N574FE
Service difficulty reports · 611
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 = 'N574FE' 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 = 'N574FE' 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 FDEA2019123183317Panel · corrodedMAIN CARGO DECK, STA1346 LBL108, CENTER WING UPPER PANEL HAS CORROSION (MARKED) REMOVED FASTENERS, REMOVED CORROSION, NDT WAS CALLED OUT TO DO A REMAINING THICKNESS CHECK, FOUND AREA TO BE WITHIN ALLOWABLE LIMITS OF SRM 57-10-01-1A FIG 101 & INSPECTED ALSDR FDEA2019123173316Panel · corrodedMAIN CARGO DECK, STA1335 LBL105 TO LBL113, CENTER WING UPPER PANEL HAS CORROSION (MARKED) REMOVED FASTENERS, REMOVED CORROSION, NDT CHECK FOR MATERIAL LOSS, FOUND AREA TO BE WITHIN ALLOWABLE LIMITS PER SRM 57-10-01-1A FIG 101 & EA # 1-5710- T03511416, PSDR FDEA2019123123339Floor Support · corrodedCTR CARGO - STA 1800 RBL 51 FLOOR SUPPORT SHOWS CORROSION MARKED DOT #3. REPLACED FLOOR SUPPORT PER DWG AFA7299. REMOVED CORRODED FLOOR SUPPORT SRM 51-31-0G-0 INSTALLED NEW FLOOR SUPPORT PER DWG AFA7299 & SRM 51-31-0G., MATERIAL VERIFIED S2929841 PER DWSDR FDEA2020011680138Frame · corrodedAFT CARGO COMPT - STA 1964 AT L46 SHOWS CORROSION ON FRAME. REPAIRED NOTED AREA OF CORROSION I.A.W. SRM 53-00-07-2R FIG 202 SHT 1.SDR FDEA2019120653193Wedge · damagedR/H O/B FLAP TRAILING EDGE DAMAGED REMOVED AND REPLACED R/H O/B FLAP I/B SECTION TRAILING EDGE PER DWG NRC6753SDR FDEA2019122063268Skin · corrodedL/E SKIN CORRODED ON R/H HORIZONTAL L/E SECTION 341BT...(MRK) 5121818: CONSIGNADO, FREDERICK J - 17-DEC-2019 22:02 REMOVED DAMAGED ON L/E, R/H HORIZ @ APPROX XFS 97. INSTALLED REPAIR PER SRM 55-10-02-2R REPAIR 1 FIG 201 SEE ATTACHMENTS NR 1274 AMT# RRB 828SDR FDEA2019112643298Channel · corrodedCTR CARGO STA 1781 LBL 28 CARGO COMPARTMENT CONVEYOR CHANNEL UNDER LATCH ASSY IS CORRODED OUT OF LIMITS REMOVED AND REPLACE CHANNEL ASSY P/N# AFJ7014-507 REF DOUGLAS DWG AFJ7014A AND SRM 51-31-01-0G.SDR FDEA2020021490328Spar Cap · corrodedR/H WING, UPPER REAR SPAR, STATION XORS 793 HAS SURFACE CORROSION. PERFORMED STRAP/ANGLE REPAIR PER EA T 1-5710-T0352042 P1SDR FDEA2020021490321Spar Cap · corrodedRH WING, AFT TOP WING SPAR HAS CORROSION AROUND FASTENER HOLE AT LOCATION APPROX STA XORS 903.0 REPAIRED PER E.A. 1-5710-T0351527 P1SDR FDEA2020021490320Spar Cap · corrodedRH WING, AFT TOP WING SPAR HAS CORROSION AROUND FASTENER HOLE AT LOCATION APPROX XORS 846.3 REMOVED CORROSION PER SRM 51-21-01-0G. REF EA T 1-5710-T0351527 P1 "BASIC WING STRUCTURE - RH WING REAR SPAR UPPER CAP AFT LEG - REWORK." REWORKED AREA ACCEPTABLSDR FDEA2020021490319Spar Cap · corrodedRH WING, AFT TOP WING SPAR HAS CORROSION AROUND FASTENER HOLE AT LOCATION APPROX STA XORS 983.5 THRU 989.0 REMOVED CORROSION PER SRM 51-21-01-0G. REF EA T 1-5710-T0351527 P1 "BASIC WING STRUCTURE - RH WING REAR SPAR UPPER CAP AFT LEG - REWORK." REWORKED ASDR FDEA2020013090247Spar · corrodedRH WING, AFT TOP WING SPAR HAS CORROSION AROUND FASTENER HOLE AT LOCATION APPROX STA XORS 1037.0 THRU XORS 1044.8 WORKED ACCOMPLISHED ON N/R 1206 AND 507 PER EA. 1-5710-T0351904SDR FDEA2020021090315Spar Cap · corrodedRH WING, AFT TOP WING SPAR HAS CORROSION AROUND FASTENER HOLE AT LOCATION APPROX STA XORS 992.5 THRU XORS 1001.5 REPAIRED PER EA T 1-5710-T0351527SDR FDEA2020021480327Spar Cap · corrodedRH WING UPPER REAR SPAR, STATION XORS 785 HAS SURFACE CORROSION. REPAIRED WITH STRAP/ANGLE PER EA T 1-5710-T0352042SDR FDEA201911180325Spar Cap · corrodedRH WING UPPER REAR SPAR, STATION XORS 789 HAS SURFACE CORROSION. PERFORMED STRAP ANGLE REPAIR PER EA T 1-5710-T0352042SDR FDEA201901300240Bracket · worn#1 ENGINE: RIGHT SIDE OF PYLON INSIDE ACCESS PANEL 438DR, PNEUMATIC DUCT SUPPORT. LOWER BRACKET HAS LOOSE ATTACH SCREWS/ELONGATED HOLES BRACKET REPAIR COMPLIED WITH I.A.W. E.A. 1-5450-T0351554 PT, REF JPF STEP ITEM 12. TITLE: NACELLES/PYLON - WING PYLON/STSDR FDEA2020021050301Spar Cap · corrodedRH WING UPPER, REAR SPAR CORROSION AT WING STATION XORS 684. REPAIRED PER EA T 1-5710-T0351924 P1SDR FDEA2019111542954Seat Track · corrodedMAIN DECK, CORROSION ON SEAT TRACK, APPROX. STA 1159 LBL 9. (MARKED) REMOVED & REPLACED SECTION OF SEAT TRACK BETWEEN STATIONS 1149 TO STATION 1189 IN REF TO DWG # SR10-53-002 AND SRM 53-00-52 REPAIR # 1, FIG 201SDR FDEA201901130109Skin · corrodedR/H AFT FUSELAGE BELOW HORZ. STAB CUT-OUT, NUMEROUS SURFACE CORROSIONS AROUND FASTENER HOLES FOR PNL 348BF AND 347DF REPAIRED AFT FUSELAGE SURFACE AT HORIZONTAL TAB CUTOUT IAW SRM 53-70-01-00 REPAIR #3 FIG 201 PG 202 AND JPF ITEMS.SDR FDEA2019122633297Skin · corrodedRT AFT FUSELAGE BELOW APU COMP COOLING AIR OUTLET, EXFOLIATION CORROSION AROUND FASTENER HOLE FOR PNL 347DF. REPAIRED AREA BELOW APU COMP COOLING AIR OUTLET REF SRM 53-70-01 FIG 201 SH 1 MAJOR REPAIR.SDR FDEA202001030006Support Bracket · worn#1 PYLON UPR PNL SUPPORT BRACKET BETWEEN PNLS 437CL AND 437DL WORN FROM PNL CHAFING. REPLACED BRACKET PER DWG AUB7564-29 AND SRM 51-31-01-0G.SDR FDEA2020011640128Floorbeam · corrodedMAIN CARGO DECK, STA1346 RBL105 CORROSION (MARKED) WORKED ACOMPLISHED ON N/R 664 AND 884 PER EA. 1-5710-T0351898SDR FDEA2019121313243Doubler · wornRT WING: DROOP L/E, INBD EDGE OF DROOP L/E REPAIR DOUBLER SKIN HAS WEAR MARK WORN INTO SKIN (MARKED AND DOT 36) REPAIRED PER SRM 57-40-01 2RSDR FDEA2020010600030Skin · chafedRT WING: OUTBD EDGE OF DROOP L/E REPAIR DOUBLER SKIN IS WORN THRU. INSTALLED REPAIR PER SRM 57-40-01-2R INSTALLED DROOP L.E IAW MM 27-80-10-4 OPS CK GOODSDR FDEA2020012493340Frame · wornFWD AVIONICS COMPT: APPROX STA 457, THE FRAME UNDER #1 PACK INLET DUCT. THE DUCT BOOT MOUNT FASTENERS HAVE WORN THRU THE UPPER PART OF THE FRAME. (UNDER THE DUCT BOOT). MARKED. REPAIR IS COMPLIED WITH E.A.#:1-5300-T0351624 PART 1, TITLE: MD-11 N574FE-FUSELSDR FDEA201911092915Doubler · corrodedRH WING UPPER SURFACE - XORS 248 LANDING GEAR DOUBLER - CORROSION AROUND THREE (3) FASTENERS. REPAIRED PER EA 1-5710-T0351593SDR FDEA2020021480317Angle · corrodedMAIN CARGO DECK, STA1341 RBL104 CORROSION ON ANGLE AT BASE OF OVERWING FUEL TANK (MARKED) WORK ACOMPLISHED ON N/R 664 AND 884 PER EA. 1-5710-T0351898 A P1SDR FDEA2019110980063Bracket · corrodedMAIN CARGO DECK, STA1321 RBL48 UNDER SEAT TRACK, CORROSION BY FASTENER (MARKED) REMOVED AND REPLACED BRACKET PER APB7244SDR FDEA201911268087Floorbeam · crackedCENTER CARGO COMPT: APPROX STA 1741 , CENTERLINE CARGO STOP. UNDER THE CARGO STOP THE FLOOR BEAM IS CRACKED.(UNDERSIDE OF STOP) REMOVED DAMAGED FLOOR BEAM IN CTR CARGO AT STA 1741. INSTALLED NEW FLOOR BEAM SECTION AND REPAIR PARTS PER SRM 51-31-01-0G.SDR FDEA202001170152Cargo Track · crackedCENTER CARGO COMPT: APPROX STA 1721, X=-91.25. O/B CARGO RAIL HAS AN O/B FLOOR BOARD FASTNENER ATTACH EAR CRACKED TWO PLACES. MARKED. PROCESSED NEW CHANNEL PER DWG AJF7011-519, REMOVED AND INSTALLED NEW CHANNEL IN CTR CARGO AT STA 1721, X=-47.25 PER SRM 51SDR FDEA2019122073267Skin · crackedLT LWR VERTICAL STAB FAIRING SKIN AT STA 2160 HAS A .300 IN CRACK PROPAGATING OUT OF THE FASTENER HOLE. BELOW PYLON CARRY THROUGH CAP, REPAIRED SKIN FAIRING PER SRM 55-00-00-2R FIG 204 DWG AJC7582-17.SDR FDEA2020022060356Spar · corrodedPERFORMED DETAIL VISUAL INSP. OF THE OUTER WING, UPPER SPAR CAP (P/N ARB7413-2) FROM STATIONS XORS-1041.500 THROUGH XORS-1044.000 PER FOLLOW UP E.A. 1-5720-87643 AND W/C SEQ. #000806, W/C #T-1-5720-87643 P2. FOUND CORROSION BETWEEN AREAS X0RS- 1035.500 TSDR FDEA201912263303Spar · corrodedRIGHT WING T/E REAR SPAR UPPER CAP, LOWER FLANGE IS CORRODED AT STA. XORS 685. BLENDED AND REMOVED CORROSION IAW SRM 57-00-00-2R REFERENCE EA 1-5710-T0350918P1REMOVED FASTENERS THROUGH UPPER SPAR T-CAP LOWER FLANGE FROM XORS 680-690 IAW SRM 51-33-01-0G. RESDR FDEA201911063188Skin · chafedRT WING LWR FIXED L/E SKIN WORN FROM SLAT CONTACT. O/B OF SLAT TRACK NR 10 PERFORMED WING FIXED LEADING EGDE REPAIR IAW SRM 57-40-02-2R FIG 201 REP 5.SDR FDEA2019110762900Skin · corrodedRH WING UPPER SURFACE - APPROX XORS 288 AFT SECTION OF LANDING GEAR DOUBLER - CORROSION AROUND FASTENER.SDR FDEA2019112243036Skin · corrodedNUMEROUS AREAS OF SURFACE CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS-340.00 TO XORS-393.00 / STR-5.5 TO STR. 2...(MRK) REMOVED CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS=345.75 TO XORS=298.501 STR 07 TO AFT SPAR REF EA#: 1-5730-T03515SDR FDEA2019112243034Skin · corrodedNUMEROUS AREAS OF SURFACE CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS-141.00 TO XORS-166.80 STR.22 TO STR-19....(MRK) REMOVED CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS=130.40 TO XORS=163.80 FRONT SPAR TO STR 16 REF SRM 57-00-01-1A SDR FDEA2019112243029Skin · corrodedNUMEROUS AREAS OF SURFACE CORROSION ON L/H WING UPPER SURFACE XORS-93.00 TO XORS-96.00 STR.17.5 TO STRINGER-19.5...(MRK) REMOVED CORROSION ON L/H WING UPPER SURGACE REF SRM 57-00-01-1A & E.A. #: 1-5730- T0351592 "TITLE: WING - PLATES AND SKINS - LH OUTERSDR FDEA2020012140137Longeron · corrodedAFT CARGO COMPT:CORROSION AT R/H STA 1957 LONGERON 43R DOT NO 4. REMOVED AND REPLACED 48" LONG SECTION OF LONGERON 43 R/H FROM STSA 1948 TO 1997 IAW SRM 53-00-05-2R FIG 201, 202 SHEET 1-3, PG 1-8 DAC DWGS AGA7073, NGA6313.SDR FDEA2019120643181Stiffener · corrodedAFT CARGO TUNNEL:EXFOLIATION AT R/H STA 1960 STRINGER 40 DOT NO 3. REMOVED CORRODED SECTION OF LONGERON AS REQUIRED IAW SRM 53-00-05-2R FIG 202 REPAIR 1 PG 1-8.SDR FDEA2019112243028Skin · corrodedNUMEROUS AREAS 0F SURFACE CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS-166.80 TO XORS-201.00/FRONT STR-14 TO STR-19.5....(MRK) REWORKED CORROSION MD-11 SRM 57-00-01-1A SHEET 6SDR FDEA2019112243027Tee Fitting · corrodedAFT CARGO WASTE COMPT:EXFOLIATION AT R/H APX STA 1960 BETWEEN STRINGER 50-51 DOT NO 6. REMOVED AND REPLACED TEE CLIP P/N AGA8002-19 AT STA 1975 BETWEEN R/H L49 AND L/H49 REF SRM 51-35-01, SRM 51-33-01 AND DOUGLAS AGA8002.SDR FDEA2019111932989Web · crackedR/H NLG WHEEL WELL WEB AT STA. 495 HAS A .200 IN. CRACK AT FASTENER HOLE ABOVE HORIZONTAL STIFFENER. (MARKED) REPAIRED RH NLG WHEEL WELL WEB AT STA 495 REF SRM 53-10-13 FIG 201 SH. 8SDR FDEA201911152938Web · crackedL/H NLG WHEEL WELL WEB AT STA. 495 HAS A .200 IN. CRACK AT FASTENER HOLE ABOVE HORIZONTAL STIFFENER. (MARKED) REPAIRED LH NLG WHEEL WELL WEB @ STA 495 REF SRM 53-10-13 FIG 201 SH. 8 'MAJOR REPAIR' JPFSDR FDEA201911152937Skin · crackedL/H LWR WING SKIN AT #16 SLAT TRACK CUT OUT AFT I/B CORNER HAS A .400 IN. CRACK. (MARKED) REPAIR NOTED SKIN CRACK AT SLAT #16 PER SRM 57-40-02-2R REPAIR 7 FIG 201SDR FDEA201911152936Skin · crackedL/H LWR WING SKIN AT #12 SLAT TRACK CUT OUT AFT O/B CORNER HAS A .300 IN. CRACK. (MARKED) REPAIRED NOTED SKIN CRACK AT SLAT TRACK #12 PER SRM 57-40-02-2R REPAIR 7 FIG 201.SDR FDEA2020040862900Doubler · corrodedRH WING UPPER SURFACE - APPROX XORS 288 AFT SECTION OF LANDING GEAR DOUBLER - CORROSION AROUND FASTENER. REPAIRED PER EA 1-5730-T0350758SDR FDEA2020011600131Web · crackedR/H NLG TRUNNION FITTING WEB AT STA. 590 HAS A .900 IN. CRACK. (MARKED) REPAIRED AS REQUIRED R/H NLG TRUNNION FITTING WEB AT STA 590, PER MD-11 SRM 53-10- 14-2R, FIGURE 202, REPAIR 2, PG 8-10.SDR FDEA201903200687Oil System · leakingFLT LVL 360 STARTED NOTICING THE NR 2 OIL QTY DECREASE. AFTER REFERENCING QRH, CAPTAIN DECIDED TO SHUTDOWN THE NR 2 ENGINE. NO ABNORMAL INDICATION ON OIL PRESS OR OIL TEMP. NO OTHER ISSUES AFTER SHUTDOWN. LOWEST QTY SEEN WAS 3. AFTER INSTALLATION OF NR 2 SDR FDEA201902150423Sensor · failedPASSING THROUGH 2000' DEPARTING ZSPD WITH LANDING GEAR RETRACTED, LEVEL 2 " BRAKE OVERHEAT" ILLUMINATED.COMPLIED WITH QRH AND EXTENDED LANDING GEAR. OVERHEATED BRAKE WAS ON #7 WHEEL W/MAX TEMPERATURE OBSERVED OF 568 DEG WHILE ALL OTHER BRAKES WERE
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