N577FE, cancelled Mar 2, 2024
Service difficulty reports · 256
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 = 'N577FE' AND deregistration_id = 'N577FE-2024-03-02' 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 = 'N577FE' AND deregistration_id = 'N577FE-2024-03-02' 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 FDEA201310022380Window · looseLEFT SIDE COCKPIT ESCAPE ROPE VIEWING DOOR GLASS IS LOOSE. CORRECTLY INSTALLED VIEWING GLASS.SDR FDEA201204241541Skin · misrepairedRT WING NR 5 SLAT AFT SURFACE OTBD LOWER CORNER STA XORS 682 MISREPAIRED. REPAIRED IAW EA 1-5750-160032. CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 114.SDR FDEA201204241539Skin · misrepairedRT WING NR 8 SLAT UPPER SURFACE STATION XORS 995 MISREPAIRED. REPAIRED IAW EA 1-5750-160031 PART 1. CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 114.SDR FDEA201204191487Skin · misrepairedNR 2 PYLON EXTERIOR APPROX STA Y = 2334 FOUND MISREPAIRED. REPAIRED IAW EO E1-5100-7-5001B PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204171449Skin · misrepairedLT WING SKIN AT NR 3 SLAT LOWER SURFACE XORS 372. REPAIRED IAW EA1-5750-159830. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204161431Skin · misrepairedSKIN AT BS 2147 - 2160, L33L MISREPAIRED. REPAIRED IAW SRM 53-70-01 FIGURE 201 REPAIR 3 REVISION 49 & EO E1-5100-7-5001B PT1. MAJOR REPAIR.SDR FDEA201204141399Attach Fitting · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION AROUND STOP DRILL HOLE OF LT NOSE LANDING GEAR TRUNNION FITTING FOUND ONE NEW ADDITIONAL CRACK PROPAGATED FROM THE STOP DRILL HOLE TOWARDS THE LOWER EDGE, APPROX 0.25". REPAIR CARRIED OUT AT LT NLG TRUNNION FITTINSDR FDEA201204121373Longeron · crackedFOUND LONGERON 49 LT FASTENER HOLE (COMMON TO NLG TRUNNION FITTING) CRACKED , APPROX 0.025". LONGERON REMOVED IAW SRM 51-31-01, REV 49. NEW LONGERON FABRICATED IAW DWG ACA 3796 REV A. NEW FABRICATED LONGERON INSTALLED IAW SRM 51-31-01, REV 49. REPAIR CLASSSDR FDEA201204101337Frame · misrepairedFRAME STA 535 AT LONGERON 19 LT MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204101335Skin · misrepairedRT WING INBD FLAP UPPER SURFACE MISREPAIRED. REPAIRED IAW SRM 57-00-01, FIG 201, REPAIR 1, REV 49.SDR FDEA201204101334Frame · misrepairedCABIN AT FRAME BS 535, LONGERON 23L FOUND MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 201 REPAIR 1, REV 49. CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204101344Skin · corrodedMAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN BS 1219 TO 1239, "X" = -90 TO "X" = -107.5 FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.180", REMAINING THICKNESDR FDEA201204101343Skin · corrodedMAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN BS 1219 TO 1239, "X" = -75.25 TO "X" = -90 FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.168", REMAINING THICKNSDR FDEA201204101342Skin · corrodedMAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN STATION 1219 TO STATION 1239, "X" = -75.25. FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.171", REMAINING TSDR FDEA201204101341Skin · corrodedMAIN DECK UPPER CARGO COMPARTMENT, UNDER FLOOR AT CENTER WING TANK BETWEEN STATION 1219 TO STATION 1239, "X" = -27.5 FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.175", REMAINING THSDR FDEA201204101340Skin · corrodedMAIN DECK UPPER CARGO COMPARTMENT, UNDER FLOOR AT CTR WING TANK BETWEEN BS 1219 TO 1239, "X" = -8.5 TO "X = -27.5. FOUND SURFACE CORROSION AT FASTENERS AREA. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL MATERIAL THICKNESS = 0.182", REMAINING THICKNSDR FDEA201204101339Longeron · corrodedCENTER CARGO COMPARTMENT, BILGE AREA BS 1646 LONGERON 50 LT FOUND WITH SURFACE CORROSION. REPAIR CARRIED OUT AT CENTER CARGO COMPARTMENT BILGE AREA STA 1646, LONGERON 50L IAW EA 1-5310-159838. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204101338Longeron · corrodedCENTER CARGO COMPARTMENT BS 1676 LONGERON 51 LT FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-05, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204101333Skin · crackedLOWER VERTICAL STABILIZER FOUND RT SIDE REAR CENTER SPAR TO REAR SPAR LOWER PANEL CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201, REPAIR 2, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114. NR 2 ENGINE FIRE DETECTION CONTROL UNIT CARRIEDSDR FDEA201204101332Skin · corrodedAFT ACCESSORY COMPARTMENT, FOUND CORROSION ON RT SKIN BS 2163 BODY FAIRING CUTOUT LOCATION. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL THICKNESS: 0.95", MATERIAL REMOVED: 0.80", REMAINING 0.015" AND FOUND EXCEED LIMIT IAW SRM 53-70-01, FIG 201, RESDR FDEA201204091326Longeron · corrodedCENTER ACCESSORY COMPARTMENT STA 6-95, LONGERON 43 RT FOUND WITH CORROSION. REPAIRED IAW EA 1-5310-157171, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204091324Bushing · wornRT WING (FLAP SIDE) OTBD FLAP, OTBD HINGE, OTBD PIVOT HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.152" AND FOUND EXCEED LIMIT IAW CMM 57-52-04, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.150". REPAIR ACCOMPLISHEDSDR FDEA201204091323Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, OTBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER 1.222". FINAL BORE DIAMETER 1.246", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR CARRIED OUT EA 1-SDR FDEA201204091322Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER = 1.2215", FINAL BORE DIAMETER 1.246", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED ESDR FDEA201204091321Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE, LOWER MOUNT, OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. OTBD BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER = 0.597", FINAL BORE DIAMETER 0.612", MSDR FDEA201204091320Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT, INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. INBOARD HOLE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER = 0.581", FINAL BORE DIAMETER 0.612",SDR FDEA201204091319Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, INBD HINGE, OTBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. ORIGINAL BORE DIAMETER = 1.2295", FINAL BORE DIAMETER 1.236", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED ESDR FDEA201204091318Bushing · wornLT WING (WING SIDE) OTBD FLAP, INBD HINGE, INBD ACTUATOR HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, DIAMETER = 1.231" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPSDR FDEA201204091317Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. EXISTING HOLE DIAMETER :0.707", FINAL HOLE DIAMETER 0.713", MAXIMUM ALSDR FDEA201204091316Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 72. UPPER EXISTING THICKNESS: 0.400", MATERIAL REMOVED: 0.004", REMAINING THICKNESS: 0.396". LOWER EXISTING THICKNESS: 0.387", MATERIAL REMOVSDR FDEA201204091314Bushing · wornLT WING (WING SIDE) OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE DIAMETER 1.251" AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. MAXIMUM ALLOWABLE DIAMETER: 1.220". REPAIR ACCOMPLISHED EA 1-5750-SDR FDEA201204091312Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORROSION. REWORKED IAW CMM 20-11-02, REVISION 72. UPPER EXISTING THICKNESS: 0.425", MATERIAL REMOVED: 0.009", REMAINING THICKNESS: 0.416". LOWER EXISTING THICKNESS: 0.413", MATERIALSDR FDEA201204091311Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, OTBD HINGE, SIDE LOAD FITTING LOWER HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE REWORKED AND FOUND EXCEEDED LIMIT CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.389", FINAL HOLE DIAMETER 0.408", MAXIMUMSDR FDEA201204091310Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, OTBD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. UPPER HOLE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.389", FINAL HOLE DIAMETER 0.408",SDR FDEA201204091309Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT, OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. OTBD BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.581", FINAL HOLE DIAMETER 0.596", MAXIMSDR FDEA201204091308Hinge Fitting · corrodedLT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. INBD BORE REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING HOLE DIAMETER 0.580", FINAL HOLE DIAMETER 0.5975", MAXISDR FDEA201204091307Bushing · wornRT WING (WING SIDE) OTBD FLAP, INBD HINGE, OTBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, DIAMETER 1.252" FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. MAXIMUM ALLOWABLE DIAMETER: 1.220". REPAIR ACCOMPLISHED IAW SDR FDEA201204091306Hinge Fitting · damagedRT WING (WING SIDE) OTBD FLAP, INBD HINGE, INBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.253" AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. MAXIMUM ALLOWABLE DIAMETER 1.220", REPAIR ACCOMPLISHED IAW ESDR FDEA201204091305Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. LOWER MOUNT INBD BORE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING BORE DIAMETER 0.705", FINAL BORE DIAMETER 0.7SDR FDEA201204091304Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE, FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. LOWER MOUNT OTBD BORE REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-08, REV 72. EXISTING BORE DIAMETER 0.708", FINAL BORE DIAMETER 0.7SDR FDEA201204091303Hinge Fitting · corrodedRT WING (WING SIDE) OTBD FLAP, INBD HINGE SIDE LOAD FITTING SURFACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02 REV 72. UPPER EXISTING THICKNESS: 0.412", MATERIAL REMOVED: 0.005", REMAINING THICKNESS: 0.407". LOWER EXISTING THICKNESS: 0.403", MATERIAL REMOSDR FDEA201204091301Hinge Fitting · damagedLEFT WING (FLAP SIDE), INBD FLAP OTBD HINGE, OTBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, OTBD LUG DIAMETER 1.254", OTBD STRAP DIAMETER 1.190" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DSDR FDEA201204091300Hinge Fitting · damagedLEFT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, INBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURE, INBD LUG, DIAMETER 1.283", INBD STRAP DIAMETER 1.217" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DISDR FDEA201204091299Hinge Fitting · damagedRT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, OTBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, OTBD LUG DIAMETER 1.250", OTBD STRAP DIAMETER 1.21" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIAMSDR FDEA201204091298Hinge Fitting · damagedRT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, INBD PIVOT HOLE FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURE, INBD LUG DIAMETER 1.252 IN, INBD STRAP DIAMETER 1.218" AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 72. MAXIMUM ALLOWABLE DIASDR FDEA201204071285Skin · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON LT WING FUEL TANK LOWER ACCESS DOOR PANEL NR 536AB CUTOUT AND FOUND CRACK INDICATION ON 04 EACH FASTENER HOLES. REPAIR CARRIED OUT IAW EA 1-5710-157169 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 11SDR FDEA201204071284Skin · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON RT WING FUEL TANK LOWER ACCESS DOOR PANEL NR 636AB CUTOUT AND FOUND CRACK INDICATION ON 06 EACH FASTENER HOLES. REPAIR CARRIED OUT IAW EA 1-5710-157168 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 11SDR FDEA201204061275Skin · crackedRIGHT WING LOWER FIXED L/E AT REFUELING PANEL CUTOUT INBD FORWARD CORNER AREA FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02. REPAIR 7 FIG 201 REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 114.SDR FDEA201204051266Skin · misrepairedLT WING DROOP L/E UPPER SURFACE FOUND MISREPAIRED IAW SRM 57-40-01, REPAIR 5, FIGURE 201. REPAIRED IAW EA 1-5730-159836, CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201204051270Skin · crackedRT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK LOWER CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK LOWER CUTOUT IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, RE
Back to N577FE, cancelled Mar 2, 2024