Douglas DC-8-62F
Service difficulty reports · 1,163
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 = 'DC862F' 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 = 'DC862F' 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 IXXA06SMN211SStructure · dentedDURING ROUTINE C CHECK INSPECTION, RT HORIZONTAL STABILIZER WITH 02 DENTS , XFS 103.760 - XFS 141.750.SDR IXXA06SMN202SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING OTBD AILERON LWR SKIN DENTED, XA 618.000.SDR IXXA06SMN201SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING OTBD AILERON LWR SKIN DENTED, XA 715.000.SDR IXXA06SMN200SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT HORIZONTAL STABILIZER.- ELEVATOR UPPER SKIN DENTED XE 60.125.SDR IXXA06SMN199SDoor Frame · crackedDURING ROUTINE C CHECK INSPECTION, EXT FUSELAGE "D" BELLY DOOR FWD LWR JAMB CORNER CRACKED 1 1/2" STA 1240.000 L-32R.SDR IXXA06SMN208SRepair · improperDURING ROUTINE C CHECK INSPECTION, RT OTBD AILERON LWR SKIN NON STANDARD REPAIR, XA 680.000 - XA 685.000.SDR IXXA06SMN207SSkin Panel · damagedDURING ROUTINE C CHECK INSPECTION, LT WING INBD FLAP PANEL UPPER SKIN HOLES ELONGATED, XW 40.000.SDR IXXA06SMN206SSkin Panel · dentedDURING ROUTINE C CHECK INSPECTION, LT WING INBD FLAP PANEL UPPER SKIN DENTED, XW 45.000.SDR IXXA06SMN205SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING.- OTBD AILERON LWR SKIN DENTED , XA 661.000.SDR IXXA06SMN204SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING OTBD AILERON LWR SKIN DENTED, XA 647.000.SDR IXXA06SMN203SSkin · dentedDURING ROUTINE C CHECK INSPECTION, LT WING OTBD AILERON LWR SKIN DENTED, XA 640.000.SDR IXXA06SMN209SSkin · dentedDURING ROUTINE C CHECK INSPECTION FOUND LEFT HAND WING FLAP PANEL UPPER SKIN DENTED AT STATION XF 364.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIGURE 4 TR NUMBER 5794 DATED 10-01-02. REMOVED DAMAGED PANEL SKIN IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21.SDR IXXA06SMN190SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE SPLICE FITTING CRACKED 1", L17R, STA 1566.000. REPAIRED PER ALL APPROVED DATA.SDR IXXA06SMN189SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE.- SPLICE FITTING CRACKED 1", L-17L, STA 1566.000. REPAIRED PER ALL APPROVED DATA.SDR IXXA06SMN186SFitting · crackedDURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE.- RT SPLICE FITTING CRACKED 1", L-10R, STA 1566.000. REPAIRED PER ALL APPROVED DATA.SDR IXXA06SMN185SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FWD CARGO CMPT, LT TUNNEL SPLICE FITTING CRACKED 3, STA 600.000 - STA 620.000 L-26L. REPAIRED PER ALL APPROVED DATA.SDR IXXA06SMN184SPanel · crackedDURING ROUTINE C CHECK INSPECTION, LT WING INBD L/E UPPER SLANT PANEL CORRODED ON SOME AREAS, STA XFS 194.000. REPAIRED PER ALL APPROVED DATA.SDR IXXA06SMN183SPanel · crackedDURING ROUTINE C CHECK INSPECTION, LT WING INBD L/E UPPER SLANT PANEL CORRODED ON SOME AREAS, STA XFS 194.000. REPAIRED PER ALL APPROVED DATA.SDR IXXA06SMN182SPanel · crackedDURING ROUTINE C CHECK INSPECTION, LT WING INBD L/E UPPER SLANT PANEL CORRODED ON SOME AREAS, STA XFS 80.000. REPAIRED PER ALL APPROVED DATA.SDR IXXA06SMN181SSupport Fitting · crackedDURING ROUTINE C CHECK INSPECTION RT MLG SUPPORT FITTING UPPER PART EDGE , STA 902.000 CRACKED 1 1/2" APPROX. REPAIRED PER ALL APPROVED DATA.SDR IXXA06SMN195SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, NR 1 LT STUB WING UPPER SKIN CORRODED ON SOME AREAS, STA XFS 554.000.SDR IXXA06SMN194SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LT WING OTBD L/E OUTER SECTION UPPER SKIN CORRODED ON SOME AREAS, STA XFS 803.000.SDR IXXA06SMN193SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, NR 1 LT STUB WING UPPER SKIN CORRODED ON SOME AREAS, STA XFS 530.000.SDR IXXA06SMN192SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LT WING OTBD L/E OUTER SECTION UPPER SKIN CORRODED ON SOME AREAS , STA XFS 747.000.SDR IXXA06SMN191SPanel · corrodedDURING ROUTINE C CHECK INSPECTION, LT WING INBD L/E UPPER SLANT PANEL CORRODED ON SOME AREAS (STA XFS 126.000 - 145.000)SDR IXXA06SMN180SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FRAME FITTING CRACKED 1" APPROX , STA 960.000 L-24R.SDR IXXA06SMN188SLongeron · crackedDURING ROUTINE C CHECK INSPECTION FOUND AFT FUSELAGE LONGERON 17 LEFT CRACKED ½ INCH AT STATION 1620.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-5-2 FIGURE 5, SHEET 1. REMOVED CRACKED LONGERON IAW DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-20D. FABRICSDR IXXA06SMN187SLongeron · crackedDURING ROUTINE C CHECK INSPECTION FOUND FUSELAGE LONGERON 17 RIGHT CRACKED ½ INCH, AT STATION 1620.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-5-2 FIGURE 5, SHEET 1. REMOVED DAMAGED LONGERON IAW DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-20D. FABRICATSDR IXXA060452OControl Valve · leakingAPPROXIMATELY 2 AND A HALF HOURS INTO CRUISE FROM TAPA TO FHAW, THE HYDRAULIC QUANTITY STARTED DECREASING. THE CREW SWITCHED TO EMERGENCY, AND THE LOSS OF HYDRAULIC FLUID STOPPED. LOSS OF HYDRAULIC FLUID CHECK LIST WAS COMPLIED WITH AND THE CREW RETURNED TO SDR IXXA060450OPrbc · stickingDURING TAKE-OFF FROM KWRI NUMBER 3 ENGINE FAILED TO ACHIEVE TAKE-OFF POWER. THE FLIGHT CREW REJECTED THE TAKE-OFF AND RETURNED TO PARKING. MAINTENANCE TROUBLESHOT THE DISCREPANCY AND FOUND THE PRESSURE RATIO BLEED CONTROL VALVE STICKING. MAINTENANCE REPLACED TSDR IXXA060436OPrbc · malfunctionedDURING TAKE-OFF FROM LPLA NUMBER 3 ENGINE DID NOT ACHIEVE TAKE-OFF POWER. THE CREW REJECTED THE TAKE-OFF AT 100 KNOTS AND RETURNED TO BLOCKS. MAINTENANCE FOUND THE PRBC TO BE DEFECTIVE. THE PRBC WAS REPLACED AND THE OPERATIONAL CHECK WAS SATISFACTORY, THE AIRCSDR IXXA060174OFan · malfunctionedDURING CRUISE FROM OBBI LEFT RECIRC FAN WAS SHUTDOWN AND CIRCUIT BREAKERS WERE PULLED DUE TO ELECTRICAL FUMES. CREW LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE RECIRC FAN ON DMI AND AIRCRAFT WAS RETURNED TO SERVICE.SDR IXXA0600087ORelief Valve · misinstalledAT LEVEL OFF, THROTTLES REDUCED TO CRUISE PWR NR 1 ENG OIL PRESS LIGHT CAME ON. OIL PRESS IND 10 PSI. CREW SHUTDOWN ENG. LANDED W/O INCIDENT. MX VERIFIED NO SIGNIFICANT OIL LOSS. C/W ABNORMAL OIL PRESS INSPECT. INSPECT MAIN FILTER AND SCAV PUMP INLET SCREENS &SDR IXXA0500130OFan · brokenDURING CRUISE FROM VTBU, A SLIGHT BURNING SMELL WAS DETECTED DURING CRUISE WHEN USING LEFT RECIRC FAN. FAN WAS TURNED OFF AND SMELL WENT AWAY. MAINTENANCE REMOVED AND REPLACED THE LT RECIRC FAN IAW ALL APPLICABLE MANUALS. THE AIRCRAFT WAS RETURNED TO SERVICSDR ARWA20050901Bleed Valve · failedABORTED TAKEOFF AT 60 KNOTS UPON HEARING A LOUD BANG; NR 1 ENGINE COMPRESSOR STALLED. REMOVED AND REPLACED BLEED VALVE AND CONTROL COMPRESSOR IN ACCORDANCE WITH M/M 75-30-3; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH 75-30-0. PERFORMED BORESCOPE INSPECTION SDR ARWA20050805Bearing · damagedAFTER TAKEOFF; DOOR NOT LATCHED, LIGHT REMAINED ON; COMPLETED PROPER CHECKLIST AND UNABLE TO HAVE SATISFACTORY UPLATCH CHECKLIST; HAD TO DUMB FUEL AND RETURN TO STATION. ACCOMPLISHED GEAR SWING FOR TROUBLESHOT; FABRICATED DOOR ASSEMBLY AND PERFORMED GEAR SWINSDR IXXA05RNG049SSkin · dentedDURING INSPECTION CHECK, SKIN DENT AND SCRATCH DAMAGE WAS FOUND ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE AT UPPER PLATING AROUND L/E STATION XFS 146.00. REMOVED DAMAGE AREA AND DOUBLER WAS INSTALLED IAW EWO ATI 55-05 & EO ATI-071905. EDDY CURRENT INSPESDR ARWA20050804Crank Assy · brokenWHEN POWER SET FOR TAKEOFF, TAKEOFF WARNING HORN SOUNDED AND SPOILER EXTENDED LIGHT ILLUMINATED. REMOVED AND REPLACED BROKEN GROUND SPOILER ACTUATION CRANKS IAW MM; RE-SAFETIED ALL PREVIOUSLY REMOVED HARDWARE. PERFORMED FUNCTIONAL CHECK OF GROUND SPOILERS PASDR IXXA0500089OTransceiver · no indicationIN CLIMB FROM KWRI, THE AIRCRAFT'S WEATHER RADAR WOULD NOT PAINT WEATHER OR GROUND. CREW RETURNED AIRCRAFT TO KWRI AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR TRANCEIVER AND WEATHER RADAR ANTENNA. THE SYSTEMS OPERATIONAL SDR IXXA05RNG040SSkin · dentedDURING INSPECTION CHECK, FOUND A DENT AT WING OUTER INBOARD EXTENDED LEADING EDGE PLATING STA XFS 610 TO SPAR LT. EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-032 AND SRM 57-2-1 FIGURE 2H.SDR IXXA05RNG044SSkin · corrodedDURING A ROUNTINE C CHECK INSPECTION FOUND CORROSION ON LOWER SKIN STA 1440-1530 LONGERON 31RH- 31LH. SKIN STA 1440-1530 LONGERON 31R-31L WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5615374, AND EXTERNAL SPLICE, INTERNAL SPLICE, FINGER DOUBLER AND LONGERONSDR IXXA05RNG041SPlate · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION AT WING OUTER INBD EXTENDED LE PLATING A STA XFS XW 560 TO SPAR RT. CORROSION ON RT WING L/E LOWER SKIN WAS REMOVED AND REPAIR WAS ACCOMPLISHED IAW EWO ATI-57-033 AND SRM 57-2-1 FIGURE 2H.SDR ARWA20050702Anti-Ice Valve · malfunctionedDURING TAXI OUT, NR 1 ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED; FOLLOWED ABNORMAL PROCEDURE; RETURN TO RAMP. REMOVED AND REPLACED NR 1 ENGINE RT ANTI-ICE VALVE IN ACCORDANCE WITH MM 75-10-1; OPERATIONAL CHECK IN ACCORDANCE WITH MM 75-10-0 AND MM 71-0 FOUND NORSDR IXXA05RNG031SSupport Fitting · crackedDURING ROUTINE "0C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF409.664 WAS FOUND CRACKED (LONG 1.570"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-021 & EO ATI-070705. FAA FORM 8110-3 WAS ISSUED APPROSDR IXXA05RNG030SSupport Fitting · crackedDURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 409.664 WAS FOUND CRACKED (LONG: 3.178"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-020 & EO ATI-070605. FAA FORM 8110-3 WAS ISSUED APPRSDR IXXA05RNG029SSupport Fitting · crackedDURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 339.723 WAS FOUND CRACKED (0.703"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-019 & EO ATI-070505. FAA FORM 8110-3 WAS ISSUED APPROVING TSDR IXXA05RNG028SSupport Fitting · crackedDURING ROUTINE "C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF 219.498 WAS FOUND CRACKED (0.177"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-018 & EO ATI-070405. FAA FORM 8110-3 WAS ISSUED APPROVINGSDR IXXA05RNG027SSupport Fitting · crackedDURING ROUTINE "C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF 97.6090 WAS FOUND CRACKED (0.2035"). REPAIR ACCOMPLISHED, STOP HOLES WERE DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-016 & EO ATI-070205. FAA FORM 8110-3 WAS ISSUED APPROVISDR IXXA05RNG026SSupport Fitting · crackedDURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF219.498 WAS FOUND CRACKED (1.599"). REPAIR ACCOMPLISHED, STOP HOLES WERE DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-017 & EO ATI-070305. FAA FORM 8110-3 WAS ISSUED APPROVINGSDR IXXA05RNG025SSupport Fitting · crackedDURING ROUTINE "0C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 97.6090 WAS FOUND CRACKED (0.2740"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-015 & EO ATI-070105. FAA FORM 8110-3 WAS ISSUED APPROVIN
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