N582FE
Service difficulty reports · 370
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 = 'N582FE' 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 = 'N582FE' 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 FDEA2020073091705Frame · dentedCABIN - MAIN DECK CARGO COMPARTMENT FRAME DENTED AT STATION 1621 , LONGERON 12 RIGHTSDR FDEA202006231316Fan · failedON DESCENT INTO KOAK PASSING THROUGH APPROX FL280 STARTED SMELLING AN ACRID SMELL ACCOMPANIED BY A RUMBLING SOUND. THE FO SAID HE FELT VIBRATIONS UNDER HIS FEET. THE SMELL INCREASED, SO WE DECLARED AN EMERGENCY. AS WE GOT BELOW 10,000FT AND THE PLANE DEPRESDR FDEA201904020753Warning Message · false activationEMERGENCY LIGHT BAT 1 LO ALERT DURING PRE-FLIGHT. T/S PER MD11 FIM 33-52-00-01. ALL TESTS PASS. NO HISTORY FOR OVER 30 DAYS. PERFORMED ADJ/TEST PER MD11 AMM 33-50-00-5. OPS CK GOOD.SDR FDEA201807201791Doubler · corrodedLT WING FOUND UNDERWING LOWER FRONT SPAR DOUBLER AT STA XOS 1198.587 JUST AFT OF NR 8 SLAT CAVITY, WITH CORROSION AS MARKED. LT WING LOWER FRONT SPAR DOUBLER AT STA XOS 1198.587 AFT OF NR 8 SLAT CAVITY CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAISDR FDEA201807121675Skin · cracked1 EA FASTENER HOLE NR 9 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 9 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR SDR FDEA201807121674Skin · cracked1 EA FASTENER HOLE NR 15 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 15 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAISDR FDEA201807121673Skin · cracked1 EA FASTENER HOLE NR 32 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 32 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAISDR FDEA201807121672Skin · cracked1 EA FASTENER HOLE NR 36 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 36 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAISDR FDEA201807121671Skin · cracked1 EA FASTENER HOLE NR 6 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT LEFT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 6 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIR SDR FDEA201807121670Skin · cracked1 EA FASTENER HOLE NR 7 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 7 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPAIRSDR FDEA201807121669Skin · cracked1 EA FASTENER HOLE NR 27 FOUND CRACK INDICATION DURING OPEN-HOLE HFEC INSPECTION AT RIGHT HAND WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND XORS 700. CRACKED FASTENER HOLE NR 27 CARRIED OUT REPAIR AS PER SRM 57-20-02-2R FIGURE 201 REPAIR 5. REPASDR FDEA201807121668Seat Track · damagedCABIN LT STA 1521, X=8.5 SEAT TRACK CROWN FOUND DAMAGED. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-83 TO STA 5-123, X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807121667Seat Track · damagedCABIN, RT STA 1541 - 1562, X=-8.5 SEAT TRACK CROWN FOUND DAMAGED. DAMAGED SEAT TRACK CROWN REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1531 TO STA 1591, X= -8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807091656Skin · crackedLT WING FOUND SLAT TRACK NR 14 CUTOUT CORNER CRACKED, STA XOS 881 LT WING SLAT TRACK NR 14 CUTOUT CORNER, STA XOS 881 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807091655Skin · crackedRT WING FOUND SLAT TRACK NR 14 CUTOUT CORNER CRACKED, STA XOS 889 RT WING SLAT TRACK NR 14 CUTOUT CORNER, STA XOS 889 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807091654Skin · crackedRT WING FOUND SLAT TRACK NR 12 CUTOUT CORNER CRACKED, STA XOS 774 RT WING SLAT TRACK NR 12 CUTOUT CORNER, STA XOS 774 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807091653Skin · corrodedAFT ACCESSORY COMPARTMENT RT FUSELAGE SKIN AT STA 2163.685 LONGERON 33R-35R, FOUND CORROSION. CARRIED OUT REPAIR AS PER SRM 53-70-01-2R FIGURE 201 REPAIR 3. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. RT FUSELAGE SKIN AT STA 2163.685 LONGERON 33R - LONGERON 35SDR FDEA201807061641Doubler · crackedLT WING FOUND LEADING EDGE CAVITY WITH BEADED DOUBLER CRACKED AS MARKED AT STA XOS 626. LT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 626 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807061640Doubler · crackedLT WING FOUND LEADING EDGE CAVITY WITH BEADED DOUBLER CRACKED AS MARKED AT STA XOS 695. LT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 695 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807061639Doubler · crackedLT WING FOUND LEADING EDGE CAVITY BEADED DOUBLER CRACKED AT STA XOS 585. LT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 585 CARRIED OUT REPAIR AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201807061638Seat Track · corrodedCABIN LT STA 1121, X=8.5 SEAT TRACK FOUND CORROSION. CORROSION FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. DAMAGED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1089 TO STA 6-0, X=8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPSDR FDEA201709052458Cable · brokenL1 DOOR MAIN AFT DRIVE CABLE BROKEN. REF IPC 52-11-05-01, ITEM 312 IS UPPER CABLE THAT IS BROKEN. REMOVED AND REPLACED AFT UPPER L1 DOOR DRIVE CABLE REF AMM 52-11-03-4 UP TO AND INCLUDING STEP E(7).SDR FDEA201706201710Light · malfunctionedEMERGENCY LIGHT TEST DID NOT PASS. CARRIED OUT ADJUSTMENT TEST ON EMERGENCY LIGHTS IAW AMM 33-50-00-5. CHECKED GOOD.SDR FDEA201705181453Warning Light · false activationDURING A PREFLIGHT, RECEIVED AN ALERT FOR THE EMERGENCY LIGHT BATTERY 1 LOW. COMPLIED WITH FIM 33-51-02-00 EMERGENCY LIGHTS BATTERY POWER SUPPLY TEST. NO FAULTS NOTED, ACFT OK FOR SERVICE. NO HISTORY IN PAST 90 DAYS.SDR FDEA201705171451Girt Bar · unsecureL1 DOOR GIRT BAR IS LOOSE AND HANGING DOWN. REINSTALLED THE GIRT BAR IAW AMM 25-61-01-4.SDR FDEA201705061366Hinge · wornMDC DOOR FWD HINGE HAS PLAY. HINGE SECTION REPLACED.SDR FDEA201612134421Light · inoperativeDOOR DISARMED ANNUNCIATOR AT L1 DOOR INOP RELAMPED, OPS CHECKS GOOD.SDR FDEA201611284283Feeder Cable · damagedNR 2 ENGINE GENERATOR FEEDER CABLE BY THE ENGINE ANTI-ICE VALVES ARE DAMAGED.SDR FDEA201607192527Feeder Cable · damagedAFT FUSELAGE COMPARTMENT AT BS 2033, DURING DEFECT RECTIFICATION, FOUND ONE FEEDER CABLE FOR ENGINE NR 2 WITH DEEP CUT AND ON EWIRING CLAMP WITH SIGN OF ARCING.SDR FDEA201607152453Spar · crackedAFTER PANEL 364RR, EMPENNAGE, INSIDE PANEL 364RR AFT SPAR WEB FOUND CRACK AT STA Y = 2164.SDR FDEA201607132433Hinge · corrodedRIGHT WING, INBD FLAP OTBD FWD HINGE, WING SIDE, PIVOT BORE FOUND, CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-07. EXISTING HOLE DIA: 2.531", FINAL HOLE DIA: 2.536" AND MAXIMUM ALLOWABLE HOLE DIA: 2.531". NEW REPAIR BUSHING FABRICATED AND INSSDR FDEA201607132432Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.289", FINAL HOLE DIA: 1.328" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED ANSDR FDEA201607132431Hinge · corrodedRIGHT WING, INBD FLAP OTBD AFT HINGE, FLAP SIDE, PIVOT INBD BORE FOUND CORROSION. CORROSION REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.290", FINAL HOLE DIA: 1.328" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRSDR FDEA201607132430Hinge · corrodedRIGHT WING, OTBD FLAP, INBD FWD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.221", FINAL HOLE DIA: 1.225", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATEDSDR FDEA201607132429Hinge · corrodedRIGHT WING, OTBD FLAP INBD FWD HINGE, WING SIDE, ACTUATOR ATTACH INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.221", FINAL HOLE DIA: 1.225", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED ASDR FDEA201607132428Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT INBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.880", FINAL HOLE: DIA 0.953", MAXIMUM ALLOWABLE HOLE: DIA 0.944". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA 1-5SDR FDEA201607132427Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND EXCEED LIMIT CMM 57-44-09. EXISTING HOLE: DIA 0.880". FINAL HOLE: DIA 0.953". MAXIMUM ALLOWABLE HOLE: DIA 0.944", REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-575SDR FDEA201607132426Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE UPPER MOUNT, INBD BORE SURFACE AREA CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.715", MATERIAL REMOVED: 0.003", REMAINING THICK: 0.712". MINIMUM ALLOWABLE THICKNESS: 0.720". REPASDR FDEA201607132425Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, UPPER MOUNT OTBD BORE SURFACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.709", MATERIAL REMOVED: 0.003", REMAINING THICKNESS: 0.706". MINIMUM ALLOWABLE THICKNESS:SDR FDEA201607132424Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE LOWER MOUNT INBD CORRODED. REWORKED AND FOUND, EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.521", FINAL HOLE: DIA 0.613", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATED AND INSTALLED IAW EA NR 1-5750SDR FDEA201607132423Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE LOWER MOUNT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 0.581", FINAL HOLE: DIA 0.613", MAXIMUM ALLOWABLE HOLE: DIA 0.584". REPAIR BUSHING FABRICATED AND SDR FDEA201607132422Hinge · corrodedRT WING, OTBD FLAP, OTBD FORWARD HINGE LOWER MOUNT INBD BORE SURFACE AREA CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.414", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.406", MINIMUM ALLOWABLE, THICKNESS: 0.408", RSDR FDEA201607132421Hinge · corrodedRT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, LOWER MOUNT OTBD BORE SURFACE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING THICKNESS: 0.387", MATERIAL REMOVED: 0.008", REMAINING THICKNESS: 0.379", MINIMUM ALLOWABLE THICKNESS: SDR FDEA201607132420Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.380", FINAL HOLE DIA: 0.407", MAXIMUM ALLOWABLE HOLE DIA: 0.391". REPAIR BUSHING FABRICATED SDR FDEA201607132419Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE FOUND CORROSION. CORROSION AT RT WING, OTBD FLAP, OTBD FORWARD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE, NR 7 HOLE, REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOSDR FDEA201607132418Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.662", FINAL HOLE DIA: 0.699", MAXIMUM ALLOWABLE HOLE DIA: 0.667". REPAIR BUSHING FABRICATED AND INSTALLSDR FDEA201607132417Hinge · corrodedRIGHT WING, OTBD FLAP, OTBD HINGE, WING SIDE, INBD ACTUATOR ATTACH BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALSDR FDEA201607132416Hinge · corrodedRT WING, OTBD FLAP, OTBD HINGE, WING SIDE, OTBD ACTUATOR ATTACH BORE, CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-44-09. EXISTING HOLE: DIA 1.220", FINAL HOLE: DIA 1.224", MAXIMUM ALLOWABLE HOLE: DIA 1.220". REPAIR BUSHING FABRICATED AND INSTALLSDR FDEA201607132415Hinge · corrodedLT WING, INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.188", FINAL HOLE DIA: 1.235" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND ISDR FDEA201607132413Hinge · corrodedLEFT WING, INBD FLAP, OTBD AFT HINGE, FLAP SIDE, PIVOT INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-52-03. EXISTING HOLE DIA: 1.188", FINAL HOLE DIA: 1.235" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRICATED AND
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