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 IXXA000OGenerator · malfunctionedDURING CLIMB OUT, NR 4 GENERATOR BREAKER CYCLES OPEN AND CLOSED SEVERAL TIMES, GENERATOR WOULD NOT CARRY ITS OWN BUSS, VOLTS AND FREQUENCY OK. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. IN WORK.SDR IXXA110028OFan · failedDURING CRUISE, WITH THE RT RECIRCULATION FAN ON HAS A STRONG ELECTRICAL ODOR, WHEN TURNED OFF ODOR WENT AWAY. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX DEFERRED THE RT RECIRCULATION FAN IAW MEL 21-16-01. MX REPLACED RECIRCULATION FAN. OPS CHECK GOOD IAW MSDR IXXA110025SSkin · damagedDURING ROUTINE MAINTENANCE CHECK FOUND LEFT HAND WING NUMBER FOUR SPOILER PANEL DAMAGED. THE SPOILER WAS REPAIRED IAW DACO MAINTENANCE MANUAL 27-61-0.SDR IXXA110013OPressure Switch · crackedDURING CRUISE, THE CREW SHUTDOWN NR 1 ENGINE DUE TO LOSS OF OIL QTY. THEY LANDED WITHOUT FURTHER INCIDENT. MX INPECTED NR 1 ENGINE AND FOUND OIL DIFFERENTIAL PRESSURE SWITCH HOUSING CRACKED. THEY REPLACED OIL DIFFERENTIAL PRESSURE SWITCH. OPS CHECK GOOD IAWSDR IXXA11SMN016SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING NR 1 STUB WING FITTING INTERNAL PART CRACKED AT STA XW 454.000. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D AND SRM 51-3SDR IXXA11SMN015SSkin · crackedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND HORIZONTAL STABILIZER TRAILING EDGE UPPER SKIN CORRODED AT STATION XE 28.843. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. SDR IXXA11SMN014SAngle · corrodedDUIRNG ROUTINE C CHECK INSPECTION FOUND RIGHT VERTICAL STABILIZER TO FUSELAGE JOINT ANGLE CORRODED AT STA 1590. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED ANGLE, SPLICE, FILLER AND SSDR IXXA11SMN012SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND FUSELAGE EXTERNAL SKIN CORRODED AT SEVERAL POINTS AT STATION 1530.000 LONGERON 23-28LEFT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW SKINSDR IXXA11SMN013SSkin · corrodedDUIRNG ROUTINE C CHECK INSPECTION FOUND AFT FUSELAGE SKIN CRACKED AT STATION 1580.000 LONGERON 20RIGHT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, INTERNAL DOUBLER AND FILLER. CLEANED, TRSDR IXXA11SMN011SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING UPPER SKIN CORRODED AT STATION XRS 360.000 STRINGER 6. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUNSDR IXXA11SMN008SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS 385.250. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPSDR IXXA11SMN007SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS 347.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPSDR IXXA11SMN006SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CORRODED AT STATION XFS 341.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPSDR IXXA11SMN004SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING UPPER SKIN CORRODED AT STATION XRS 811.000 STRINGER 3 TO STRINGER 4. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRSDR IXXA11SMN002SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING UPPER SKIN CORRODED AT STATION XRS 763.000 STRINGER 2-4. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW SDR IXXA11SMN003SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING UPPER SKIN CORRODED AT STATION XRS 795.000 STRINGER 3-5. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUND. FABRICATED NEW SDR IXXA11SMN010SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING CTR L/E UPPER PANEL CORRODED AT STA XW 408.000. REMOVED CORRION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND RSDR IXXA11SMN009SDoubler · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING CTR L/E UPPER SURFACE DOUBLER CORRODED AT STA XFS 423.000 - XFS 400.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED DOUBLER. FABRICATED DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALSDR IXXA11SMN005SSkin · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING UPPER SKIN CRACKED AND CORRODED AT STA XRS -17.000 STR-9. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FSDR IXXA11SMN001SFastener · improper partDURING ROUTINE C-CHECK INSP, FOUND CHERRY MAX RIVETS USED IN REPAIR AT STATION ES 1360-1380. REMOVED FASTENERS FROM REPAIRED AREA. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, FINGER DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NESDR IXXA100059OCoupler · defectiveDURING CRUISE, NR1 HF RADIO WILL NOT CHANNELIZE AND HAD NO RECEPTION, NR 2 HF RADIO WOULD NOT WORK. THE CREW RETURNED TO DEPARTURE WITH OUT FURTHER INCIDENT. MX REPLACED NR1 ACCESSORY COUPLER AND 2 COAX CONNECTORS ON THE NR2 ACCESSORY COUPLER. OPS CHECK GOOD SDR IXXA100056OSwitch · shortedFIFTEEN MINUTES INTO FLIGHT, BOTH AIR CYCLE MACHINES ON THE RT ENVIRONMENTAL CONTROL CIRCUIT BREAKER AND THE BATTERY DIRECT PACS OVERTEMP TRIPPED. NO CONTROL OF THE LOAD CONTROL VALVE WAS AVAILABLE. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT.SDR IXXA100055OControl Valve · defectiveAFTER TAKEOFF, WHEN THE RT AIR CONDITIONING PACK WAS TURNED ON, THE RT ENVIRONMENTAL CONTROL CIRCUIT BREAKER AND THE RT ACM CONTROL CIRCUIT BREAKER OPENED AND WOULD NOT RESET. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT THE SYSSDR IXXA100054ODuct · disconnectedDURING CRUISE, NR 4 ENGINE GENERATOR UNPARALLEL LIGHT FOLLOWED BY GENERATOR DRIVE OIL LIGHT, MANIFOLD PRESSURE LIGHT ILLUMINATED WITH HIGH PRESSURE MANIFOLD AIR PRESSURE OVERTEMP LIGHT CAME ON, LOSS OF EGT INDICATION, ZERO FUEL FLOW AND ZERO EPR. THE CREW SHUTSDR IXXA100052SSkin · crackedDURING INSP, FOUND SKIN CRACKED AT STA 255 BETWEEN LONGERONS 33 AND 34 RT SIDE. INSTALLED INTERIM REPAIR IAW REA D853-60270.SDR IXXA100042OFan · odorDURING CRUISE, THE LT RECIRCULATION FAN WHEN TURNED ON EMITTED A ELETRICAL ODOR. THE CREW TURNED OFF THE LT RECIRCULATION FAN AND CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1. ACFT WAS RETSDR IXXA100041OFan · defectiveDURING CRUISE, THE RIGHT HAND RECIRCULATION FAN WHEN TURNED ON EMITTED A ELECTRICAL ODOR. THE CREW TURNED OFF RIGHT RECIRCULATION FAN AND SMELL WENT AWAY. THEY LANDED IN KWRI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT RECIRCULATION FAN. OPERATIONSDR 2010FA0000919Beam · cracked(SPUY) NR80 ACCESS DOOR - BULKHEAD BEAM CRACKED 4" AT STA 1606.000 L-19 ON RBL-2: TO LBL 2".SDR 2010FA0000918Skin · corroded(SPUY) FUSELAGE SKIN CORRODED AT STA FS 1558.000 L-10L.SDR 2010FA0000917Skin · cracked(SPUY) RT WING NR 4 STUB WING LWR SKIN CRACKED APPROX 1.5" (CORRECTING SOURCE DOCUMENT: INS-100R-5700).SDR 2010FA0000916Skin · dented(SPUY) LT WING OTBD FLAP UPPER SKIN DENTED (STA XF 238.00 - 304.000).SDR 2010FA0000915Skin · corroded(SPUY) RT WING OTBD L/E OUTER SECTION LWR SKIN CORRODED (XFS 710.000-760.000).SDR 2010FA0000914Longeron · corroded(SPUY) AFT ACCY COMPT - L-23R INTERIOR CORRODED (STA 1380.000 - 1400.000).SDR 2010FA0000913Skin · corroded(SPUY) RT WING UPPER SKIN CORRODED AT AROUND STA XRS 74.889.SDR 2010FA0000912Cargo Track · corroded(SPUY) MAIN CARGO COMPT NR 6 TRACK CORRODED AT STA 372.000.SDR 2010FA0000911Skin · corroded(SPUY) LT HORZ STAB - ELEVATOR LWR SKIN CORRODED AT STA XE 195.313.149.000 AND 132.750.SDR 2010FA0000910Angle · corroded(SPUY) EMPENAGE - VERTICAL STAB TO FUSELAGE LT JOINT ANGLE CORRODED AT STA 1640.382.SDR 2010FA0000909Frame · corroded(SPUY) LT MLG WW - FRAME FITTING CORRODED AT STA FS 879.000 L-24.SDR 2010FA0000907Structure · corroded(SPUY) RT WING INBD L/E OUTER SECTION UPPER PART CORRODED AT STA XW 257.000.SDR 2010FA0000906Skin · corroded(SPUY) EXTERNAL FUSELAGE - LOWER SKIN PANEL BUTT SPLICE CORRODED AT STA 1480.000 L-11L.SDR 2010FA0000905Skin · corroded(SPUY) LT WING - UPPER PANEL EXTERNAL SKIN CORRODED AT STA XRS 204.000 S-14.SDR 2010FA0000904Hook · cracked(SPUY) AFT PAX DOOR- HOLD OPEN HOOKS (02EA) CRACKED 1", APPROX AT STA FS 1440.000L TO L-15L.SDR IXXA10SMN073SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND EXTERNAL FUSELAGE SKIN CORRODED AT STA FS 1556.000 LONGERON 10 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, REPAIR DOUBLER, FILLER, ANSDR IXXA10SMN072SSkin · crackedDURING ROUTINE C-CHECK INSP FOUND RT WING NR 4 STUB WING LOWER SKIN CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLERS AND INTERNAL DOUBLERS. PERFSDR IXXA10SMN071SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND THE LT WING OTBD FLAP UPPER SKIN DENTED AT STA XF 238.000 - 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FSDR IXXA10SMN070SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD L/E OUTER SECTION LOWER SKIN CORRODED AT STA XFS 710.000 - 760.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSP. NO DISCREPANSDR IXXA10SMN069SLongeron · corrodedDURING ROUTINE C-CHECK INSP FOUND AFT ACCESSORY COMPARTMENT LONGERON L-23 RT INTERIOR CORRODED AT STA 1380-1400. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABERCATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW SDR IXXA10SMN068SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING UPPER SKIN CORRODED AT STA XRS 38.000 -112.000. REMOVED CORROSION. FOUND OUT OF LIMITS. PERFORMED NDT INSP. NO DISCREPANCY FOUND. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED NEW SKIN, REPAIR DOUBLESDR IXXA10SMN067SCargo Track · corrodedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 6 TRACK CORRODED AT STA 372.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW TRACK SEGMENT AND RESDR IXXA10SMN066SSkin · corrodedDURING ROUTINE C-CHECK INSP, FOUND LT HORIZ STABILIZER ELEVATOR LOWER SKIN CORRODED AT STA XE 195.313, 149.000, AND 132.750. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, FINGE
Back to Douglas DC-8-62F