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 IXXA10SMN029SHook · crackedDURING ROUTINE C-CHECK INSP FOUND FWD PASSENGER DOOR HOLD OPEN HOOK CRACKED AT STA FS 15.000 LONGERON 16 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED REPAIR DOUBLERS, FILSDR IXXA100021OValve · leakingDURING CRUISE, THE RT HYD PRESSURE WAS AT ZERO AND THE LT HYD WAS FLUCTUATING. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX FOUND RESERVOIR DEPRESSURIZTION VALVE LEAKING. REPLACED RESERVOIR DEPRESSURIZATION VALVE. OPS CHECK GOOD IAW UAL MM29-13-SDR IXXA100016OPump · crackedDURING CRUISE, THE AILERON AND RUDDER REVERSION LIGHT CAME ON, THE CREW ALSO NOTICED LOSS OF HYD PRESSURE AND QUANTITY. CREW ACCOMPLISHED PROCEDURES IAW QRH NR 27. DECLARED EMERGENCY LANDING WITHOUT FURTHER INCIDENT. MX FOUND CABIN AIR CHECK VALVE CLOGGED ANSDR IXXA100015OPlug · unsecureDURING CRUISE, THE CREW SHUTDOWN NR 1 ENG DUE TO LOSS OF OIL QUANTITY. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND THE STARTER FILLER PLUG OFF. THEY REINSTALLED FILLER PLUG AND LOCKED SERVICED ENGINE. OPS CHECK GOOD IAW AMM 80-10, AMM 12-10. SDR IXXA100014OBulb · burned outDURING APPROACH, NOSE GEAR LIGHT DID NOT ILLUMINATE UPON GEAR EXTENSION. CREW CYCLED NOSE GEAR AND VISUALLY CHECKED THE GEAR WAS DOWN AND LOCKED, THEY LANDED WITHOUT FURTHER INCIDENT. MX FOUND TOP LIGHT BULB BURNED OUT AND BOTTOM LIGHT WAS INTERMITTENT WHEN PSDR IXXA100013ORheostat · failedDURING DESCENT, THE OVERHEAD LIGHTS WENT OUT, FOLLOWED BY SMOKE AND FUMES THEN OVERHEAD SWITCH PANEL INTEGRAL LIGHTS CIRCUIT BREAKER POPPED AND SMOKE AND FUMES CLEARED. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX REPLACED OVERHEAD LIGHT PANEL RHEOSTAT, NO HELSDR IXXA100009OVbv · out of rigDURING POWER REDUCTION TO CRUISE POWER, NR 2 ENG COMPRESSOR STALLED. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX PERFORMED TROUBLESHOOTING FAULT 41 AND FOUND VBV'S OUT OF RIGGING. THEY RERIGGED THE VBV'S AND REPLACED CIT SENSOR. OPS CHECK GOOD IAW SDR IXXA100006SSkin · crackedLT WING LOWER SKIN CRACKED AT STATION 428.0. REPAIRED SKIN IAW CASTLE SKETCH 20100104028.SDR IXXA100004SStringer · crackedLT WING STRINGER 62 CRACKED. REPAIRED STRINGER IAW SRM 57-2-1 AND CASTLE SKETCH 20100104018.SDR IXXA100005SStringer · crackedLT WING STRINGER 63 CRACKED. REPAIRED STRINGER 63 IAW SRM 57-2-1 AND CASTLE SKETCH 20100104018.SDR IXXA100003SStringer · crackedRT WING FOUND STRINGER 62 CRACKED. REPAIRED STRINGER 62 IAW SRM 57-2-2.SDR IXXA100002SSkin · crackedRT WING LOWER SKIN CRACKED BETWEEN FWD AND AFT OF STRINGER 62. REPAIRED SKIN IAW SRM 57-2-1.SDR IXXA090074OAdi · defectiveDURING CLIMB OUT, CAPTAIN’S FLIGHT DIRECTOR INDICATOR READ’S DIFFERENT FROM THE F/O FLIGHT DIRECTOR INDICATOR, ALSO READ’S DIFFERENT IN FLIGHT LEVEL AND DESCENT. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED CAPTAIN’S FLIGHT DIRECTOR INSDR IXXA090070ORelief Valve · defectiveDURING CLIMB OUT, HYD PRESSURE DROPPED TO ZERO, AILERON AND MANUAL REVERSION LIGHTS ILLUMINATED. THE CREW ACCOMPLISHED ALL PROCEDURES IAW QRH, NO LOSS OF HYD QUANTITY. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED AND REPLACED DUAL FILTSDR IXXA090062OIndicator · defectiveDURING TAKEOFF, THE CAPT'S AIRSPEED INDICATOR HAD NO INDICATION. CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MX REPLACED CAPT'S AIRSPEED INDICATOR. OPS CHECK GOOD IAW UAL MM 30-30-04. ACFT WAS RETURNED TO SERVICE.SDR IXXA090060OConnector · dirtyDURING CRUISE, THE RT BLEED VALVE'S DO NOT SHUT OFF INDIVIDUALLY, BUT WHEN THEY ARE SHUT OFF PRESSURE DROP'S TO 10 PSI, MANIFOLD TEMP IS 10 TO 20 DEGREE CELSIUS, RT PACK SEEMS TO BE INOPERATIVE. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX CLESDR IXXA090057OFuel Filter · cloggedDURING CLIMB OUT NR 1 ENGINE FLAMED OUT. THE CREW ACCOMPLISHED FLAME OUT IN FLIGHT START CHECKLIST. THE NR 1 ENGINE STARTED ALL PARAMETER NORMAL. CREW LANDED WITHOUT FURTHER INCIDENT. MX PERFORMED TROUBLESHOOTING FAULT 51 AND REPLACED ENGINE FUEL FILTER. OPSDR 2009F00089Line · crackedDURING DESCENT HYD QUANITY AND PRESSURE LOST. UTILIZED EMERGENCY/ABNORMAL HYD CHECKLIST FOR APPROACH AND LANDING. FOUND LEAK AT NLG PIPE ASSY-CROSS TO GLAND STA 244 TO 240. REPLACED PIPE ASSY. ACFT RETURNED TO SERVICE.SDR U2RA2009F00088Line · crackedIN DESCENT HYDRAULIC QUANITY AND PRESSURE LOST. UTILIZED EMERGENCY/ABNORMAL HYDRAULIC CHECKLIST FOR APPROACH AND LANDING AT LBBG. FOUND LEAK AT NLG PIPE ASSY-CROSS TO GLAND STA 244 TO 240. REPLACED PIPE ASSY. AIRCRAFT RETURNED TO SERVICE.SDR IXXA090054ORmi · defectiveDURING CRUISE, THE COMPASS CARD ON NR 2 RADIO MAGNETIC INDICATOR FROZE IN POSITION. AFTER SEVERAL MINUTES THE COMPASS CARD STARTED MOVING BUT IS 180 DEGREE OFF OF AIRCRAFT HEADING. THE CREW RETURNED TO KLRD WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 RSDR IXXA090052OEngine · power lossDURING CRUISE, SHUT DOWN NR 2 ENGINE DUE TO POWER LOSS AND VIBRATION. CREW LANDED WITHOUT FUTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE. OPERATIONAL CHECK GOOD IAW ATI ERH 70.01. AIRCRAFT WAS RETURNED TO SERVICE.SDR IXXA090046OFire Loop · defectiveDURING CLIMB OUT, NR 4 FIRE WARNING HORN SOUNDED, THEN SILENCED AND SOUNDED AGAIN. THE CREW DISCHARGED BOTH BOTTLES AND SHUTDOWN NR 4 ENGINE. CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED CORE FIRE LOOP, CORE LOOP CONNECTORS AND BOTH FIRESDR IXXA090045ORadio · defectiveDURING CLIMB OUT, NR 2 VHF RADIO WILL NOT TRANSMIT FROM ANY POSITION. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX REPLACED FIRST OBSERVERS AUDIO SELECT PANEL AND VHF/FM COMM TRANSCEIVER. OPS CHECK GOOD IAW MM 23-20-1, AND 23-50-1. ACFT WASSDR IXXA090042OFuel Control · out of rigDURING TAKEOFF, NR 4 ENG WOULD NOT MAKE PWR. ONCE AIRBORNE HAD TO PUSH THROTTLE PAST OTHER THROTTLES NR 4 EGT WENT TO 907 DEGREE. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED NR 4 ENG AND FOUND VSV'S AND VBV OUT OF RIG. MX ACCOMPLISSDR IXXA090041STee Fitting · crackedDURING INSP IAW AD2007-21-18 AND SB DC8-53A081 FOUND RT AFT PRESSURE BULKHEAD TEE FITTING CRACKED. STOP DRILLED CRACK IAW SRM 53-2-5.SDR IXXA090031OTransducer · defectiveDURING CRUISE, AN UNCOMMANDED RUDDER KICK WITH NO MOVEMENT OF PEDALS. THE CREW DIVERTED TO KDFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE DEFERRED THE AUTOPILOT SYSTEM. MAINTENANCE IN KTOL REPLACED THE LINEAR POSITION TRANSDUCER. OPERATIONAL CHECK SDR IPXA09855884Door Frame · crackedINSPECTION TYPE:SV VALIDATE REPAIR NUMBER EFN 71819941030, ORIGINAL NO ROUTINE NUMBER 1966 28. LOCATION WEB AT TOP AFT END OF PAX DOOR FRAME HAS DOUBLE DRILLED HOLES AND IS CRACKED. REPAIR ACCOMPLISHED PER SRM 52-2-0 FIG 4 SHT 3, AND 52-2-0 FIG 2 SHT 4.SDR IPXA09855882Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 718-S2-01 RT ELEVATOR UPPER SKIN REPAIR AT STA XE 200 DOESN’T CORRELATE TO SRM. REPAIR ACCOMPLISHED PER TIMCO REO-G12769 REV A AND EO DC8-5520-33403-ASDR IPXA09855881Seat Track · brokenINSPECTION TYPE:SV SEAT TRACK AT STA 140 LBL 60 TOP FLANGE BROKEN OFF 3 EACH PLACES. REPAIR ACCOMPLISHED PER DC8 SRM 53-2-3 FIG 8A SHT 1.SDR IPXA09855880Skin · gougedINSPECTION TYPE:SV SURVEY SEQ 718-W3-25 REPAIR DOUBLER GOUGED LT WING I/B FLAP. REPAIR ACCOMPLISHED PER TIMCO REO-G12765 REV A AND EO DC8-5720-33327-ASDR IPXA09855812Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 718-F1-72 RT EXTERNAL FUSELAGE AT STA 62 L18R-L19R HAS A FL FLUSH REPAIR THAT DOES NOT CORRELATE TO A SRM. REPAIR ACCOMPLISHED PER DC8 SRM 53-02-1 REV 78 FIG 7 SHT 11.SDR IPXA09855966Skin · cutINSPECTION TYPE:SV SS NR 718-W4-16, WHEN REPAIR DOUBLER WAS REMOVED FOUND A CUT OUT IN LOWER SKIN OF RT CTR L/E OF THE WING, 12 INCHES LONG AND 3.75 WIDE, STA XFS 425. REPAIRED PER TIMCO REO-G12804 REV A, AND PER UPS EO NR DC8-5730-33497-A.SDR IXXA090029ORelay · defectiveUPON DESCENT INTO KTOL, THE CREW PUSHED IN ANTI FOGGING CIRCUIT BREAKER AND THE CREW DETECTED SMOKE, THE CREW PULLED THE CIRCUIT BREAKER AND SMOKE ODOR DIMINISHED. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RELAY. OPERATIONAL CHESDR IXXA090027OMechanism · dirtyAFTER TAKEOFF AND GEAR RETRACTION FROM KDFW, A SEVERE VIBRATION WAS FELT IN THE NOSE GEAR AREA. THE CREW RECYCLED THE LANDING GEAR AND THE CONDITION PERSISTED. THE CREW RETURNED TO KDFW AND LANDED WITHOUT INCIDENT. MAINTENANCE OBSERVED THE LEFT NOSE GEAR DOSDR IXXA090026SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 143 LONGERON 28.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND SDR IXXA090025SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 31 LONGERON 30.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND RSDR IXXA090024SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS287 LONGERON 35.5 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND RESDR IXXA090023SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS160 LONGERON 22 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPASDR IXXA090022SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1718 LONGERON 17.5. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIRSDR IXXA090021SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS1204 LONGERON 16.25. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAISDR IXXA090020SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS363 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARSDR IXXA090019SSkin · misrepairedDURING ROUTINE CPCP INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 349. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. NO CRACK’S OR CORROSION NOTED. FABRICATED NEW SKIN. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTASDR IPXA09855786Doubler · gougedINSPECTION TYPE:SV "A" PIT DOOR AT FS 300 UPPER INTERNAL EDGE HAS A GOUGED DOUBLER. REMOVED AND REPLACED DOUBLER PER DC8 SRM 52-2-0 FIG 4 SHT 3.SDR IPXA09855477Skin · misrepairedINSPECTION TYPE:SV SS 752-F1-06 STA -77 TO STA -2 L21L TO L24L SKIN SPLICE REPAIR DOES NOT CORRELATE WITH SRM. ACCOMPLISHED REPAIR IAW REO-G12621 REV B AND IPXA EO DC8-5320-32359-A.SDR IPXA09855476Doubler · crackedINSPECTION TYPE:SV SURVEY SEQUENCE 752-F1-59 DOUBLER AT L1 DOOR UPPER AFT CORNER IS CRACKED. ACCOMPLISHED REPAIR IAW DC8 SRM 55-02-00-0 PAGE 1 REV 78.SDR IPXA09855473Doubler · damagedINSPECTION TYPE:SV BS 1600 TO 1657 BETWEEN LONGERON 31R AND 32R AT INTERNAL DOUBLER AREAS HAS NUMEROUS OVERSIZED HOLES. REPAIR PER REO-G127714 REV E EO DC8-5320-33030-B.SDR IPXA09855453Structure · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 752-S4-03 RUDDER LT AT STA ZR 281.250 REPAIR DOES NOT MATCH CURRENT SRM. ACCOMPLISHED REPAIR IAW REO-G12616 REV B AND IPXA EO DC8-5520-32343B.SDR IPXA09855452Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 752-F1-19 FUSELAGE EXTERIOR SKIN SURFACE STA 1752 - 1774 L33L REPAIR CONFIGURATION DOES NOT CORRELATE TO A SRM REPAIR. ACCOMPLISHED REPAIR IAW REO-G12613 REV C AND IPXA EO DC8-5320-32917A.SDR IPXA09855451Structure · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 752-F1-72 REPAIR DOUBLER DOES NOT CORRELATE TO SRM REPAIR STA 115.5 TO 126.5. ACCOMPLISHED REPAIR IAW DC8 SRM 53-21-1 FIG 7 SHT 13 AND TR 53-203.SDR IPXA09855450Doubler · dentedINSPECTION TYPE:SV SURVEY SEQUENCE 752-S2-06 RT ELEVATOR UPPER SURFACE STA XE 200.2187 8 INTERNAL DOUBLER IS DENTED AND CRACKED. ACCOMPLISHED REPAIR IAW REO-G12604 REV C AND EO DC8-5520-32867A.
Back to Douglas DC-8-71F