Douglas DC-10-30F
Service difficulty reports · 1,152
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'DC1030F' 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 aircraft_model_key = 'DC1030F' 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 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 CLCA20080805001Smoke Detector · failedAFTER TAKEOFF, LWR FWD CARGO SMOKE DETECTOR POS. 1 LT ON, FOLLOWED BY FWD FIRE LT ON. CREW FOLLOWED PROCEDURES AND DISCHARGED NR1 FIRE BOTTLE CYLINDER. REPLACED NR1 FIRE BOTTLE AND 2 EA SQUIBS AND NR 1 FWD SMOKE DETECTOR. NO EVIDENCE OF FIRE AFTER POST FLIGHTSDR 08FDEA03254Floor 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 ARWA20080706Hydraulic System · lowNR 1 HYDRAULICS NEED SERVICING. SERVICED NR 1 HYDRAULIC SYSTEM AS REQUIRED IN ACCORDANCE WITH DC10 M/M 12-13-02; CHECKED FOR LEAKS IN ACCORDANCE WITH DC10 M/M 29-00-00, NO LEAKS NOTED. (A)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.SDR 08FDEA03013None · noneFWD CARGO COMPARTMENT STRUT SUPPORT BEAM NOT IN CONFIGURATION.SDR 08FDEA03012None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.SDR 08FDEA03011None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.SDR 08FDEA03010None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.SDR 08FDEA03009None · noneFWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION.SDR 08FDEA03007Seat Track · wornMAIN CARGO, LUGS ON SEAT TRACK ARE WORN AT FOUR PLACES BETWEEN FS 1249 - 1319 LBL 8. INSPECTED FOUND AREAS TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED NEW TRACK AND SPLICE HAT/PLATE AND INSTALLED ALL REPAIR PARTS ALL ON MAE TRAVILERS T8/748406, T8/SDR FDEA200807182982Engine · failedDURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFROMED PHASE 1'S AND QRH PROCEDURE. RETURN TO MEM FOR ENGINE OUT LANDING. MX MEM - INSPECTED NR 1 ENGINE. FOUND OIL PUDDLED IN EXHAUSDR 08FDEA02982Engine · failedDURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFORMED PHASE 1'S AND QRH PROCEDURE. RETURN TO MEM FOR ENGINE OUT LANDING. MX MEM, INSPECTED NR 1 ENGINE. FOUND OIL PUDDLED IN EXHAUSSDR 08FDEA02941Seat Track · wornMAIN CARGO, LUGS ON SEAT TRACK WORN AT FS 1406 LBL 47. REMOVED SEAT TRACK SECTION, FABRICATED NEW SECTION AND SPLICES INSTALLED NEW SECTION IAW SRM 53-70-00 ON TRAVELER T8/748310. MAJOR REPAIR.SDR 08FDEA02835Channel · corrodedFWD CARGO COMPT CHANNEL WITH SEVERE EXFOLIATION CORROSION. WORK COVERED BY NRC N00418.SDR FDEA200807092773Skin · dentedEXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2.50 INCH BY 1.50 INCH DEEP .082 INCH ON SKIN. REPAIRED SKIN IAW SRM 53-20-00 FIG 13 SHT 7 VOL I.SDR FDEA200807092772Skin · dentedEXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2 INCH BY 1 INCH DEEP .074 INCH ON SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 13 VOL I.SDR FDEA200807092770Skin · crackedEXT FUSELAGE LWR SURFACE FOUND CRACK ON SKIN (UPPER CORNER). REPAIRED SKIN IAW SRM 53-20-00 VOL I FIG 2.SDR 08FDEA02773Skin · dentedEXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2.50 INCH BY 1.50 INCH DEEP .082 INCH ON SKIN.SDR 08FDEA02772Skin · dentedEXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2 INCH BY 1 INCH DEEP .074" ON SKIN.SDR 08FDEA02771Skin · dentedDURING INSPECTION EXT FUSELAGE LWR SURFACE FOUND DEEP DENT AND NICK 3 INCH BY .75 INCH DEEP .047 INCH ON SKIN.SDR 08FDEA02770Skin · crackedEXT FUSELAGE LWR SURFACE FOUND CRACK ON SKIN (UPPER CORNER).SDR 08FDEA02385Beam · crackedWHILE PERFORMING J/C 8-2550-7-2354 PT 2 CTR CARGO HANDLING SYSTEM FOUND CRACK ON LOWER FLANGE OF BEAM. REPAIRED AREA IAW SRM 53-00-01 FIG 9 SHT 7 VOL I.
Back to Douglas DC-10-30F