodedDURING MSG24 MAINTENANCE CORROSION WAS FOUND AT CABIN FLOOR SUPPORT STATION 160 RBL 6 AND RBL5. REMOVED CORROSION PER SRM 51-10-3. REPLACED WITH NEW PART PER SRM 51-01 P71 PAR C AND SRM 6-70-01. INSTALLED FASTNERS PER SRM 51-30-2 PG9, PART NUMBER 07-91.SDR TWAA0002301Floorbeam · corrodedDURING CHECK-C MAINTENANCE, FOUND CORROSION IN THE AFT CARGO COMPT ON FLOOR SUPPORT STA 1212, RBL 9 TO 15. INSTALLED NEW SUPPORT PN 5936597-509 PER SRM 51-30-2 AND 51-30-0.SDR TWAA0002014Skin · gougedDURING CHECK-C MAINTENANCE, FOUND SHARP EDGE GOUGE MARKS AND DENT APPROX 15 IN FWD OF MAIN ENTRY DOOR AND APPROX 4 IN ABOVE THE FLOOR LINE. DIMENSIONS MEASURE 2 IN W BY 3 IN H TIMES 0.052 DEEP. NDT TEST INDICATED MINIMUM SKIN THICKNESS OF 0.040 PER PART 51-0SDR TWAA0001906Hinge Plate · corrodedDURING CHECK-C MAINT, THE HORIZONTAL STABILIZER RT I/B PIVOT BEARING HINGE PLATES WERE CORRODED/PITTED IN BORE. REAMED, BUSHED AND FINAL HONED TO DIMENSION PER SRM 55-02.SDR TWAA0001905Hinge Plate · corrodedDURING CHECK-C MAINT, THE HORIZONTAL STABILIZER LT O/B PIVOT BEARING HINGE PLATES WERE CORRODED AND PITTED IN BORE. REAMED HOLE, BUSHED AND FINAL HONED PER SRM 55-02.SDR TWAA0001904Hinge Plate · corrodedDURING CHECK-C MAINT, THE HORIZONTAL STABILIZER LT I/B PIVOT BEARING HINGE PLATES HAD CORROSION AND PITTING IN THE BORE. REAMED HOLE TO REMOVED CORROSION. HOLE DIMENSION 1.435 PER SRM 55-02. INSTALLED BUSHINGS AND FINAL HOLE DIM PER SRM 55-02.SDR TWAA0001903Floorbeam · corrodedDURING CHECK-C MAINT, THE AFT CARGO FLOOR SUPPORT AND ANGLE THRESHOLD TRANSITION HAD CORROSION AT NUT PLATE AREA. REMOVED OLD ANGLE AND REPLACED WITH PER DAC DRAWING 5936587 AND SPM 6-70-01, PAGE 3 PARA B. ALSO SRM 51-30-2 RIVETS 51-30-1 AND 51-20-0.SDR TWAA0001902Longeron · crackedDURING CHECK-C MAINT, FOUND A CRACK IN LONGERON 4L, STA 160. REPLACED LONGERON 4L PER SPM 6-70-01, PAGE 1 AND 4.SDR TWAA0001907Floorbeam · corrodedDURING OP 16 MAINT CHECK, THE CABIN STA 1251 FLOOR SUPPORT WAS CORRODED BETWEEN NUMBER 1 AND 2 SEAT TRACKS. REMOVED CORRODED FLOOR SUPPORT AND FABRICATED PART PER SPM 6-70-01, PER DOUGLAS PN 5930544-97, AND INSTALLED PER SRM 51-30-02. TREATED AND PRIMED PER SDR TWAA0001612Threshold · corrodedDURING CHECK-C MAINT THE AFT CARGO DOOR SILL THRESHOLD HAD CORROSION UNDER THE SILL PLATE SUPPORT. REPLACED SUPPORT WITH (P/N 5936660-67). REPLACED RIVETS AND BOLTS PER SRM 51-30-02 AND 51-30-0.SDR TWAA0001611Bearing · corrodedDURING CHECK-C MAINT THE HORIZONTAL STABILIZER O/B PIVOT BEARING, RT SIDE, INNER AND OUTER PLATES WERE RUSTY AND PITTED. REMOVED RT O/B, INNER AND OUTER PLATES AND INSTALLED NEW PLATES PER MO 72N10.SDR TWAA0001610Seat Track · corrodedDURING CHECK-C MAINT THE CABIN RT O/B TRACK NUMBER 4 HAD CORROSION AT STA 262 TO 269. BLENDED AREA FREE OF CORROSION PER SPM 6-80-01 USING LIMITS PER SRM 57-05 FIG 4B SHEET 2 AND 3. AREA REFINISHED PER SRM 51-10-03 PAGE 14.SDR TWAA0002302Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON AFT CARGO COMPT FLOOR SUPPORT STA 1155 TO 1212, RBL 8. REMOVED CORROSION ON FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01 DRAWING 5936020.SDR TWAA0001609Tab · brokenDURING CHECK-C MAINT FOUND FWD GALLEY DOOR TAB BROKEN ON DOOR FRAME, INNER PLATE, STA 207 AT LONGERON 15L. MADE DOUBLER TO REPAIR BROKEN TAB PER ARA 16527. SEALED DOUBLER WITH PR1022-1/2A.SDR TWAA0001608Longeron · bentDURING CHECK-C MAINT LONGERON 15R WAS BENT EXCESSIVELY, TWO PLACES ALONG EDGE, STA 842, 3 INCHES FWD OF FORMER, STRINGER 845 FRAME. REMOVED DAMAGED AREA OF FREE FLANGE PER LIMITS OF SRM 53-01, PAGE 4, TABLE 1.SDR TWAA9914401Battery · dischargedEMERGENCY EGRESS LIGHTS INOP ROWS 8, 9 AND 11. REPLACED BATTERY. CHECK C 03/26/99 STL.SDR TWAA9818905Oven · failedDURING DESCENT, SMOKE IN FIRST CLASS CABIN. REPLACED GALLEY OVEN.SDR TWAA9800501Door · not closedSTL - FLT 350 - DURING FLIGHT CLIMB, CABIN WOULD NOT PRESSURIZE IN AUTO OR MANUAL. CLOSED L-2 DOOR PROPERLY. (M)SDR TWAA9719001Heat Exchanger · failedJFK - DURING CRUISE, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. REMOVED AND REPLACED RIGHT HAND SECONDARY HEAT EXCHANGER, MFG P/N 184060-3-2. OPERATIONAL CHECK NORMAL. (M)SDR 96ZZZX3032Prox Sensor · failedSTL - FLT 24 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NLG RED UNSAFE LIGHT REMAINED ILLUMINATED. VERIFIED NLG RETRACTION BY MECHANICAL INDICATOR. FOUND NLG PROXIMITY SENSOR, MFG PN 8-337-03, FAULTY. REPLACED NLG PROXIMITY SENSOR. NLG INDICATION THESDR 96ZZZX1203Engine · failedSTL - FLT 414 - DURING CLIMB, LT ENGINE SURGED ACCOMPANIED WITH A DROP IN EPR. SHUT DOWN LT ENGINE, SN 3201. FOUND METAL PARTICLES IN TAILPIPE AND TURBINE BLADE DAMAGE. CHANGED LT ENGINE AND ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 31,874 HRS;
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