N604FE
Service difficulty reports · 447
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 = 'N604FE' 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 = 'N604FE' 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 FDEA201303220648Access Panel · crackedRIGHT WING L/E LOWER ACCESS PANEL 619CB CUTOUT FORWARD INBD CORNER FOUND CRACKED AT XOS 612. REPAIRED IAW SRM 57-40-02 FIGURE 202 REPAIR 7 REVISION 52. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.SDR FDEA201303220647Doubler · crackedRIGHT WING L/E COMPARTMENT BEADED DOUBLER AT XOS 666 FOUND CRACKED. REPAIRED IAW SRM 57-40-40-02 REPAIR 15 FIGURE 203 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201303220646Doubler · crackedRT WING L/E COMPARTMENT BEADED DOUBLER AT XOS 870 FOUND CRACKED. REPAIRED IAW SRM 57-40-02 REPAIR 15 FIGURE 203 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201303220645Longeron Splice · crackedLOWER CENTER CARGO COMPARTMENT, LONGERON SPLICE AT BS 5-123, LONGERON 43 RT FOUND CRACKED. LONGERON SPLICE REMOVED IAW SRM 51-33-01 REVISION 52. FABRICATED IAW DRAWING A5A7114 REVISION J. REPAIR CLASSIFED AS MAJOR AS PER GMM 6-2-100 REVISION 116.SDR FDEA201303220644Intake · crackedNR 2 ENGINE INTAKE DUCT RT ON PANEL NR 364RR STATION 2140, REAR CENTER SPAR TO REAR SPAR LOWER PANEL FOUND CRACKED. REPAIRED AS PER SRM 55-30-02 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.SDR FDEA201303220650Bulkhead Web · crackedLOWER CENTER CARGO COMPARTMENT, SUMP PANEL AREA FOWARD BULKHEAD RT UPPER WEB FOUND CRACKED AT STATION 1701, "X" = -32. REPAIRED IAW EA 1-5310-166105. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.SDR FDEA201303220649Door Frame · crackedLOWER CENTER CARGO DOOR UPPER FRAME CENTER SECTION FOUND CRACKED. REPAIRED IAW EA 1-5310-167407. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201303200617Skin · crackedLEFT WING NR 8 L/E SLAT LOWER SURFACE SKIN FOUND CRACKED AT XOS 1178. REPAIR CARRIED OUT IAW SRM 57-40-01 REPAIR 3 FIGURE 201 REVISION 52 AND E.A. 1-5750-167409. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.SDR FDEA201303200616Wedge · delaminatedLEFT WING - OTBD AILERON T/E WEDGE INBD EDGE FOUND DELAMINATED. REPAIRED IAW EO 1-5100-7-5001 B2 PT 1AND SRM 57-60-80 REPAIR 1 PARA 4A: 1.A REVISION 52. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.SDR FDEA201303180592Wedge · delaminatedRT WING OTBD FLAP T/E WEDGE INBD EDGE FOUND DELAMINATION. REPAIRED IAW EA 1-5750-165912. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 116.SDR FDEA201204131397Control Cable · failedRT MAIN GEAR DOOR WAS DOWN AND OPEN AT BLOCK IN. REPLACED RT MLG DOOR FOLLOW UP CABLE IAW AMM 32-31-00-5. ACFT OK FOR SERVICE.SDR FDEA201110144491Compressor · stalledON CLIMBOUT PASSING FL 260 ENGINE NR 1 COMPRESSOR STALLED, EVM COMP STARTED VIBRATION 4.8 UPD TO 5.0,N1 DROPPED FROM 102.5 TO 96, EGT RISE TO 580. ON ACFT ARRIVAL FIRST INSP FOUND ALL TURBINE BLADES DAMAGED MOCC P/P CONSULTED. REMOVED AND REPLACED NR 1 ENGINSDR FDEA201107152949Skin · cracked3.1875 INCH CRACK EXIST ON THE UPPER SURFACE OF THE INBD FLAP AT APPROX STA 25.875 COMPLIED WITH PT1 OF EA 1-0550-153068 ON 7/22/11 AT AREA FLAP. EA 1-5750-153138. CLEANED UP DAMAGED AREA AS REQUIRED AND FABRICATED DOUBLER. ALODINE, AND PRIMED IAW SRM 57SDR FDEA201104291673Seat Track · corrodedUPON REMOVAL OF FLOOR PANEL FOUND SEAT TRACK AT STATION 1661 TO 1721 X=-75 CORRODED. CORRODED SEAT TRACK AT STATION 1661TO 1721 X=-75 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1651 TO STATION 1751 X=-75 AS PER SRM 53-00-52 FIG 201 REPAIR 1 RESDR FDEA201104281658Stringer Splice · crackedUPON REMOVAL OF STRINGER SPLICE 9L, HFEC FOUND CRACK APPROX 0.1" LENGTH AT CABIN STA 5-0 ON LONGERON 9L FWD SECTION. REPAIRED AS PER SRM 53-00-05 FIG 202 REPAIR 1 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112. REPAIR LONGERON SEGMENTSDR FDEA201104281657Seat Track · corrodedUPON REMOVAL OF FLOOR PANEL FOUND CURVE SEAT TRACK FLANGE CORRODED AT STA 1761 TO STATION 1821 X=-75.25. REPAIRED BY SECTIONAL SEGMENT REPLACEMENT AS PER SRM 53-00-52 FIG 201 REPAIR 1 AND REPAIR 6 REVISION 46. NEW CURVED SEAT TRACK SEGMENT UTILIZED AS PER ESDR FDEA201104281656Seat Track · corrodedUPON REMOVAL OF FLOOR PANEL, FOUND SEAT TRACK CORRODED AT STA 1661-1721, X=-75. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1651 TO STATION 1751 X=-75 AS PER SRM 53-00-52 FIG 201 REPAIR 1 REVISION 46. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-SDR FDEA201104271636Longeron Splice · crackedLONGERON SPLICE AT STATION 6-85, LONGERON 51R FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISION 46. NEW LONGERON SPLICE FABRICATED PER DRAWING AAA7088 REVISION NEW. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.SDR FDEA201104271635Longeron Splice · crackedFUSELAGE - CAC COMPARTMENT LONGERON SPLICE AT STA 6-85, LONGERON 52 FOUND CRACKED. REMOVED AS PER SRM 51-31-01 REVISION 46. NEW LONGERON SPLICE MACHINED FABRICATED AS PER DRAWING AAA7088-1 REVISION NEW. NEW MACAHINED FABRICATED LONGERON SPLICE INSTALLED PER SDR FDEA201104271634Stringer Splice · crackedDURING X-RAY INSP AT STA 5-0, LONG -9L, STRINGER SPLICE FOUND CRACKED, CRACK LENGTH APPROX 0.1 INCH. REMOVED AND REPLACED AS PER SRM 51-33-01 REVISON 46. NEW STRINGER SPLICE FABRICATED BY MACHINING AS PER DRAWING AEA7633 REVISION J. REPAIR CLASSIFIED AS MAJSDR FDEA201104251602Skin · crackedRT WING DROOP LEADING EDGE EXTERNAL SURFACE INBOARD EDGE FOUND CRACKED. RIGHT HAND WING DROOP LEADING EDGE EXTERNAL SURFACE INBOARD SIDE CARRIED OUT REWORKED AS PER EA 1-5740-143564. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 112.SDR FDEA201104251603Skin · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND 08 EACH HOLES WITH CRACK INDICATION AT LT OUTER WING LOWER ACCESS DOOR CUTOUT AT STA XORS 696.730. REPAIR CARRIED OUT AT LEFT WING OUTER WING LOWER ACCESS DOOR CUTOUT AT XORS 696.730 AS PER DRAWING SG11570004 REVISION SDR FDEA201104251604Skin · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND 05 EACH HOLES WITH CRACK INDICATION AT RT OUTER WING LOWER ACCESS DOOR CUT-OUT AT STA XORS 696.730. REPAIR CARRIED OUT PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 112.SDR FDEA201104241601Longeron Splice · crackedSTATION 1529 LONGERON 31R EXTERIOR LONGERON END FITTING CRACKED. CRACKED LONGERON END FITTING (SPLICE) AT FUSELAGE STATION 1529 L319R EXTERIOR AREA REMOVED AS PER SRM 51-31-01 REVISION 46. NEW LONGERON END FITTING (SPLICE) MACHINED FABRICATED AS PER DRAWING SDR FDEA201104241600Longeron · crackedFUSELAGE - STA 1529, LONGERON 30R EXTERIOR LONGERON END FITTING CRACKED. REMOVED AS PER SRM 51-31-01 REVISION 46. NEW LONGERON END FITTING (SPLICE) MACHINED FABRICATED AS PER DOUGLAS DRAWING AEA7644-1 REVISION B. NEW MACHINED FABRICATED LONGERON END FITSDR FDEA201101060019Shoulder Belt · malfunctionedCAPTAINS SHOULDER HARNESS VERY DIFFICULT TO UNLOCK. OPS CHECKED THE CAPTAINS SHOULDER HARNESS WITH CAPTAIN WATCHING AND SHOULDER HARNESS, OPS CHECKED NORMAL. ACFT OK TO CONTINUE.SDR FDEA201005151540Skin · crackedLOWER FUSELAGE - NR 1 AIR CONDITION COMPARTMENT DOOR CUT OUT AFT UPPER CORNER EXTERIOR SKIN FOUND CRACKED. REPAIRED IAW EA1-5330-140315.SDR FDEA200907102581Skin · misrepairedRT WING INBD FLAP AFT OTBD SEGMENT LWR SURFACE FOUND 1EA EXISTING DOUBLER NOT REPAIRED IAW SRM AT XIFH 276. REPAIRED AS PER SRM57-10-00 FIG3 VOL1 REV 40.SDR FDEA200907092553Support Fitting · corrodedLT WING OTBD FLAP VANE NR 3 SUPPORT FITTING FWD FASTENER HOLE FOUND CORRODED. REPAIRED AS PER EA1-5750-132677. (MAJOR REPAIR)SDR FDEA200907092552Tee Fitting · corrodedLTW OTBD FLAP, FLAP VANE NR 4 TEE FITTING FWD HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132678. (MAJOR REPAIR)SDR FDEA200907092551Tee Fitting · corrodedLTW OTBD FLAP, FLAP VANE NR 2 TEE FITTING FWD HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132676. (MAJOR REPAIR)SDR FDEA200907092550Tee Fitting · corrodedRTW OTBD FLAP, FLAP VANE NR 2 TEE FITTING FWD HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132679. (MAJOR REPAIR)SDR FDEA200907072504Skin · misrepairedEXISTING REPAIR AT AFT CARGO FWD LOWER DOOR JAMB AT STA 1921, LONGERON 42-L. REPAIRED AS PER SRM53-50-00 FIG17 VOL1 REV40 (MAJOR REPAIR).SDR FDEA200907072502Skin · misrepairedLT WING EXISTING REPAIR FOUND ON NR 7 SLAT. REPAIRED AS PER EA1-5750-132686. (MAJOR REPAIR)SDR FDEA200907072522Structure · corrodedMAIN DECK CARGO UNDERFLOOR CTR AUX FUEL TANK UPPER SURFACE CORROSION FOUND ALONG STA 1227 AT X=77.00. REPAIR CARRIED OUT AS PER EA 1-5710-132666.SDR FDEA200907072521Fuel Tank · corrodedMAIN DECK CARGO UNDERFLOOR CTR AUX FUEL TANK UPPER SURFACE CORROSION FOUND AT STA 1233 X=46.00. REPAIR CARRIED OUT AS PER EA 1-5710-132666.SDR FDEA200907062500Hinge Bracket · corrodedLT WING OTBD FLAP OTBD HINGE (WINGSIDE) OTBD ACTUATOR HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132671. (MAJOR REPAIR)SDR FDEA200907062487Hinge Bracket · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE) LOWER MOUNT I/B HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132674. (MAJOR REPAIR)SDR FDEA200907062486Hinge Bracket · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE) O/B ACTUATOR HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132674. (MAJOR REPAIR)SDR FDEA200907062485Hinge Bracket · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE) I/B ACTUATOR HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132674. (MAJOR REPAIR)SDR FDEA200907062484Hinge Bracket · corrodedLT WING O/B FLAP I/B HINGE (WING SIDE) PIVOT HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132674. (MAJOR REPAIR)SDR FDEA200907062483Hinge Bracket · corrodedRT WING O/B FLAP O/B HINGE (WING SIDE) I/B ACTUATOR HOLE FOUND CORROSION. REPAIRED AS PER EA1-5750-132671. (MAJOR REPAIR)SDR FDEA200907062482Hinge Bracket · corrodedRT WING O/B FLAP I/B HINGE (WING SIDE) I/B ACTUATOR HOLE FOUND CORROSION. REPAIR AS PER EA1-5750-132673. (MAJOR REPAIR)SDR FDEA200907062481Bushing · looseLHW O/B FLAP O/B HINGE (WING SIDE) I/B ACTUATOR HOLE BUSHING FOUND LOOSE. BUSHING REPLACED AS PER CMM 57-44-09 REV 64.SDR FDEA200907062480Hinge Bracket · corrodedLT WING O/B FLAP O/B HINGE (WING SIDE) UPPER MOUNT I/B HOLE FOUND CORROSION. REPAIR AS PER EA1-5750-132672 (MAJOR REPAIR).SDR FDEA200907052479Longeron · crackedCRACK INDICATION FOUND APPROX. 0.3" IN LENGTH ON THE LONGERON DURING HFEC INSPECTION ON THE RT NOSE LANDING GEAR TRUNNION FITTING AREA. REPLACED AS PER SRM51-31-01 VOL2 REV40 (MAJOR REPAIR)SDR FDEA200907052478Longeron · crackedCRACK INDICATION FOUND APPROX 0.2" IN LENGTH DURING HFEC INSPECTION ON THE LT NOSE LANDING GEAR TRUNNION FITTING LONGERON. REPAIRED AS PER DRAWING ACA3796 REV A (MAJOR REPAIR).SDR FDEA200907052477Seat Track · crackedMAIN DECK STA 635, X= 27.5 SEAT TRACK FOUND CRACKED. REPAIRED AS PER SRM 53-70-00 FIG 1 VOL 1 REV 40 (MAJOR REPAIR).SDR FDEA200906302417Trunnion · crackedNLG SUSPECT CRACKED RT TRUNNION FITTING. REPAIRED AS PER SRM 53-40-00 FIG 23 VOL 1 REV 40 (MAJOR CAT B REPAIR).SDR FDEA200906302416Trunnion · crackedNLG SUSPECT CRACKED ON LT TRUNNION FITTING. REPAIRED AS PER SRM 53-40-00 FIG 23 VOL 1 REV 40 (MAJOR CAT B REPAIR).
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