N318FE
Service difficulty reports · 311
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 = 'N318FE' 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 = 'N318FE' 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 FDEA200906112037Generator · malfunctionedREJECTED TAKE-OFF X 2 FOR LEVEL 2 "GEN DRIVE 2 FAULT ". FIRST TIME CAME ON FOR 2 SECONDS. SECOND ATTEMPT CAME ON STEADY WITH POWER AT T/O THRUST. GEN DRIVE 2 FAULT CLEARED WITH POWER REDUCED. OPENED RT SIDE NR 2 ENGINE FAN COWL TO INSPECT NR 2 ENGINE GENERSDR FDEA200902120512Actuator · leakingLEFT BOGEY ACTUATOR LEAKING.SDR 08FDEA04907Door Frame · corrodedUPPER CARGO DOOR FOUND CORROSION ON UPPER EXT FACE OF LWR JAMB. REPAIRED AREA IAW EA NR 8-5310-125423.SDR FDEA200810174386Intercostal · crackedRT WING LEADING EDGE FOUND INTERCOSTAL CRACK. REPAIR AREA IAW SRM 57-00-01 FIG 10 SHEET 1 VOL 1.SDR 08FDEA04386Intercostal · crackedRT WING LEADING EDGE FOUND INTERCOSTAL CRACK.SDR 08FDEA04351Skin · dentedRT WING INBD FLAP FOUND DEEP DENT ON UPPER SKIN 0.50 INCH BY 0.50 INCH DEEP .062 INCH. REPAIRED AREA IAW SRM 57-10-00 FIG 85 SHT 1 VOL I.SDR 08FDEA03989Floor Skin · corrodedAFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND SEVERE CORROSION ON MEMBRANE. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.SDR FDEA200809193950Web · crackedENGINE PYLON NR 1 FOUND 3 CRACKS ON UPPER FWD SECTION STRUCTURE, RT SIDE, FIRST CRACK 2 INCHES LONG ON INT ANGLE AT STA YN 213, SECOND CRACK 2 INCHES LONG ON WEB AT STA YN 213 RT, THIRD CRACK 2 INCHES LONG ON WEB AT STA YN 213 LT. REPAIR AREA IAW SRM 54-20-00SDR 08FDEA03950Web · crackedENGINE PYLON NR 1 FOUND 3 CRACKS ON UPPER FWD SECTION STRUCTURE, RT SIDE, FIRST CRACK 2 INCHES LONG ON INT ANGLE AT STA YN 213, SECOND CRACK 2 INCHES LONG ON WEB AT STA YN 213 RT, THIRD CRACK 2 INCHES LONG ON WEB AT STA YN 213 LT.SDR 08FDEA03816Skin · dentedRT WING INBD FLAP FOUND DEEP DENT ON LOWER SKIN 0.25 INCH BY 0.25 INCH DEEP .074 INCH (SUSPECT CRACK ). REPAIRED DENT IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.SDR 08FDEA03815Skin · dentedRT WING INBD FLAP FOUND DEEP DENT ON LOWER SKIN 0.25 INCH BY 0.25 INCH DEEP .066 INCH (SUSPECT CRACK ). REPAIRED DENT IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.SDR FDEA200808293635Skin · wornRT WING L/E, FOUND DEEP WEAR ON SKIN AND PANEL LOWER SIDE L/E AT STA XORS 264. REPAIR AREA IAW SRM 57-00-01 VOL 1 SHT 3 FIG 1A.SDR FDEA200808293634Seat Track · corrodedMAIN DECK, FROM STA 808 TO STA 879 AT X=-75, CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIR PER SRM 53-70-00 VOL 1 FIG 1 SHEET 1.SDR 08FDEA03635Skin · wornRT WING L/E, FOUND DEEP WEAR ON SKIN AND PANEL LOWER SIDE L/E AT STA XORS 264. REPAIR IAW SRM 57-10-00 VOL 1 FIG 15 .SDR 08FDEA03634Seat Track · corrodedMAIN DECK, FROM STA 808 TO STA 879 AT X=-75, CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIR PER SRM 53-70-00 VOL.1 FIG.1 SHEET 1.SDR FDEA200808183474Skin · dentedRT STAB INBD ELEV, XE 118, DENT ON UPPER SKIN. DIMENSIONS ARE 1 INCH BY 1 INCH BY .075 INCH. REPAIR SKIN IAW SRM 55-00-01 VOL 1 FIG 3 SHEET 2.SDR FDEA200808183473Skin · dentedRT STAB INBD ELEV, XE 136, DENT ON UPPER SKIN. DIMENSIONS ARE 1 INCH AND 1 INCH BY .075 INCH. REPAIR SKIN IAW SRM 55-00-01 FIG 3 SHEET 2 VOL 1.SDR 08FDEA03474Skin · dentedRT STAB INBD ELEV, XE 118, DENT ON UPPER SKIN. DIMENSIONS ARE 1 INCH BY 1 INCH BY .075 INCH. REPAIR SKIN IAW SRM 55-00-01 VOL 1 FIG 3 SHEET 2.SDR 08FDEA03473Skin · dentedRT STAB INBD ELEV, XE 136, DENTED ON UPPER SKIN. DIMENSIONS ARE 1 INCH BY 1 INCH BY .075 INCH. REPAIR SKIN IAW SRM 55-00-01 FIG 3 SHEET 2 VOL.1.SDR FDEA200808123380Frame · crackedRT AIR COND COMPT FOUND CRACK ON CAP OF FRAME, SEE NRC N00755 AND N00756. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I.SDR 08FDEA03380Frame · crackedRT AIR COND COMPT FOUND CRACK ON CAP OF FRAME.SDR FDEA200808073298Former · crackedLT WING L/E INT FOUND CRACK ON FORMER. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I.SDR FDEA200808073297Frame · crackedAVIONIC COMPT FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I.SDR 08FDEA03303Frame · wornLT AIR COND COMPT FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-00-00 FIG 4A VOL I.SDR 08FDEA03298Former · crackedLT WING L/E INT FOUND CRACK ON FORMER.SDR 08FDEA03297Frame · crackedAVIONIC COMPT FOUND CRACK ON FRAME.SDR FDEA200808053254Floor Panel · crackedAFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED AREA IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.SDR FDEA200808053253Floor Panel · crackedAFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED AREA IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.SDR FDEA200808053252Beam · corrodedFWD CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON BEAM LOWER SIDE. REPAIRED AREA IAW SRM 53-00-01 FIG 9 VOL I.SDR FDEA200808053251Web · crackedRT AIR COND COMPT FOUND CRACK ON VERTICAL WEB. REPAIRED AREA IAW SRM 53-40-00 FIG 34 VOL I.SDR FDEA200808053250Strut · corrodedAFT FUSELAGE WASTE TANK COMPT, FOUND EXFOLIATION CORROSION ON STRUT BULKHEAD. REPAIRED AREA IAW SRM 53-00-01 FIG 7 VOL I.SDR 08FDEA03254Floor Panel · crackedAFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE.SDR 08FDEA03253Floor Panel · crackedAFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE.SDR 08FDEA03252Beam · corrodedFWD CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON BEAM LOWER SIDE.SDR 08FDEA03251Bulkhead · crackedRT AIR COND COMPT FOUND CRACK ON VERTICAL WEB.SDR 08FDEA03250Strut · corrodedAFT FUSE WASTE TANK COMPT, FOUND EXFOLIATION CORROSION ON STRUT BULKHEAD.SDR FDEA200808013208Skin · crackedLT WING OTBD FLAP FOUND CRACKS ON LWR SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 65 VOL I.SDR FDEA200808013207Beam · crackedFWD CARGO COMPT, CRACK ON BEAM. REPAIRED BEAM IAW SRM 53-60-01 FIG 3 VOL I.SDR 08FDEA03206Channel · corrodedFWD CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON CHANNEL UPPER SIDE. REPAIRED CHANNEL IAW SRM 53-70-00 VOL I FIG 7.SDR 08FDEA03208Skin · crackedLT WING OUTBD FLAP FOUND CRACKS ON LWR SKIN.SDR 08FDEA03207Floorbeam · crackedFWD CARGO COMPT, CRACK ON BEAM.SDR FDEA200807303165Skin · crackedDURING INSPECTION RT WING SLAT NR 2 FOUND CRACK ON INNER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 31 VOL I.SDR 08FDEA03165Skin · crackedDURING INSPECTION RT WING SLAT NR 2 FOUND CRACK ON INNER SKIN.SDR 08FDEA03037Skin Panel · crackedDURING INSPECTION OF COSTANT AND OUTER SECTION MACHINED SKIN PANELS ON HORIZONTAL STAB, FOUND NR 5 PANELS WITH CRACK, ARE WITHIN LIMITS IAW TABLE MM PANELS P/N: 7228-1, 7227-1, 7281-2, 7226-1 AND 7225-1SEE ATTACHED SHEET FOR DETAIL.SDR FDEA200807233027Skin · wornRT WING L/E SLAT NR 6 FOUND DEEP WEAR INTERNAL SIDE. REPAIRED AREA IAW SRM 57-10-00 FIG 30 SHT 1 VOL I.SDR 08FDEA03027Skin · wornRT WING L/E SLAT NR 6 FOUND DEEP WEAR INTERNAL SIDE.SDR 08FDEA03026None · noneMAIN CABIN EXISTING ANGLE REPAIR ON TEE FLOOR SUPPORT.SDR FDEA200807223014Skin · crackedRT WING L/E FOUND CRACK ON LEADING EDGE LOWER EXTERNAL SIDE. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.SDR FDEA200807223013Support Beam · unknownFWD CARGO COMPARTMENT STRUT SUPPORT BEAM NOT IN CONFIGURATION. REPLACED SUPPORT IAW DWG AFA0039.SDR 08FDEA03014Skin · crackedRT WING L/E FOUND CRACK ON LEADING EDGE LOWER EXTERNAL SIDE.
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