N578FE
Service difficulty reports · 364
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 = 'N578FE' 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 = 'N578FE' 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 04FDEA02514Spar · corrodedLEFT WING, REAR SPAR, XORS= 540 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 540 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION ANDSDR 04FDEA02513Spar · corrodedLEFT WING, REAR SPAR, XORS= 585 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 585 LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSSDR 04FDEA02512Spar · corrodedLEFT WING, REAR SPAR, XORS= 613 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 613 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION ASDR 04FDEA02511Spar · corrodedLEFT WING, REAR SPAR, XORS= 620 TO XORS= 633, UPPER AND LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 620 TO XORS= 633 UPPER AND LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, SDR 04FDEA02510Spar · corrodedLEFT WING, REAR SPAR, AT XORS 680 TO XORS 687 LOWER CHORD AREA FOUND WITH CORROSION. N1819 ¾ LEFT HAND WING, REAR SPAR, XORS= 680 TO XORS= 687 UPPER AND LOWER CHORD AREA CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WISDR 04FDEA02509Spar · corrodedLEFT WING, REAR SPAR, AT XORS 690 TO XORS 700 LOWER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 690 TO XORS= 700 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LSDR 04FDEA02508Spar · corrodedLEFT WING, REAR SPAR, XORS= 720 UPPER CHORD AREA FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 720 UPPER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION ANDSDR 04FDEA02507Spar · corrodedLEFT WING, REAR SPAR, AT XORS 600 TO XORS 611 LOWER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 611 LOWER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CSDR 04FDEA02506Spar · corrodedLEFT HAND WING, REAR SPAR, UNKNOWN TO XORS= 620 UPPER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 600 TO XORS= 620 UPPER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER SDR 04FDEA02505Spar · corrodedLT WING, REAR SPAR, XORS= 690 UPPER CHORD FOUND WITH CORROSION. LEFT HAND WING, REAR SPAR, XORS= 690 UPPER CHORD CORROSION, REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR CORROSION AND CRACKSDR 04FDEA02504Spar · corrodedLEFT WING, REAR SPAR, AT XORS= 713 UPPER CHORD FOUND WITH CORROSION. LEFT WING, REAR SPAR, XORS= 713 UPPER CHORD CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA NR 1-5710-76826, WINGS, LEFT UPPER AND LOWER REAR SPAR, CORROSION AND CRACSDR 04FDEA02503Splice · crackedMAIN DECK, RIGHT HAND SIDE STA 5-113 STA 1541 LONGERON 25 FOUND CRACKED. MAIN DECK, RIGHT HAND SIDE STA 5-11 TO STA 1541 DAMAGED. LONGERON 25 CUT, REMOVED AND FABRICATED PER SRM 53-10-00 TYPE 1 VOLUME I. FABRICATED REPAIR PARTS AND EXISTING SPLICE INSTALLSDR 04FDEA02528Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AREA AT XORS 730 TO XORS 755 FOUND WTH CORROSION. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.SDR 04FDEA02527Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AREA AT XORS 680 TO XORS 690 FOUND WTH CORROSION. CORROSION REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.SDR 04FDEA02526Spar · corrodedRT WING, REAR SPAR, LOWER CHORD AT XORS 650 AREA FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.SDR 04FDEA02525Spar · corrodedRT WING, REAR SPAR, UPPER CHORD AT XORS 600 TO XORS 650 FOUND WITH CORROSION. CORROSION REMOVED PER SRM 51-31-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB - CORROSION AND CRACK REPAIR.SDR 04FDEA02502Frame · corrodedAFT CARGO, AFTER REMOVAL OF DOOR CUTOUT AFT LOWER LINER, CORROSION FOUND ON FRAME SIDE SURFACE AT STA 1959. AFT CARGO, CORROSION ON FRAME SIDE SURFACE AT STA 1959 REMOVED PER SRM 53-00-01 FIGURE 3 VOLUME I. MATERIAL THICKNESS= 0.130 INCH, MATERIAL REMOVED=SDR 04FDEA02501Shear Tie · corrodedAFT CARGO, AFTER FLOOR PANEL NR 187DF REMOVAL FOR ACCESS, CORROSION FOUND AT STA 1964 BETWEEN LONGERON 47L AND 48L. AFT CARGO, STA 1964 BETWEEN LONGERON 47L AND 48L SHEAR TIE CLIP. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II.SDR 04FDEA02488Longeron · corrodedCENTER CARGO, CORROSION OBSERVED ON LONGERON 46R BETWEEN STA 1701 AND STA 1721. CENTER CARGO, STA 1671 TO STA 1811 LONGERON 46R REMOVED AND NEW LONGERON P/N AFA7098-501, INSTALLED PER DWG AFA7098, SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II.SDR 04FDEA02485Skin · corrodedCENTER WING TANK, STA 1219 - STA 1239, LBL 27 - LBL 47 HORIZONTAL PRESSURE PANEL TOP SURFACE CORRODED. CORROSION REMOVED, MATERIAL ORIGINAL THICKNESS = 0.175 INCH, MATERIAL REMOVED = 0.017 INCH, REMAINING MATERIAL = 0.158 INCH AND FOUND WITHIN LIMITS AS PERSDR 04FDEA02486Web · canningCENTER LANDING GEAR WHEEL WELL, LEFT VERTICAL WEB FOUND WITH OIL CANNING CONDITION. CENTER LANDING GEAR WHEEL WELL, LEFT VERTICAL WEB INSPECTION CARRIED OUT AND FOUND WITHIN SRM 53-00-01 VOLUME I LIMITS. STA Y= 1394-1401, Z= 100-115, 0.087" STA Y= 1401-14SDR 04FDEA02489Frame · gougedMAIN DECK, LEFT SIDE 9G NET ATTACH YOKE ASSEMBLY AT FRAME STA Y= 535 FOUND WITH GOUGE MARK. MAIN DECK, LEFT SIDE 9G NET ATTACH YOKE ASSEMBLY FRAME AT STA Y= 535 CARRIED OUT REPAIR AS PER DWG NR: SRZ-53-503 AND SRM51-31-01 VOLUME II.SDR 04FDEA02487Web · canningCENTER LANDING GEAR WHEEL WELL, RT VERTICAL WEB FOUND WITH OIL CANNING CONDITION. CENTER LANDING GEAR WHEEL WELL, RT VERTICAL WEB INSPECTION CARRIED OUT AND FOUND WITHIN SRM 53-00-01 VOLUME I LIMITS. STA Y= 1394-1401, Z= 100-115, 0.067" STA Y= 1401-1411, SDR 04FDEA02481Spar · corrodedRT WING, REAR SPAR UPPER CHORD XORS= 1079 FOUND WITH CORROSION. RT WING, REAR SPAR UPPER CHORD XORS= 1079 CORROSION REMOVED PER SRM 51-21-01 VOLUME II COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACSDR 04FDEA02480Spar · corrodedRT WING, REAR SPAR UPPER CHORD XORS= 1042 FOUND WITH CORROSION. RT WING, REAR SPAR UPPER CHORD XORS= 1042 CORROSION REMOVED PER SRM 51-21-01 VOLUME II, COMPLIED WITH FEDEX EA NR 1-5710-76824, WINGS, RIGHT UPPER AND LOWER REAR SPAR AND WEB, CORROSION AND CRACKSDR 04FDEA02479Spar Cap · corrodedRT WING, WING PLANK, UPPER SURFACE, MOST OUTBOARD AFT CORNER ABOUT XORS= 1090 TO XORS= 1094 FOUND WITH CORROSION AND FIXED TRAILING EDGE PANEL FOUND BULGING. RT WING, WING PLANK, UPPER SURFACE, MOST OUTBOARD AFT CORNER XORS= 1090 TO XORS= 1094 CORROSION REMSDR 04FDEA02475Longeron · corrodedFORWARD CARGO, CORROSION OBSERVED ON LONGERON 43R STA 1125. TRIMMED OFF AS PER SRM 53-10-00 VOLUME 1. REPAIR LONGERON FABRICATED AND INSTALLED AS PER SRM 53-10-00 VOLUME 1.SDR 04FDEA02430Intercostal · corrodedINTERCOSTAL BETWEEN STA 1481 AND STA 1501 AT LONGERON 19R FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II.SDR 04FDEA02429Intercostal · corrodedMAIN DECK INTERCOSTAL BETWEEN STA 1481 AND STA 1501 AT LONGERON 19R FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II PAGE 27. MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.096, ORIGINAL THICKNESS = 0.100 FOUND WITHIN LIMITS PER SRM 53-00-01 VOLSDR 04FDEA02428Intercostal · corrodedINTERCOSTAL BETWEEN STA 1361 AND STA 1381 AT LONGERON 15R FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II.SDR 04FDEA02427Intercostal · corrodedINTERCOSTAL BETWEEN STA 1341 AND STA 1361 AT LONGERON 15R FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II.SDR 04FDEA02426Intercostal · corrodedINTERCOSTAL BETWEEN STA 1175 AND STA 1199 AT LONGERON 15R FOUND CORRODED. REMOVED AND REPLACED AS PER 51-33-01 VOLUME II.SDR 04FDEA02425Intercostal · corrodedINTERCOSTAL BETWEEN STA 1159 AND STA 1175 AT LONGERON 15R FOUND CORRODED. REMOVED AND REPLACED AS PER MD-11 SRM 53-33-01.SDR 04FDEA02424Intercostal · corrodedMAIN DECK INTERCOSTAL BETWEEN STA 1341 AND STA 1361 AT LONGERON 19L FOUND CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME II PAGE 27. MATERIAL REMOVED = 0.005, REMAINING THICKNESS = 0.095, ORIGINAL THICKNESS = 0.100 FOUND WITHIN LIMITS PER SRM 53-00-01 VOSDR 04FDEA02423Intercostal · corrodedMAIN DECK - INTERCOSTAL BETWEEN STA 1175 AND STA 1199 AT LONGERON 15R FOUND CORRODED. REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II.SDR 04FDEA02422Intercostal · corrodedINTERCOSTAL BETWEEN STA 1421 AND STA 1441 AT LONGERON 15L FOUND CORRODED. INTERCOSTAL REMOVED AND REPLACED PER SRM 51-33-01 VOLUME II.SDR 04FDEA02421Longeron · corrodedCORROSION FOUND BETWEEN STA 6-70 AND STA 6-90 AT LONGERON 15L. REMOVED AS PER MD-11 SRM 51-31-01 VOLUME I. NEW LONGERON FABRICATED AS PER DWG NO.: ADA3011 AND FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOLUME I.SDR 04FDEA02420Longeron · corrodedCORROSION FOUND BETWEEN STA 6-50 AND STA 6-70 AT LONGERON 15L. REMOVED AS PER MD-11 SRM 51-31-01 VOLUME I. NEW LONGERON FABRICATED AS PER DWG NO.: ADA3011 AND FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOLUME I.SDR 04FDEA02419Longeron · corrodedCORROSION FOUND BETWEEN STA 6-30 AND STA 6-50 AT LONGERON 15L. REMOVED AS PER MD-11 SRM 51-31-01 VOLUME I. NEW LONGERON FABRICATED AS PER DWG NO.: ADA3011 AND FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOLUME I.SDR 04FDEA02418Longeron · corrodedMAIN DECK CORROSION FOUND BETWEEN STA 6-10 AND STA 6-30 AT LONGERON 15R. CORRODED LONGERON REMOVED AS PER MD-11 SRM 51-31-01 VOLUME I. LONGERON FABRICATED AS PER DWG NR.: ADA3011. FABRICATED LONGERON INSTALLED AS PER MD-11 SRM 51-31-01 VOLUME I.SDR 04FDEA02395Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE OB PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLECORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.097. COMPLIED WITH FEDEX EA 1-5750-76808, SDR 04FDEA02400Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE IB ACTUATOR ROD END ATTACHING HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.408, MATERIAL REMOVED = 0.002, REMAINING THICKNESS = 0.406. COMPLIED WITH FEDEX EA 1-5750-76808, LEFSDR 04FDEA02399Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE IB ACTUATOR ROD END ATTACHING HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.090. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGESDR 04FDEA02398Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE PIVOT HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.504, MATERIAL REMOVED = 0.010, REMAINING THICKNESS = 0.494. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLSDR 04FDEA02397Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER=1.082, FINAL DIAMETER=1.097. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA02396Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE PIVOT HOLE OB FLANGE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD FLANGE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.503, MATERIAL REMOVED = 0.004, REMAINING THICKNESS =SDR 04FDEA02414Longeron · corrodedCENTER CARGO, CORROSION OBSERVED ON LONGERON 52 SPLICE BETWEEN STA 1701 AND STA 1721. CORROSION REMOVED PER SRM 53-00-01 FIGURE 3 VOLUME 1. MATERIAL THICKNESS= 0.125, MATERIAL REMOVED= 0.020, MATERIAL REMAINING= 0.105. WITHIN LIMITS PER SRM 53-00-01 FIGURE 3SDR 04FDEA02413Skin · corrodedRT WING, WING UNDER SURFACE JUST ABOVE NR 3 PYLON FWD INBOARD OF THRUST LINK CORRODED. CORROSION REMOVED PER SRM 51-21-01 VOLUME I. COMPLIED WITH FEDEX EA 1-5750-76815, WINGS RT WING - LOWER FORWARD PANEL ASSEMBLY - CORRODED.SDR 04FDEA02412Skin · dentedRIGHT FUSELAGE SKIN AT STA Y= 1847, LONGERON 34R FOUND WIND DENT MARK. SKIN TRIMMED-OFF AND REPAIRED PER MD-11 SRM 53-20-00 VOLUME I FIGURE 2.SDR 04FDEA02411Longeron · corrodedCENTER CARGO, CORROSION OBSERVED ON LONGERON 46R BETWEEN STA 1741 AND 1761. LONGERON 46R REMOVED AND NEW LONGERON P/N AFA7098-501 INSTALLED PER DWG AFA7098, SRM 51-33-01 VOLUME II AND SRM 51-35-01 VOLUME II.
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