N601FE
Service difficulty reports · 546
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 = 'N601FE' 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 = 'N601FE' 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 FDEA2019101422613Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) PIVOT INBOARD HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-04. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-04, AND EA 1-5750-76649 A, PART 2, STSDR FDEA2019101422610Hinge Fitting · corrodedRIGHT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159802 G, PART 3,SDR FDEA2019101422609Hinge Fitting · corrodedRIGHT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159802 G, PART 3, SDR FDEA2019101422608Hinge Fitting · corrodedLEFT WING INBOARD FLAP, OUTBOARD AFTER HINGE (FLAP SIDE) OUTBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159801 H, PART 3, SSDR FDEA2019101422607Hinge Fitting · corrodedLEFT WING, INBOARD FLAP OUTBOARD AFTER HINGE (FLAP SIDE) INBOARD PIVOT HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-52-03, AND EA 1-5750-159801 H, PART 3, SDR FDEA201910112596Longeron · crackedLOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 43 RIGHT FOUND CRACK AT STATION 1821. REMOVED AND INSTALLED FABRICATED LONGERON FITTING AS PER SRM 51-31-01-OG. LONGERON FITTING FABRICATED AS PER DOUGLAS DRAWING AGA 7369 REVISION H. REPAIR CLASSIFIED SDR FDEA201910112595Floorbeam · corrodedLOWER CENTER CARGO COMPARTMENT FLOOR BEAM FOUND WITH CORROSION AT STA 1701 X = -34. REPAIR CARRIED OUT AS PER SRM 53-50-51-2R FIGURE 201 REPAIR 1 AND EA # 1-5310- T0350373 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. LOWER CENTER CARGO COMPARTMENSDR FDEA201910112594Longeron · corrodedLOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 44 RIGHT FOUND CORROSION AT STATION 1661 TO 1681. CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 205. LONGERON 44 RIGHT CORROSION AREA CARRIED OUT REPAIR AS SDR FDEA201910112593Longeron · corrodedLOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 47 RIGHT FOUND CORROSION AT STATION 1731. CORROSION REMOVED AS PER SRM 51-21-01-OG AND FOUND EXCEEDED LIMIT AS PER SRM 53- 00-00-2R, FIG 205. LONGERON 47 RIGHT AT STATION 1731 CARRIED OUT REPAIR AS PER SRMSDR FDEA201910112597Bulkhead Web · crackedLOWER AFT CARGO COMPARTMENT BILGE AREA FORWARD BULKHEAD FOUND WEB SKIN PUNCTURED AT STA 1841 X = 17. REMOVED AS PER SRM 51-31-01-0G. NEW WEB FABRICATED AS PER DOUGLAS DRAWING AGA7170 REV R AND INSTALLED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PSDR FDEA201910112598Longeron Splice · crackedLOWER CENTER CARGO COMPARTMENT BILGE AREA LONGERON 51 RIGHT SPLICE FITTING CRACK AT BETWEEN STATION 5-113 TO 1541. LONGERON SPLICE REMOVED AND INSTALLED A FABRICATED SPLICE IAW SRM 51-33-01-OG. SPLICE FITTING FABRICATED AS PER DOUGLAS DRAWING A5A7114 REVISDR FDEA201910102569Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK CORROSION AT BS 675, RBL 100. THE CORROSION WAS REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101 ALLOWABLE DAMAGE 1. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R, REPAIR 5, FIGURE 201, AND EA 1-5310-T0SDR FDEA201910102582Hinge Bracket · corrodedRIGHT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0SDR FDEA201910102581Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), INBOARD ACTUATOR HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T035SDR FDEA201910102580Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350048, PART 1, SDR FDEA201910102579Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) OUTBOARD ACTUATOR HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350044, SDR FDEA201910102578Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350044, PART 1, SSDR FDEA201910102577Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER BARREL NUT HOLE BORE CORRODED. THE NR 7 NUT HOLE BORE WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-57SDR FDEA201910102576Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) UPPER BARREL NUT HOLE BORE CORRODED. NUT HOLE NR 7 BORE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T03500SDR FDEA201910102575Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT, OUTBOARD HOLE SURFACE CORRODED. OUTBOARD HOLE SURFACE REWORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5SDR FDEA201910102574Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT, OUTBOARD NR 3 HOLE BORE CORRODED. THE HOLE BORE WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-57SDR FDEA201910102573Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE CORRODED. HOLE NR 3 BORE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T035004SDR FDEA201910102572Hinge Bracket · corrodedRIGHT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE (WING SIDE) PIVOT HOLE BORE CORRODED. HOLE 4 BORE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44- 09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44- 09, AND EA 1-5750-T0350044, PART 1, SSDR FDEA201910102566Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE, WING SIDE, LOWER MOUNT OUTBOARD HOLE SURFACE WAS CORRODED. HOLE SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350SDR FDEA201910102565Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP, INBOARD FORWARD HINGE, WING SIDE LOWER MOUNT INBOARD HOLE SURFACE CORRODED. HOLE SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113SDR FDEA201910102564Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE PIVOT HOLE BORE FOUND CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08 AND EA 1-5750-T0350113, PART 1, STEP 1A, AND STEP 1. THSDR FDEA201910102562Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE WAS CORRODED. THE CORROSION WAS REWORKED, AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-575SDR FDEA201910102560Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), INBOARD ACTUATOR HOLE BORE FOUND CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0350113, PART 1, SDR FDEA201910102559Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE), OUTBOARD FWD MOUNT HOLE BORE FOUND CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-57SDR FDEA201910102556Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP, INBOARD FORWARD HINGE (WING SIDE), INBOARD FWD MOUNT BORE WAS CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-08, AND EA 1-5750-T0SDR FDEA201910102555Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), UPPER MOUNT, OUTBOARD HOLE BORE CORRODED. THE CORROSION WAS REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-TSDR FDEA201910102554Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT OUTBOARD HOLE SURFACE CORRODED. SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1,SDR FDEA201910102553Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT INBOARD HOLE SURFACE CORRODED. SURFACE REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, SDR FDEA201910102552Hinge Bracket · corrodedLEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER MOUNT OUTBOARD HOLE BORE CORRODED. CORROSION REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, SDR FDEA201910102551Hinge Bracket · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. SHOULDER BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1.SDR FDEA201910102550Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT HOLE BORE WAS CORRODED. THE CORROSION WAS WORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED, AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T035001SDR FDEA201910102549Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), LOWER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1SDR FDEA201910102548Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), UPPER BARREL NUT HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP SDR FDEA201910102547Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE), OUTBOARD ACTUATOR HOLE BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED, AND INSTALLED IAW CMM 57-44-09 AND EA 1-5750-T0350013 PART 1 STEP 1 . REPAIR SDR FDEA201910102546Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) INBOARD ACTUATOR HOLE BORE CORRODED. REWORKED AND FOUND TO EXCEED LIMITS IAW CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED IAW CMM 57-44-09, AND EA 1-5750-T0350013, PART 1, STEP 1. THE RSDR FDEA201910102563Doubler · crackedRIGHT WING BEADED DOUBLER AT STA XOS 564 WAS FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201910102558Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 643 WAS FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201910102571Seat Track · crackedMAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK WAS FOUND CRACKED BETWEEN BS 1581 - 1641, RBL 8.5. THE SEAT TRACK WAS REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICE BS 1571 TO 1651 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. THE REPAIR WAS CLASSIFIED IAW SDR FDEA201910102570Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK FLANGE CORRODED BS 5-91, RBL 8.5. THE CORROSION WAS REMOVED AND FOUND TO EXCEED LIMITS IAW SRM 53-00-52-1A, FIGURE 101. THE SEAT TRACK WAS REPAIRED BY SECTIONAL AT EXISTING SPLICES BS 5-63 TO BS 1531, IAW SRM 53-00-52-SDR FDEA201910102568Doubler · crackedLEFT WING BEADED DOUBLER AT XOS 692 FOUND CRACKED. THE DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201910102567Doubler · crackedLEFT WING BEADED DOUBLER AT STA XOS 763 WAS FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201910102561Doubler · crackedLEFT WING BEADED DOUBLER AT STA XOS 795 FOUND CRACKED. THE BEADED DOUBLER WAS REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA2019062081392Scuff Plate · damagedSCUFF PLATE DAMAGED OF THE LOWER FWD CARGO DOOR REPAIRED DAMAGE IN ACCORDANCE WITH EA 1-5330-T0347600 A, PS P2.SDR FDEA2019060651224Duct · damaged#3 MANIFOLD FAILURE. SHGN 08JUN19 09:03 KIX INSTALLED NEW DUCT PER AMM 36-14-02-4 AND NO LEAK NOTED. ALSO #3 PNEUMATIC SYSTEM DECAY CHECK W/APU AIR SATISFACTORY PER MD11 JRH. MDC FLOOR BOARD AND SIDEWALL PANEL IN FWD CARGO COMPARTMENT BEING INSTALLED PESDR FDEA201905181095Cable · shortedPDIS 601 26-10 0334 17MAY19 MEM OPEN U LOGPAGES:2723226 LVL 3 ENG 2 FIRE LIGHT PASSING FL 290. NR 2 ENG. FIRE LOOP "A" DEFERRED. COMPLIED W/ QRH FOUND RIGID CABLE BETWEEN DH7 AND DH8 SHORTED, ALSO FOUND UPP TUR RIGHT A AND B RAIL ASSEMBLY BROKE
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