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 FDEA201607132411Hinge · corrodedLEFT WING, OTBD FLAP, INBD FORWARD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08. EXISTING HOLE DIA: 1.218", FINAL HOLE DIA: 1.224", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRISDR FDEA201607132409Hinge · corrodedLEFT 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: 1.225", FINAL HOLE DIA: 1.231", MAXIMUM ALLOWABLE HOLE DIA: 1.220". REPAIR BUSHING FABRICATED AND SDR FDEA201607132406Hinge · corrodedLT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, PIVOT BORE FOUND, CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 2.311", FINAL HOLE DIA: 2.316" AND MAXIMUM ALLOWABLE HOLE DIA: 2.3135". NEW REPAIR BUSHING FABRICATED AND INSTASDR FDEA201607132403Hinge · corrodedLEFT 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: 0.618", FINAL HOLE DIA: 0.645" AND MAXIMUM ALLOWABLE HOLE DIA: 0.584". NEW REPAIR BUSHING FABRICATSDR FDEA201607132401Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT UPPER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.391", FINAL HOLE DIA: 0.407" AND MAXIMUM ALLOWABLE HOLE DIA: 0.391". NEW REPAIR BUSHING FASDR FDEA201607132399Hinge · corrodedLEFT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, BARREL NUT LOWER BOLT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA, 0.390", FINAL HOLE DIA: 0.407" AND MAXIMUM ALLOWABLE HOLE DIA: 0.391". NEW REPAIR BUSHING FABRSDR FDEA201607132397Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, BARREL NUT HOLE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 0.674", FINAL HOLE DIA: 0.691" AND MAXIMUM ALLOWABLE HOLE DIA: 0.667". NEW REPAIR BUSHING, FABRICATED ANSDR FDEA201607132395Hinge · corrodedLEFT WING, OTBD FLAP OTBD FWD HINGE, WING SIDE, ACTUATOR ATTACH INBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 1.238", FINAL HOLE DIA: 1.244" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRISDR FDEA201607132393Hinge · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE, WING SIDE, ACTUATOR ATTACH OTBD BORE FOUND CORROSION. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09. EXISTING HOLE DIA: 1.247", FINAL HOLE DIA: 1.252" AND MAXIMUM ALLOWABLE HOLE DIA: 1.220". NEW REPAIR BUSHING FABRSDR FDEA201607082331Spar Cap · crackedDURING HFEC INSPECTION, CARRIED OUT ON REAR SPAR CAP LT FORWARD FLANGE UPPER SECTION FOUND CRACKED. CRACK APPROXIMATE 2.0 INCHES IN LENGTH AS MARKED AT STA Y =2164. CRACKED AREA REPAIRED PER EA NR 1-5530-T0326617 PT 1 TITLE: AD 98-25-15 - STABILIZERS - VERTISDR FDEA201607082330Spar Cap · crackedDURING HFEC INSPECTION CARRIED OUT ON REAR SPAR CAP RT FORWARD FLANGE UPPER SECTION CRACKED. APPROXIMATE 0.50 INCH IN LENGTH AS MARKED AT STA Y=2164. CRACKED AREA REPAIRED PER EA NR 1-5530-T0326616 PT 1 TITLE: AD 98-25-15 - STABILIZERS - VERTICAL STABILIZER.SDR FDEA201607062294Skin · gougedTO COMPLY WITH EA 1-5730-T0320378, PART 4. WINGS, PLATES AND SKIN GOUGED AT STA XIS 250-XIS 256 APPROXIMATELY 8" FWD OF AFT EDGE L/E SKIN, RT WING.SDR FDEA201607062293Stringer · crackedLEFT WING, LT FIXED L/E AT STA XOS 669, STR FOUND CRACKED AS MARKED.SDR FDEA201607062292Stringer · crackedRIGHT WING, RT L/E AT STA XOS 669, STRINGER FOUND CRACKED AS MARKED.SDR FDEA201607062291Floor Support · corrodedMAIN DECK, AFT CABIN LT FLOOR SUPPORT AT STA 1887-2007, X=57 FOUND CORROSION AS MARKED.SDR FDEA201607062290Doubler · crackedRT WING, RT L/E AT STA XOS 639 BEADED DOUBLER FOUND CRACKED AS MARKED.SDR FDEA201607062289Doubler · crackedRT WING, RT L/E AT STA XOS 626 BEADED DOUBLER FOUND CRACKED AS MARKED.SDR FDEA201607062288Doubler · crackedRIGHT WING, RT L/E AT STA XOS 788.5 RIB DOUBLER FOUND CRACKED AS MARKED.SDR FDEA201607052276Longeron · corrodedCENTER CARGO COMPARTMENT, BILGE AREA FOUND LONGERON 52, STA 5-85, CORRODED AS MARKED.SDR FDEA201607052275Frame · dentedCABIN - RT STA 1741, LONGERON L-11R FRAME FOUND DENT.SDR FDEA201607052274Frame · dentedCABIN - LT STA 1761, LONGERON L-11L FRAME FOUND DENT.SDR FDEA201607052273Frame · crackedCABIN -RT STA 1761, LONGERON L-11R FRAME FOUND CRACKED.SDR FDEA201607052272Doubler · crackedLEFT WING L/E AT STA XOS 731 BEADED DOUBLER FOUND CRACKED AS MARKED. CRACKED DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607052271Doubler · crackedLEFT WING L/E AT STA XOS 669 BEADED DOUBLER FOUND CRACKED AS MARKED. CRACKED DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607052270Doubler · crackedLT WING L/E AT STA XOS 645 BEADED DOUBLER FOUND CRACKED AS MARKED. CRACKED DOUBLER REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042269Seat Track · crackedMAIN DECK RT FLOOR SEAT TRACK AT STA 635, X=-47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625-STA 645X= -47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042268Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X= 8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 745-STA 785 X= 8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042267Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 755, X=47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT IAW SRM 53-00-52-2R, FIG 201, REPAIR NR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042266Seat Track · corrodedMAIN DECK RT FLOOR SEAT TRACK AT STA 778, X=-74.5 FOUND CORROSION AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 765-STA 818 X= -74.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. COMPLIED WITH EA 1-5320-T0326733 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-SDR FDEA201607042265Seat Track · damagedMAIN DECK LT FLOOR SEAT TRACK AT STA 770, X= 74.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 765-STA 783 X=74.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042264Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 635, X= 47.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 665X=47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042263Seat Track · crackedMAIN DECK LT FLOOR SEAT TRACK AT STA 635, X= 8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625 TO STA 645 X=8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042262Seat Track · crackedMAIN DECK RT FLOOR SEAT TRACK AT STA 635, X=-8.5 FOUND CRACKED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 625-STA 645 X= -8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042261Seat Track · damagedMAIN DECK RT FLOOR SEAT TRACK AT STA 1425, X=-47.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1390 TO STA 1431 X = -47.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042259Seat Track · damagedMAIN DECK RT FLOOR SEAT TRACK AT STA 1285, X=-8.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1264 TO STA 1311 X= -8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100.SDR FDEA201607042258Seat Track · corrodedMAIN DECK LT FLOOR SEAT TRACK AT STA 1643, X= 8.5, FOUND CORROSION AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 1570 TO STA 1651 X=8.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042257Seat Track · damagedMAIN DECK LT FLOOR SEAT TRACK AT STA 5-5, X= 27.5, FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 TO STA 5-63 X=27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042256Seat Track · damagedMAIN DECK RT FLOOR SEAT TRACK AT STA 5-5, X= -27.5 FOUND CROWN DAMAGED AS MARKED. REPAIRED BY SECTIONAL REPLACEMENT FROM STA 5-0 TO STA 5-63 X= -27.5 IAW SRM 53-00-52-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042255Beam · crackedCABIN-L3 DOOR PLUG NR 7 FWD STOP FITTING BEAM FOUND CRACKED. R & R WITH NEW STOP FITTING BEAM IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042247Floor Support · corrodedMAIN DECK, AFT CABIN RT FLOOR SUPPORT AT STA 1887 - STA 2007, X=-25, FOUND CORROSION AS MARKED. R & R WITH NEW FABRICATED FLOOR SUPPORT IAW SRM 51-31-01-0G. NEW FLOOR SUPPORT FABRICATED IAW DWG AGA7087, REV P. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042246Web · crackedMAIN DECK L3 DOOR AFT JAMB LOWER WEB BOX AT STA 1305.25 TO 1315.42, LONGERON L26L TO L27L FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201 REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201607042245Web · crackedMAIN DECK L3 DOOR FWD JAMB LOWER WEB BOX AT STA 1250.75 TO 1256.75, LONGERON L26L TO L27L, FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201. REPAIR NR 3 AND EA 1-5310-T0326798A, PT 1 TITLE: FUSELAGE MAIN FRAME, CENTER FUSELAGE, OVERWISDR FDEA201607042244Web · crackedMAIN DECK R3 DOOR FWD JAMB LOWER WEB BOX AT STA 1250.75 TO 1256.75, LONGERON L26R-L27R, FOUND CRACKED AS MARKED. CARRIED OUT REPAIR IAW SRM 53-40-15-2R, FIG 201. REPAIR NR 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201605181732Seat Track · damagedSEAT TRACK DAMAGED AT POSITION 10L & 9L MCD & LOCK POSITION S1539. R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-00-52.SDR FDEA201601070076Lamp · inoperativeLEFT CABIN DOOR, FWD PRESS TO TEST SLIDE BOTTLE LIGHT INOPERATIVE. REPLACED THE LAMP IN THE L1 EVAC SLIDE REMOTE PRESSURE INDICATOR. OPS CHECKED NORMAL IAW 25-61-04-5.SDR FDEA201512184029Switch · inoperativeDON O2 MASK COURIER COMPARTMENT FAIL TO ILLUMINATE, DURING PREFLIGHT CHECK. R & R COURIER DON OXYGEN SWITCH PN JMS2109-42-20A IAW SWPM 20-00. OPERATIONS TESTED SATISFACTORY IAW AMM 35-21-07-5. ITEM OK FOR SERVICE.SDR FDEA201506031695Wire Harness · chafedDURING OFF LOAD RAMP, REPORTED CTR CARGO LOADING SYS IS INOPERATIVE. CHECKED & FOUND CTR CARGO LOADING SYS CB LATERAL ROLLERS & LOADING CONTROL, 2 EACH POPPED OUT. TROUBLESHOOTING FOUND WIRE HARNESS AGS 9122-J504 CHAFING WITH PANEL STRINGER, CAUSED BURNED WISDR FDEA201502130529Unknown · malfunctionedAFTER SWITCHING EMER POWER TO ARM DURING PREFLIGHT, WE RECEIVED A LEVEL ONE, EMER PWR TST FAIL, ALERT. CYCLED BATTERY CHARGER CB'S & PERFORMED RTS OF EPCU IAW AMM 24-08-01-5. ALL CHECKED NORMAL AT THIS TIME. PERFORMED EMER POWER TEST IAW AMM 24-24-00-5. OPESDR FDEA201412244183Lamp · inoperativeR1 DOOR EVACUATION SLIDE PRESS TO TEST SWITCH IS INOPERATIVE. R & R LAMP.SDR FDEA201408052080Cover · dislodgedR1 DOOR SLIDE COVER IS DISLODGED FROM DOOR. REINSTALLED EVACUATION SLIDE RAFT & CONTAINER. ALL TESTS SATISFACTORY.
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