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 IXXA05RNG035SSupport Fitting · crackedDURING ROUTINE "C" CHECK, CRACKS 2.023" AND 0.521" LONG WERE FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING STA XF 409.6675 OUTBOARD. FITTING WAS REPAIRED IAW EWO ATI 57-025 AND EO ATI-071105. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.SDR IXXA05RNG034SSupport Fitting · crackedDURING ROUTINE "C" CHECK, CRACK 0.5220" LONG WAS FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING LOCATED AROUND STATION XF 339.7232 OUTBOARD. LEFT WING OUTBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO ATI 57-024 AND EO ATI-071005. FAA FORM 8110-3 WAS ISSUESDR IXXA05RNG033SSupport Fitting · crackedDURING ROUTINE "C" CHECK, CRACK 0.2740" LONG WAS FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING LOCATED AROUND STATION XF 339.7232 INBOARD. LEFT WING INBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO-ATI-57-023 AND EO ATI-070905. FAA FORM 8110-3 WAS ISSUED ASDR IXXA05RNG032SSupport Fitting · crackedDURING ROUTINE "C" CHECK, CRACK 0.385" LONG WAS FOUND ON THE LEFT WING INBOARD FLAP AT FITTING LOCATED AROUND STATION XF 97-6090 INBOARD. LEFT WING OUTBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO ATI 57-022 AND EO ATI-070805. FAA FORM 8110-3 WAS ISSUED APSDR IXXA05RNG045SSkin · corrodedSKIN CORROSION DAMAGE FOUND ON RIGHT OUTER WING AT UPPER PLATING AROUND WING STATION XRS 727.00 AND STRINGER 3RH DURING A ROUTINE C CHECK INSPECTION. CORRODED AREA WAS BLENDED OUT, DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-035 AND EO ATI-071605. FASDR IXXA05RNG039SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION FOUND SKIN CORROSION DAMAGE ON THE RT OUTER WING AT INBD EXTENDED L/E AROUND STA XFS 603.750REMOVED CORROSION DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW EWO ATI 57-031 & EO ATI-071405. FAA FORM 8110-3 WAS ISSUED APPSDR IXXA05RNG042SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION OVER EXISTING REPAIR ON WING ON INNER OUTBOARD EXTENDED L/E SLAT STA XFS 207-XILD42. CORROSION ON RT WING LEADING EDGE UPPER SKIN WAS REMOVED AND REPAIR "DOUBLER' WAS INSTALLED IAW EWO ATI 57-034 AND SRM 57SDR IXXA05RNG038SSkin · corrodedDURING A "C" CHECK INSPECTION, FOUND SKIN CORROSION DAMAGE ON THE RIGHT OUTER WING AT THE INBOARD EXTENDED L/E STA XFS 653.750. RT WING L/E UPPER SKIN WAS REPAIRED IAW EWO ATI 57-030 AND EO ATI-071305. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.SDR IXXA05RNG037SSkin Panel · corrodedDURING INSPECTION CHECK CORROSION WAS FOUND ON PANEL AT WING OUTER INBOARD EXTENDED LEADING EDGE PLATING STA XFS 710.0, RT. CORROSION ON RT WING LEADING EDGE UPPER SKIN WAS REMOVED AND REPAIR "DOUBLER" WAS INSTALLED IAW EWO ATI 57-029 AND EO ATI-071505. FAA SDR IXXA05RNG036SSkin · corrodedDURING INSPECTION CHECK, SKIN CORROSION DAMAGE WAS FOUND ON THE LEFT INNER WING AT OUTBOARD EXTENDED LEADING EDGE SLOT AROUND L/E STATION XFS 207.00. REMOVED CORROSION AND ACCOMPLISHED REPAIR "DOUBLER" IAW EWO ATI 57-028 AND EO ATI-071205. FAA FORM 8110-3 WASDR IXXA05RNG043SAngle · corrodedCORROSION ON LT WHEEL WELL "DOG HOUSE" AREA LOWER SIDE STA 857.000, ANGLE WAS FOUND CORRODED. ANGLE WAS FABRICATED IAW DOUGLAS DRAWING 5644678 AND ASSEMBLED IAW DC8 SRM 53-7-2 FIGURE 4.SDR IXXA05RNG048SDoor · crackedDURING A ROUTINE C CHECK INSPECTION A CRACK WAS FOUND AT FUEL ACCESS DOO 506A LH.CORRECTIVE ACTION: ACCESS DOOR 506A LH WAS REPAIRED IAW EWO ATI-57-027 & SRM 57-2-1 FIGURE 43.SDR IXXA05RNG047SDoor · crackedDURING A ROUTINE C CHECK INSPECTION A CRACK WAS FOUND AT FUEL ACESS DOOR 506B LH. CORRECTIVE ACTION: ACCESS DOOR # 506B WAS REPAIRED IAW EWO ATI 57-026 & SRM 57-2-1 FIGURE 43.SDR IXXA05RNG046SSkin · misdrilledDURING A ROUTINE C CHECK INSPECTION FOUND A MISS DRILL HOLE ON PLATING STA XRS 795 LONGERON 3-RHD. REPAIR WAS MADE AND DOUBLER WAS INSTALLED IAW EWO ATI 57-036 & EO ATI-071705.FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.SDR IXXA0500079OConnector · looseDURING CRUISE, ACFT STARTING LOSING HYDRAULIC FLUID. CREW ACCOMPLISHED EMERGENCY PROCEDURES AND RETURNED ACFT. LANDED WITHOUT INCIDENT. MX FOUND LOOSE HYDRAULIC CONNECTOR RT SIDE OF NR 2 ENGINE. SECURED LINE. OPS CHECK GOOD PER ALL APPLICABLE MANUALS. ACFSDR IXXA0500061OTransmitter · brokenAFTER TAKEOFF FROM TAPA NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. CREW PERFORMED ENGINE SHUTDOWN CHECK LIST AND CREW RETURNED AIRCRAFT TO TAPA AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE DIFFERENTIAL TRANSMITTER PER ALL APSDR IXXA05000180Seal · missingUPON CLIMBOUT FROM KBWI EN ROUTE TO KWRI AFTER GEAR RETRACTION CREW NOTED AIR NOISE FROM UNDER COCKPIT FLOOR. AFTER GEAR RECYCLE, UNDER AIR LOAD NOISE DECREASED. CREW PROCEEDED TO KWRI AND MADE AN UNEVENTFUL LANDING. UPON INSPECTION MX NOTED NLG DOOR SEAL OSDR IXXA0500016OIndicator · inoperativeCREW REJECTED TAKEOFF FROM RJTY, DUE TO LOW EPR ON NR 1 ENGINE. ALL OTHER PARAMETERS WERE NORMAL. CREW RETURNED AIRCRAFT TO BLOCKS. MAINTENANCE TROUBLESHOT TO A BAD EPR INDICATOR IN THE NR 1 POSITION. THE INDICATOR WAS REMOVED AND REPLACED AND THE OPERATIOSDR ARWA20050105Actuator · failedSPLIT FLAPS INTO SJO, RETURN TO PTY. REMOVED AND REPLACED RT FLAPS INBOARD ACTUATING CYLINDER IN ACCORDANCE WITH DC8 MM 27-51-9. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH DC8 MM 27-50-0. NO ADJUSTMENT WAS NEEDED.SDR IXXA0500013ORegulator · failedDURING CRUISE FROM PKWA, TAKEOFF PLUS 45 MINS TURNED ON RECIR FAN AND HEARD LOUD BANG FROM AREA UNDER CAPTAIN SEAT, COULD NOT STOP CABIN FROM CLIMBING. GOT CONTROL OF CABIN AT ABOUT 15,000, ACFT ALTITUDE CABIN WAS AT 10,2000. TURNED BLEED OFF ON LEFT SIDE, PSDR IXXA0400120OTransceiver · brokenDURING FLIGHT FROM KSUU TO PHIK, HF NR 1 AND NR 2 RADIO REPORTED TO HAVE LOUD BACKGROUND SQUEAL AND IS UNREADABLE. CREW RETURNED AIRCRAFT TO KSUU AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 HF ACCESSORY COUPLER AND NR 2 HF R/T. OPERATSDR IXXA0400118OHose · wornDURING TAKEOFF FROM KMCC, AIRCRAFT LOST HYDRAULIC PRESSURE. HYDRAULIC QUANTITY DROPPED TO AUX LEVEL. CREW RETURNED AIRCRAFT TO KMCC AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. AS SOON AS INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTSDR IXXA0400117OComputer · weakDURING CRUISE FROM RJTY AIRCRAFT YAWS TO THE RIGHT WHEN YAW DAMPER IS TURNED ON. THE AUTOPILOT RUDDER IS OFF SCALE RIGHT INDICE AUTOPILOT RUDDER OFF SCALE RIGHT. MAINTENANCE TROUBLESHOT AUTOPILOT SYSTEM AND FOUND YAW AND ROLL CHANNEL COMPUTERS WEAK. REMOVEDSDR IXXA0400114OControl Box · burnedDURING LANDING, ON GEAR EXTENSION NO GREEN LIGHTS FOR GEAR DOWN AND LOCKED. C/B ON DC BUS 1 RESET NO HELP. VISUAL INDICATORS ON WING AND NOSE GEAR DOWN ALL CHECKED, GEAR DOWN AND LOCKED. CREW LANDED THE AIRCRAFT WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WSDR ARWA20041004Compressor · stalledREJECTED TAKEOFF AT 60 KTS DUE COMPRESSOR STALL NR 3 ENGINE. INSPECTED ENGINE INLET AND EXAUST, NO DEFECTS FOUND. ENGINE RUN UP C/W IN ACCORDANCE WITH MM 71-00. UNABLE TO DUPLICATE PROBLEM. OK FOR SERVICE.SDR IXXA0400113OWarning Light · false activationDURING CRUISE AT FL 370 LOWER CARGO COMPARTMENT FIRE WARNING ILLUMINATED. DISCHARGED BOTH FIRE EXTINGUISHERS. CREW RETURNED AND LANDED WITHOUT INCIDENT. UPON LANDING MAINTENANCE INSPECTED ALL LOWER CARGO COMPARTMENTS AND FOUND NO EVIDENCE OF FIRE. REF DMI NRSDR ARWA20041001Engine · vibrationNR 2 ENGINE HUMMING NOISE CHANGING IN PITCH DIRECTLY PROPORTIONAL TO VIBRATION IN THROTTLE, ALL OTHER PARAMETERS NORMAL, POWER RETARDED TO IDLE, HUMMING & VIBRATION STOPPED. REMOVED AND REPLACED NR 2 ENGINE PER JOB CARD DC8-UM-003. OPERATIONAL CHECK ON ENGINSDR IXXA060196SLongeron · corrodedDURING ROUTINE C CHECK, FOUND LONGERON 23 RIGHT CORRODED BETWEEN STATION Y1000 AND STATION Y1020. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060193SLongeron · corrodedDURING ROUTINE C CHECK, FOUND LONGERON 24 RIGHT CORRODED FROM STATION Y879.375 TO STATION Y402.000. REPAIRED LONGERON PER ALL APPLICABLE DATA.SDR IXXA060192SGuide · crackedDURING ROUTINE C CHECK, FOUND ROLLER GUIDE DOOR ANGLE CRACKED AT STATION Y500, LONGERON 29 RIGHT. REPLACED ROLLER GUIDE PER ALL APPLICABLE DATA.SDR IXXA060190SLongeron · corrodedDURING ROUTINE C CHECK, FOUND LONGERON 29 LEFT CORRODED FROM STATION Y510 TO STATION Y490. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060187SLongeron Splice · crackedDURING ROUTINE C CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON SPLICE CRACKED BETWEEN STATIONS 600, AND STATION 620 LONGERON 31 RIGHT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060191SFrame · corrodedDURING ROUTINE C CHECK, FOUND FRAME CORRODED AT STATION Y181, -X35, BETWEEN LONGERONS 21 RIGHT AND 32 RIGHT. REPLACED FRAME SECTION PER ALL APPLICABLE DATA.SDR IXXA060195SSkin · dentedDURING ROUTINE C CHECK, FOUND SKIN DENTED AT STATION Y1190 BETWEEN LONGERONS 31 LEFT AND 33 LEFT. REPAIRED SKIN PER ALL APPLICABLE DATA.SDR IXXA060194SDoubler · crackedDURING ROUTINE C CHECK, FOUND AIR START ACCESS DOOR CUTOUT DOUBLER CRACKED. REPLACED DOUBLER PER ALL APPLICABLE DATA.SDR IXXA060189SSkin · bulgedDURING ROUTINE C CHECK FOUND SKIN BULGING AT STATION 1582 BETWEEN LONGERONS 27 LEFT AND 28 LEFT. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060188SFillet · delaminatedDURING ROUTINE C CHECK, FOUND LEFT WING FILLET PANEL (NUMBER 1612) DELAMINATED. REPLACED PANEL PER ALL APPLICABLE DATA.SDR IXXA0400110OOutflow Valve · malfunctionedAFTER TAKEOFF LEFT PACK CONTROL VALVE WOULD NOT MAINTAIN CABIN ALTITUDE OF 10000 FEET WITH AIRCRAFT AT FL250 AND RIGHT PACK OFF. RIGHT PACK CONTROL VALVE WILL NOT MAINTAIN CABIN ALTITUDE OF 10000 FEET WITH AIRCRAFT AT FL 250 AND LEFT PACK OFF. CREW RETURNED SDR IXXA0400109OFlow Valve · failedAFTER TAKEOFF, LEFT PACK CONTROL VALVE WOULD NOT MAINTAIN CABIN ALTITUDE OF 1000 FEET WITH AIRCRAFT AT FL 250 AND RIGHT PACK OFF. CREW RETURNED TO PHIK AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED SECURTIY OF LEFT PACK/FLOW CONTROL SYSTEM, DUCTS AND COMSDR COOSDR040039Panel · corrodedLT WING, INNER WING T/E UPPER PANEL WITH HEAVY CORROSION.SDR ARWA20040901Engine · shutdownAT TOP OF DESCENT 08:23 ZULU, SHUT DOWN NR 2 ENGINE DUE TO OIL PRESS LIGHT ON AND OIL PRESS 30 PSI WITH ENGINE AT IDLE. WINDMILLING OIL PRESS 11 PSI N1 26.5 PERCENT. SECURED NR 2 ENGINE FOR FERRY FLIGHT IN ACCORDANCE WITH GMM 6-3-4 AND 6-3-5. COMPLETED RED SDR COOSDR040034Cover · damagedMAIN CARGO CABIN Y STA 119, Z0, -X 20 COVER, DAMAGED.SDR COOSDR040033Fitting · corrodedMAIN CARGO CABIN FROM Y STA 960 TO Y STA 980 FITTINGS, CORRODED.SDR COOSDR040032Floorbeam · crackedMAIN CARGO CABIN Y STA 360.0, FLOORBEAM UPPER CAP CRACKED AT +X 31.25.SDR COOSDR040030Fitting · corrodedRT AND LT WING TRAILING EDGE SUPPORT, CANOE FITTING OB/IB HOLES ID CORRODED AT STA XF=97.906, STA XF=219.498 AND STA XF=399.723.SDR COOSDR040019Floorbeam · crackedMAIN CARGO CABIN Y, STA 1380 FLOORBEAM UPPER CAP AFT FLANGE CRACKED.SDR COOSDR040022Skin · corrodedRT WING LEADING EDGE SLOT SKIN CORRODED, BETWEEN XW 329.25 AND XW 359.0.SDR COOSDR040021Fitting · corrodedLT HORIZONTAL STABILIZER ELEVATOR HINGE STA XE 140 SUPPORT HOLE CORRODED.SDR COOSDR040020Skin · corrodedFUSELAGE TAIL SECTION, FROM Y STA 1530 TO Y STA 1633 BETWEEN LONGERON 24L AND LONGERON 32L UPPER AND LOWER FUSELAGE SKIN CORRODED.SDR ARWA20040803Engine · leakingDURING CLIMBOUT OF MGGT NOTICED NR 4 ENGINE LOSS OF OIL QUANTITY, OIL PRESSURE AND LIGHT. PROCEEDED TO SHUTDOWN ENGINE ACCORDING TO CHECKLIST. REMOVED AND REPLACED ENGINE NR 4 S/N 669510, AND INSTALLED ENGINE S/N P671066 IN ACCORDANCE WITH ARROW AIR JOB CARD
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