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 08FDEA04724Skin · crackedLH WING L/E FOUND CRACK ON SKIN L/E.SDR 08FDEA04721Skin · crackedLT WING NR 4 SPOILER FOUND CRACK ON UPPER SURFACE SPOILER.SDR 08FDEA04718Angle · crackedLH WING SLATS FOUND CRACK ON ANGLE OUTBOARD SIDE NR 2 SLAT.SDR FDEA200811034676Floor Panel · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL WITH J/C MD10-0600C210-1 JR FOUND CRACK ON HORIZ WEB FLOOR. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.SDR FDEA200811034675Floor Panel · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL WITH J/C MD10-0600C210-1 JR FOUND CRACK ON HORIZ WEB FLOOR. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.SDR FDEA200811034674Floor Panel · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL WITH OAN J/C MD10- 0600C210-1JR FOUND CRACK ON HORIZ WEB FLOOR. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.SDR 08FDEA04676Web · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR.SDR 08FDEA04675Web · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR.SDR 08FDEA04674Web · crackedFLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR.SDR FDEA200810304625Skin · crackedDURING U/S INSP OF HORIZ STB, FOUND UPPER INTERIOR SKIN PANELS PN 7229-1, PN 7228-1 (POSITION 7 AND 11) WITH CRACK IN FLYABLE LIMITS, INSP FINDING FORM FOR DETAIL. ACCOMPLISHED EA NR 8-5510-125425.SDR 08FDEA04625Skin · crackedDURING U/S INSP OF HORIZONTAL STAB, FOUND UPPER INTERIOR SKIN PANELS P/N 7229-1, P/N 7228-1 (POSITION 7 AND 11) WITH CRACK IN FLYABLE LIMITS,SDR FDEA200810294607Handle · stuckON DEPARTURE FROM MEM GEAR HANDLE WOULD NOT MOVE TO UP POSITION RAN QRH PROCEDURE FOR GEAR HANDLE, WILL NOT MOVE TO UP POSITION UNABLE TO RAISE GEAR HANDLE RETURNED TO MEM.SDR 08FDEA04607Handle · malfunctionedON DEPARTURE FROM MEM, GEAR HANDLE WOULD NOT MOVE TO UP POSITION. RAN QRH PROCEDURE FOR GEAR HANDLE WILL NOT MOVE TO UP POSITION UNABLE TO RAISE GEAR HANDLE, RETURNED TO MEM.SDR 22AA20081006Slat · damagedON SERVICE CHECK, RT WING SLAT NR 8 LEADING EDGE DAMAGE. FOUND BIRD STRIKE ON RT WING SLAT NR 8 LEADING EDGE; INSPECTED RT WING SLAT NR 8 LEADING EDGE IN ACCORDANCE WITH DC10 M/M 05-62-00. PERFORMED TEMPORARY REPAIR IN ACCORDANCE WITH ENGINEERING AUTHORIZATISDR CLCA-1008-2Slide · unwanted deploy1R EMERGENCY SLIDE ACCIDENTALLY BLOWN. 1R EMERGENCY SLIDE ORDERED AND REPLACED.SDR 22AA20081004Engine · malfunctionedAFTER TAKEOFF HEARD LOUD NOISE. TOWER ADVISED, FLAMES COMING FROM AIRCRAFT AND NR 1 ENGINE EGT WENT TO RED LINE. ENGINE SHUTDOWN ON ITS OWN. ENGINE CHANGE IN PROGRESS.
SDR FDEA200810204445Pump · failedAT CRUISE FLT, NR 2 HYDRAULIC QTY AND PRESSURE WENT TO ZER0. NO HIGH TEMP INDICATED. COMPLIED WITH QRH AND RETURNED TO MEMPHIS. REMOVED AND REPLACED 2/1 NON-REV MOTOR PUMP SHUTOFF VALVE.SDR 08FDEA04445Pump · failedAT CRUISE FLT, NR 2 HYDRAULIC QTY AND PRESSURE WENT TO ZER0. NO HIGH TEMP INDICATED. COMPLIED WITH QRH AND RETURNED TO MEMPHIS. REMOVED AND REPLACED 2/1 NON-REV MOTOR PUMP SHUTOFF VALVESDR FDEA200810174387Bulkhead Web · crackedDURING INSP NLG W/W FOUND CRACK ON VERTICAL WEB. REPAIRED WEB IAW SRM 53-30-00 FIG 6 SHT 2-3 VOL I.SDR FDEA200810174386Intercostal · crackedRT WING LEADING EDGE FOUND INTERCOSTAL CRACK. REPAIR AREA IAW SRM 57-00-01 FIG 10 SHEET 1 VOL 1.SDR 08FDEA04387Pressure Panel · crackedDURING INSPECTION NLG W/W FOUND CRACK ON VERTICAL WEB.SDR 08FDEA04386Intercostal · crackedRT WING LEADING EDGE FOUND INTERCOSTAL CRACK.SDR FDEA200810154353Skin · dentedLOWER FUSELAGE DENT ON EXT SKIN DIM: 2" X 2" DEPTH 0.09". REPAIRED DENT IAW SRM 53-20-01 FIG 13 SHT 2A VOL I.SDR FDEA200810154352Skin · crackedLT WING L/E CRACK ON EXT LWR SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 VOL I.SDR 08FDEA04373Sense Line · leakingPNEU SUPPLY RED FAIL LIGHT ILLUMLINATED. PRESS GAUGE SYS NR 2 VERY HIGH, 30 PSI WOULD NOT GO DOWN WITH THROTTLE TO IDLE, SUPPLY PNEU SWITCH OFF, FINALLY PSI WENT TO 20 PSI. FOUND LEAKS ON LINE GOING TO FAN AIR VALVE. REMOVED AND REPLACED SENSE LINE PER SMSDR 08FDEA04353Skin · dentedLOWER FUSELAGE DENT ON EXT SKIN DIM, 2 INCH BY 2 INCH DEPTH 0.09 INCH.SDR 08FDEA04352Skin · crackedLT WING L/E CRACK ON EXT LOWER SKIN.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 22AA20081001Hydraulic Line · damagedAFTER CLOSING CARGO DOOR FOR DEPARTURE, HARD ODOR OF HYDRAULIC FLUID IN FLIGHT DECK. REMOVED AND REPLACED MAIN CARGO DOOR CLOSE LINE AS REQUIRED; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 52-34-01, NO LEAKS FOUND.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 22AA20080903Slide Raft · deployedL-1 DOOR SLIDE RAFT DEPLOYED. REMOVED L-1 DOOR SLIDE RAFT IN ACCORDANCE WITH DC-10 M/M 25-61-07; PERFORMED DOOR CHECK FOUND NORMAL IN ACCORDANCE WITH DC-10 M/M 52-11-07. TRANSFERRED TO DMI 22064 AS PER MEL 52-10-2, CAT "C". REMOVED & REPLACED L-1 DOOR RAFT SDR ARWA20080903Slide · unwanted deployL-1 DOOR SLIDE RAFT DEPLOYED. REMOVED L-1 DOOR SLIDE RAFT IAW MM 26-61-07, PERFORMED DOOR CHECK FOUND NORMAL IAW MM 52-11-07. TRANSFERRED TO DMI NR 22064 IAW MEL 52-10-2,, CAT (C). (K)SDR 08FDEA03885Line · leakingCENTER GEAR FAILED TO EXTEND WITH GEAR HANDLE. RAN CHECK LIST, CENTER GEAR EXTENDED WHEN THE CENTER GEAR ALTERNATE EXTENSION HANDLE WAS PULLED. ON LANDING ROLLOUT HYD QUE ILLUMINATED, HYD SYS 3 ELEV ILLUMINATED. FOUND HYD LINE TO CENTER GEAR UNLOCK CYLINDESDR 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 WRLA2008075Intercostal · corrodedDURING INSPECTION FOUND CORROSION RT MLG WW. STA 1505 AT LONGERON 31R, INTERCOSTAL SKIN ATTACH. REF DELTA NR40.SDR WRLA2008074Skin · corrodedDURING INSPECTION FOUND CORROSION RT MLG WW. STA 1505 AT LONGERON 35R SKIN, INTERCOSTAL AND FRAME ATTACH. REF DELTA NR 41.SDR WRL2008F00008Intercostal · corrodedDURING INSP, FOUND CORROSION IN THE RT MLG WHEEL WELL STA 1606 AT LONGERON 31R, INTERCOSTAL SKIN ATTACH, REF DELTA NR 40. REMOVED CORROSION ON SKIN AND FRAME AT LONGERON 31R BETWEEN STA 1505-1521, WITHIN LIMITS IAW SRM 53-00-01. TREAT AND PAINTED SKIN AND FRSDR WRL2008F00007Intercostal · corrodedDURING INSPECTION FOUND CORROSION IN THE RT MLG WHEEL WELL STA 1505 AT LONGERON 35 R SKIN INTERCOSTAL AND FRAME ATTACH, REF DELTA N/R 41. REMOVED CORROSION ON SKIN AND FRAME AT LONGERON 35R BETWEEN STA 1505-1521, WITHIN LIMITS IAW SRM 53-00-01, TREAT AND PAINTSDR 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 CLCA080802Tube · damagedNR (3) ENG FIRE WARNING CAME ON DURING CLIMB THROUGH 22KFT. ENG WAS SHUTDOWN IAW AOM PROCEDURE E-12, ACFT FUEL WAS DUMPED, AND ACFT RETURNED TO DEPARTURE. UPON EXTERIOR INSP OF THE ENG, DISCOVERED THE SEALS TO THE HIGH PRESSURE TURBINE (HPT), COOLING TUBE WAS
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