Douglas DC-8-71F
Service difficulty reports · 8,938
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 = 'DC871F' 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 = 'DC871F' 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 RRXA10764Stringer · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING STR.53 AT STA. 495 AND AFT HORZ. LEG, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O. #01-SDR RRXA10763Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGE DAMAGE TO LT. WING CANOE FITTING AT STA.340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 03/23/01SDR UPS01835646Fitting · crackedINSPECTION TYPE:C2,3 STA. 280 LOWER FLOORBEAM TO CUSP FITTING IS CRACKED AT LONG. 21R REMOVED AND REPLACED FITTING I.A.W. DWG. 9754022,AND SRM. 51-1-20D,& 51-1-21SDR UPS01835449Light · inoperativeINSPECTION TYPE:PREFLT, BOTH COCKPIT & ENTRY DOOR EMERGENCY LIGHTS INOP REMOVED & REPLACED EMERGENCY BATTERY & RELAY UNIT. OPS CHECK GOOD. OK FOR SERVICE.SDR RRXA010028Outflow Valve · failedON DESCENT, CABIN BEGAN TO CLIMB. WENT TO MAX RATE ON AUTO CONTROLLER AND MAX FLOW ON PACKS, WOULD NOT STOP CLIMB, CABIN COULD NOT BE CONTROLLED MANUALLY EITHER. ANY ATTEMPT TO MANUALLY CONTROL PRESSURE CAUSED CABIN TO CLIMB HIGHER, MANUAL LEVER COULD NOT BESDR RRXA010027Door · malfunctionedLOUD NOISE AND BUFFET FROM NOSE SECTION. RIGHT NOSE LANDING GEAR DOOR IN OPEN POSITION WHEN AIRCRAFT TAXIED IN. INSPECTED NOSE GEAR DOORS FOR CONDITION AND OPERATION NO DEFECTS NOTED. RE-SET POSITION, AIRCRAFT OK FOR FURTHER FLIGHT DC-8 M/M 32-20-00.SDR RRXA10767Skin · damagedDURING A MAINTENCE VISIT FOUND HOLE DAMAGE TO HORZ STAB RT. ELEVATOR AT STA. XE 228.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 02/SDR RRXA10765Door Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT. MLG BODY DOOR AT AFT O/B CORNER FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024 WITH APPROVED 8110-3 DATEDSDR RRXA10760Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LAV. FLOOR PANEL AT STA. 46-66, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 AND SDR RRXA10766Spar · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BOTTOM OF SPAR AT STA. 781 AND INSIDE L/H CENTER TANK THUR MID-SPAR ACCESS HOLE560E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FSDR RRXA10762Skin · damagedDURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO TAIL CONE SKIN AT STA.1902 AND RT 14 INCHES O/B AND 8 INCHES AFT OF ACCESS DOOR NR 62, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW PART AND INSTALLESDR RRXA10761Bushing · elongatedDURING A MAINTENANCE VISIT FOUND ELONGATED BUSHING DAMAGE TO #3 LT. FLAP 2ND FROM O/B VANE AT 2ND O/B VANE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED ISDR IXXA0100033Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE EXTERNAL PLATING AFT OF THE L-1 DOOR LOWER AFT CORNER.SDR RRXA10770Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGED TO A-PIT DOOR SEAL FRAME WORN/CRACKED OUT INCLUDING SKIN--LOC CENTER SECTION OF DOOR AT A-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSSDR RRXA10769Bracket · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO A-PIT DOOR SEAL FRAME AT A-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O 01-024 WITH APPROVED 8110-3 DATED 03/13/01.SDR RRXA10768Skin · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO A-PIT DOOR SEAL FRAME & DOOR SKIN AT THE A-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 SDR UPS01835349Tab · brokenINSPECTION TYPE:N/A, MAIN CABIN SLIDE COVER LOCKING TAB BROKEN OFF. REMOVED AND REPLACED LOCKING TAB BRACKET ON SLIDE CASE. THIS CLEARS M211497 PLACARD REMOVED.SDR RRXA10773Skin · tool damageDURING A MAINTENANCE VISIT FOUND TOOLING MARK DAMAGE TO LWR. WING SKIN UPPER SURFACE AT STA. XRS 507.625 AND STR. 54, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WSDR UPS01835291Slide · looseINSPECTION TYPE:IN, ESCAPE SLIDE NEEDS REPACKING. RESECURED SLIDE TO DOOR.SDR IXXA0100042SFrame · gougedDURING ROUTINE C CHEACK INSPECTION, A GOUGE WAS DETECTED ON FUSELAGE FRAME AT FUSELAGE STATION 1520, LONGERON 17 LEFT. REPAIR ACCOMPLISHED BLENDED GOUGE AND FABRICATED AND INSTALLED REPAIR DOUBLEERS IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINSDR IXXA0100041SIntercostal · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON INTERCOSTAL AT FUSELAGE STATION 8 LONGERON 35 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF INTERCOSTAL, FABRICATION AND INSTALLATION AN NEW INTERCOSTAL IN ACCORDANCE WITH DOUGLAS DRAWING 5615530 AND ENINEERSDR IXXA0100030Fitting · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED AT LONGERON END FITTING LOCATED AT FUSELAGE STATION 857, LONGERON 1. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND ISTALLATION NEW END FITTING IN ACCORDANCE WITH DACO DRAWING 4750521 ANDSDR IXXA0100029Cap · gougedDURING ROUTINE C CHECK INSPECTION, A GOUGED WAS DETECTED AT FUSELAGE STATION 1703, LONGERON 22 LEFT FUSELAGE FRAME CAP. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED CAP, FABRICATION AND INSTALLATION IN ACCORDANCE WITH DACO DRAWING 5612146 AND ENGINEERING ORDER 53-DCSDR IXXA0100028Flange · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON FRAME FLANGE AT FUSELAGE STATION 1380, LONGERON 35 LEFT. REPAIR ACCOMPLISH CORROSION REMOVAL, FABRICATION AND INSTALLATION A REPAIR ANGLE IN ACCORDANCE WITH DACO STRUCTURAL REPAIR MANUAL AND ENGINEERSDR IXXA0100027Pan · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LOWER C-PIT CARGO DOOR FORWARD DOOR PAN. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION A NEW DOOR PAN IN ACCORDANCE WITH DACO DRAWING 5704349 AND ENGINEERING ORDER SDR IXXA0100031Doubler · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT HORIZONTAL STABILIZER AFT SPAR WEB INTERNAL DOUBLER AT STATION XE 105. REPAIR ACCOMPLISHED REMOVAL OF DAMAGE AREA, FABRICATION AND INSTALLATION A NEW INTERNAL DOUBLER IN ACCORDANCE WITH DOUGLSDR IXXA0100021Pan · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LOWER C-PIT DOOR CORNER PAN. REPAIRED ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION A NEW PAN AND SPLICE PLATES IN ACCORDANCE WITH DAC DRAWINGS 5707387-501, 5074349-7 AND DACOSDR UPS01835290Seal · brokenINSPECTION TYPE:IN, FIRST AID KIT SEAL BROKEN. REMOVED AND REPLACED FIRST AID KIT.SDR UPS01835289Life Raft · missingINSPECTION TYPE:IN A/C NEEDS TWO SIX MAN LIFE RAFTS FOR OVERWATER FLIGHT. INSTALLED TWO SIX MAN LIFE RAFTS PART 600-107RU SER D112M & F41M.SDR RRXA10861Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BRACKET AT STA. 1140-1160 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20DSDR RRXA10744Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO OUTER SKIN L35L AT STA.705, DAMAGE EXCEEDED LIMITATIONS IAW DC-8SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSSDR UPS01835287Slide · unsecureINSPECTION TYPE:PFLT, DOOR SLIDE NEEDS TO BE RESECURED. REINSTALLED SLIDE.SDR IXXA0100045SStiffener · crackedDURING ROUTINE C CHECK INSPECTION, CRACKS WERE DETECTED ON THE FORWARD BULKHEAD LOWER STIFFENER AT FUSELAGE STATION -156. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTUAL REPAIRE MSDR UPS01835280Slide · out of positionINSPECTION TYPE:IN, ESCAPE SLIDE NEEDS TO BE PUT BACK IN SLIDE CASE. RE-SECURED ESCAPE SLIDE IN CASE.SDR RRXA10743Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H STRESS PANEL AT KEEL BEAM, AT STA 740, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4.SDR RRXA10742Fitting · gougedDURING A MAINTENANCE VISIT FOUND GOUGING DAMAGE TO RT. CANOE FITTING TOP FWD 3 INCHES AT RT. STA 340, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024 WITH APPROVED 811SDR RRXA10860Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FILLET ATTACH HOLES AT STA. 640-610 AND L31L TO L28L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED ISDR IXXA0100047SRib · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE LOWER RIB OUTBOARD ACCESS PANEL 518. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION A REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUALSDR IXXA0100044SRib · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE RIB BETWEEN ACCESS PANELS 519A AND 519B. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERINGSDR IXXA0100043SRib · gougedDURING ROUTINE C CHECK INSPECTION, A GOUGE WAS DETECTED ON THE LEFT WING LEADING EDGE RIB AT STATION XFS 445. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 57-DC8-17SDR RRXA10772Bulkhead · crackedDURING A MAINTENANCE INSPECTION FOUND CRACK DAMAGE TO C & D PIT R/H BULKHEAD AT C & D PIT, DAMAGE EXCEEDS LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITSDR RRXA10749Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN AT STA. 772-721 AND L35L-L36R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO#01-024 WITHSDR RRXA010016Fire Detector · activatedNR 2 ENG FIRE WARN SYS ACTIVATED INFLIGHT. ENG SHUTDOWN. OUTBOARD FIRE AGENT DISCHARGED. REMOVED AND REPLACED 3 FIRE DETECTOR ELEMENTS AND FIRE DETECTOR CNT''L UNIT. OP''S CHECKS GOOD IAW UAL MM 26-11-07.SDR IXXA0100048SPan · crackedDURING ROUTINE C CHECK INSPECTION, THE "A" PIT BASKET DOOR AFT CENTER SECTION DOOR PAN WAS FOUND CRACKED. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PAN, FABRICATION AN INSTALLATION A NEW SIDE PAN IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL, DACO DRAWING 5SDR UPS01835317Angle · crackedINSPECTION TYPE:B STA 958 CRACKED T-ANGLE ATTACHED TO KEEL BEAM. REMOVED AND REPLACED TEE IAW DRAWING 5616306.SDR IXXA0100035Intercostal · crackedDURING ROUTINE C CHECK INSPECTION, CORROSION AND CRACKS WERE DETECTED ON INTERCOSTALS BETWEEN FUSELAGE STATION 520 AND 560, LONGERON 33 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGE AREA, FABRICATION AND INSTALLATION INTERCOSTALS IN ACCORDANCE WITH DOUGLAS DRAWSDR UPS01835185Angle · crackedINSPECTION TYPE:PFLT, CRACKED T-ANGLE ATTACHED TO KEEL BEAM. *S/D* REMOVED AND REPLACED TEE.SDR UPS01835142Panel · failedINSPECTION TYPE:N/A, RTR-NR 4 GEN PWR FAIL ILLUM, LWR CGO FIRE LIGHT ILLUM ALL PANEL LIGHTS WENT OUT, SMOKE OF UNKNOWN ORIGIN FILLED COCKPIT AND CABIN. SHUTDOWN 1, 2 AND 4 ENGINES. *S/D* T/S AND FOUND NR 4 VRG FAILED PREVENTING NR 1 BTR CLOSURE. REMOVED ANSDR IXXA0100009Wire · brokenEN ROUTE FOR JFK TO TOL, THE GEAR DOOR WARNING LIGHT REMAINED ON DIM AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR AND THE WARNING LIGHT EXTINGUISHED. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFTSDR RRXA10748Skin · gougedDURING A MAINTENANCE VISIT FOUND GOUGED AND DENTED DAMAGE TO SKIN AT STA.1890 AND TAIL POST SUPPORT, DAMAGE EXCEEDED LIMITAIONS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-2-1 AND DC-8 SRM
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