Douglas DC-8-72
Service difficulty reports · 201
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 = 'DC872' 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 = 'DC872' 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 2021F00362Duct · crackedFORWARD CARGO COMPARTMENT PNEUMATIC DUCT FOUND WITH 6" CRACK. REF NRC# B000386.SDR 2022F00019Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION FROM STA. 1100-1120 BL 0". REF NRC# B000312.SDR 2022F00018Seat Track · corrodedMAIN CABIN LWR SURFACE OF DOUBLE WIDE SEAT TRACK HAS CORROSION AT STA. 781 LBL 48. REF NRC# B000293.SDR 2021F00365None · noneR/H HORZ. STAB L/E I/B SECTION LOWER SURFACE HAS CORROSION AROUND 2 FASTENERS BETWEEN STA. XFS. 122.500 & 128.750, REF NRC B000142.SDR 2021FA0000324Rib · crackedL/H WING O/B LOWER RIB A IS CRACKED AT STA. XFS.= 616.250, REF. NRC B000110SDR E4EB20151115008Finger Doubler · brokenCOCKPIT SUBFLOOR RT SIDE CUSP AREA STATION 148, FINGER DOUBLER HAS MANY BROKEN OFF FASTENERS.SDR E4EB20151115007Seat Track · corrodedMAIN DECK CARGO COMPARTMENT, SEAT TRACK LUGS DAMAGED 2 PLACES STATION 834, LBL 24.SDR E4EB20151115006Cap · corrodedLT WING INBD LE FUEL TANK UPPER TE TEE CAP HAS INTERGRANULAR CORROSION. BETWEEN XFS 30.000 - 57.000.SDR E4EB20151115005Skin · corrodedLEFT HORIZONTAL STAB TIP HAS CORROSION ON SKIN AT STATIC WICK BASES.SDR E4EB20151115004Skin · corrodedLT WING UPPER SKIN HAS CORROSION AROUND FASTENERS, BETWEEN STRINGER 9 & FWD SPAR, BETWEEN XRS 255 - 289.28-063.SDR E4EB20151115003Skin · corrodedLT WING UPPER SURFACE HAS INTERGRANULAR CORROSION AROUND A FASTENER AT XRS763 & STRINGER 2 28-039.SDR E4EB20151115002Rivet · crackedLT INBD FLAP UPPER SURFACE INBD RUB PLATE HAS POPPED & CRACKED RIVETS 28-010.SDR E4EB20151115001Seat Track · corrodedMAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION AT SPLICE SAT 590, LBL 24.32-156.SDR 2015FA0000537Finger Doubler · corrodedCOCKPIT SUBFLOOR FINGER DOUBLER AT LT SIDE OF CUSP BS 148 IS LIFTED UP DUE TO POSSIBLE CORROSION UNDERNEATH AND FASTENER IS LOOSE.SDR E4EB2016F00009Finger Doubler · corrodedCOCKPIT SUBFLOOR FINGER DOUBLER AT LT SIDE OF CUSP WEB BS 148 IS LIFTED UP DUE TO POSSIBLE CORROSION UNDERNEATH AND FASTENER IS LOOSE.SDR E4EB2015110200536Skin · delaminatedRT WING OTBD FLAP, NR 4 VANE INBD UPPER SURFACE DENTED WITH DELAMINATION.SDR E4EB2016F00008Vane · delaminatedRT WING OTBD FLAP NR 4 FLAP VANE INBD UPPER SURFACE DENTED WITH DELAMINATION.SDR E4EB2015110200535Frame · corrodedFRAME BS 1060, UPPER CAP CORRODED INCLUDING EXFOLIATION AT SEVERAL PLACES FROM S34L TO S31R.SDR E4EB2015113020Finger Doubler · damagedCOCKPIT SUBFLOOR RT CUSP AREA, STATION 148, FINGER DOUBLER HAS MANY BROKEN OFF FASTENERS. REMOVED DOUBLER FITTING & ATTACHMENT. FABRICATED TWO EACH FINGER DOUBLERS & INSTALLED IAW SRM.SDR E4EB2015FA0000587Fitting · corrodedNR A017107, AFT ACCESSORY COMPARTMENT S32R END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.SDR E4EB2015FA0000586Fitting · corrodedNR A017106, AFT ACCESSORY COMPARTMENT S34R END FITTING AT AFT SIDE OF FRAME FS 1530 IS CORRODED.SDR E4EB2015FA0000585Fitting · corrodedAFT ACCESSORY COMPARTMENT S36 END FITTING AFT AFT SIDE OF FRAME FS 1530 IS CORRODED.SDR E4EB2016111400002Skin · corrodedLEFT WING UPPER SKIN HAS CORROSION AROUND FASTENERS AND VORTEX GENERATORS AT CENTER SPAR BETWEEN XW 408 AND XW 485.28-49.SDR IXXA20120306007OBattery · inoperativeEMERGENCY FLASHLIGHT IN PASSENGER COMPARTMENT, INBD POSITION HAS WEAK BATTERY. R & R RECHARGEABLE EMERGENCY BATTERY IAW MM 33-50-1. OPS CHECKED GOOD.SDR IXXA20110331002Longeron · corrodedDURING ROUTINE C-CHECK INSP FOUND AFT ACCESSORY COMPARTMENT LONGERON 23 RT CORRODED AT STA 1380.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW LONGERON SEGMENT AND SPLICERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTSSDR IXXA11SMN0062SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND AFT ACCESSORY COMPARTMENT AFT BATHTUB FITTING CRACKED AT STA 1530.000 LONGERON 34 LT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-21 AND SRM 51-3-1.SDR IXXA11SMN0055SSkin · wornDURING ROUTINE C CHECK INSP, FOUND LT OTBD FLAP UPPER SKIN WORN AT STA XF 169.000 - 213.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIRED PARTS IAW SRM CHAP 57-7-1, FIG 4 ITEM "C", DPS 4.710 SDR IXXA11SMN051SFitting · crackedDURING ROUTINE C-CHECK INSP FOUND RT MLG WHEEL WELL FITTING CRACKED AT STATION 920, LONGERON 24 RT. REMOVED CRACKED FRAME FITTING. FABRICATED SPLICERS, SHIMS AND DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING AND REPAIR PARTSDR IXXA10SMN010SSkin · dentedDURING ROUTINE C CHECK INSP FOUND RT OTBD FLAP LOWER SKIN DENTED AT STA XF 380.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PSDR IXXA10SMN006SSkin · wornDURING ROUTINE C CHECK INSP FOUND LT OTBD FLAP UPPER SKIN WORN AT STA XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRSDR IXXA10SMN003SSkin · deformedDURING ROUTINE C CHECK INSP FOUND RT OTBD AILERON LOWER SKIN L/E DEFORMED AT STA XA 724.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE. FOUND WITHSDR IXXA10SMN001SSkin · brokenDURING ROUTINE C CHECK INSP FOUND THE FWD PASSENGER DOOR OUTER SKIN UPPER PART EDGE BROKEN AND AFT UPPER CORNER DENTED. STRIPPED PAINT. REMOVED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED SKIN IAW SRM 52-3-2 FIGURESDR IXXA070037OWire · arcedDURING APPROACH INTO KBWI, THE FLIGHT ATTENDANT NOTICED A FLASH AT THE CIRCUIT PANEL ABOVE THE RIGHT AFT SERVICE DOOR. THE CREW CONTINUED WITH THE APPROACH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND POWER WIRES CONTACTING LATCH OTHER BEHIND SDR IXXA060610OCabin Pressure · unknownAFTER TAKEOFF FROM RJTY, THE AIRCRAFT WOULD NOT PRESSURIZE. THE CREW RETURNED TO RJYT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AIR-CONDITIONING PACK SYSTEM AND PERFORMED AN OPERATIONAL CHECK OF THE AIRCRAFT PACK SYSTEM. THE AIRCRAFT SSDR IXXA060604OSelector Valve · out of adjustDURING CRUISE FROM RJTY NUMBER ONE ENGINE FLAMED OUT AT FL340. THE CREW RETURNED TO RJTY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE, AND NO DEFECTS WERE FOUND. THE FUEL FILTER WAS REMOVED AND NO ABNORMAL CONTAMINATION WAS FOUND. NEW FUELSDR IXXA060603OEngine · flamed outDURING CLIMBOUT FROM RJTY AT FL390 NUMBER THREE ENGINE FLAMED OUT. THE CREW DESCENDED TO FL320 WITH IGNITERS IN BOTH AND OVERRIDE IN ALL ENGINES. APPROXIMATELY AT FL340 THE ENGINE RESTARTED, ALL INDICATIONS RETURNED TO NORMAL AND THE CREW CONTINUED THE FLIGHSDR IXXA060600OEngine · flamed outDURING CRUISE FROM FJDG TO WSAP NR 2 ENGINE FLAMED OUT. THE CREW CONTINUED TO WSAP WHERE THEY LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE IAW ALL APPLICABLE DATA. NO DEFECTS WERE FOUND. THE FUEL FILTERS WERE INSPECTED, NO CONTAMINATION FOUND. NEWSDR IXXA06SMN101SVent · crackedDURING ROUTINE C-CHECK INSPECTION, REMOVED THE FWD BUFFET VENT TRIMMER VALVE AND PLUG OUTLET ON FUSELAGE. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7. REMOVED FWD BUFFET VENT TRIMMER VALVE IAW DC-8 MM 38-20-11 PAGES 201-202. REMOVED EXISTING INTERNAL DOSDR IXXA06SMN067SPanel · displacedDURING ROUTINE C-CHECK INSPECTION, EO 25-DC8-520 R4 PARTITION UPPER ATTACHMENT RELOCATION TO FS-STC00171 LA-D. PERFORMED ALTERATION MAJOR IAW FAA FORM 8110-3 DATE 10-04-05. EO 25-DC-8-520 REV STATES 4 DATES 11-11-2005, ATI DWG C40-MO2 REV C DATE 10-04-05. FSDR IXXA06SMN068SNone · noneDURING ROUTINE C-CHECK INSPECTION, ELT ANTENNA REMOVAL AND BLANKING PLATE INSTALLATION. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-06-06, ENGINEERING AUTHORIZATION AA71-2 REV IR DATE 01-24-06. REMOVED ELT ANTENNA IAW DC-8 MM 25-60-0 PAGE 201. FABRICSDR IXXA06SMN066SNone · noneDURING ROUTINE C-CHECK INSPECTION, EO 25-DC8-198 R9 INSTALL COMAT BOX. PERFORMED MAJOR ALTERATION IAW FAA FORM 8110-3 DATE 09-23-05, ATI DWG A95166-4 REV N DATE 09-23-05. INSTALLED COMAT BOX IAW ATI DWG 95166-4. COMPLIED WITH EO 25-DC8-198.SDR IXXA06SMN065SDrain Mast · pluggedDURING ROUTINE C-CHECK INSPECTION, INSTL; FWD LAV DRAIN MAST PLUG AT LOWER CENTER LINE. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-19-06, ATI DWG H74-102 REV B DATED 01-19-06, EO SEMAN 2006114 DATED 01-19-06. REMOVED EXISTING DRAIN MAST IAW DC8 SRMSDR IXXA06SMN064SRepair · misinstalledDURING ROUTINE C-CHECK INSPECTION, RT INBD AILERON SHOWS SEVERAL SPOTS OF CORROSION AND NON STANDARD REPAIR ON LWR PLATING, STA XA 550.000. PERFORMED MAJOR REPAIR. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED EXISTING PANEL PLATING (CORRODED) + REPAIR NOSDR IXXA06SMN063SNone · noneDURING C CHECK, INSTALLATION OF DOUBLER ON FS 188.000 L-1 TO L-2R REQUIRED DUE TO SEXTANT EQUIPMENT REMOVAL. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06029 DATED 01-23-06, SEMAN DWG ED-4167 DATE 01-21-06, EO SEMAN # 2006100 DATE 01-23-06. REMOVED EXISTINSDR IXXA06SMN058SFitting · corrodedDURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPT- AFT SVC DOOR JAMB FITTING CORRODED, STA 1520.000 RBL 50. REMOVED CORROSION FROM FITTING IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED CORRODED FITTING IAW DC-8 SSDR IXXA06SMN059SPan · crackedDURING ROUTINE C CHECK INSPECTION, RT WING CTR L/E, ZEE-PAN CRACKED 1" AT STA XS 526.000. REMOVED CRACKED ZEE PAN IAW DC8 SRM 51-1-20D ATI REPAIR SPECIFICATION NR 2003-05, DWG DOUGLAS NR 5769 857. PERFORMED HEAT TREATMENT IAW DC8 SRM 51-1-1 PAGES 1, 13, 17. SDR IXXA06SMN062SPlug · installedDURING C CHECK, 'LAVATORY DRAIN HOLE PLUG INSTALLATION REQUIRED (STA 240.000 - 260.000, L-19R TO L-18R). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06029 DATED 01-23-06, SEMAN DWG ED-4168 DATED 01-21-06, EO SEMAN NR 2006101 DATED 01-23-06. REMOVED EXISTINSDR IXXA06SMN061SNone · noneDURING C CHECK, 'FWD LAVATORY DRAIN HOLE PLUG INSTALLATION REQUIRED, STA 270.000 - 280.000, L-22R TO L-23R. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 1 (SHEET 1, 3). REMOVED FASTENERS IAW DC8 SRM 51-3-0. CUT OUT AREA, FABRICATED REPAIR DOUBLER, (02EA) ISDR IXXA06SMN060SRepair · misinstalledDURING C CHECK, 'NON-STANDARD REPAIR ON FUSELAGE EXTERNAL SKIN (STA 1540.000 - 1550.000,L-17R TO L-19R. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 4, 5). REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTISDR IXXA06SMN057SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, 'FWD ACCY COMPT- L-34R CRACKED BETWEEN STA 208.000 - STA 270.000. REMOVED CRACKED L-34R IAW DC-8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW LONGERON WITH RIVETS + HILOKS IAW DC-8 SRM
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