Douglas DC-8-62
Service difficulty reports · 2,778
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 = 'DC862' 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 = 'DC862' 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 RRXA99202Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 35 LEFT AT STA 980, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-0 FIGURE 1F. (CORROSION DAMASDR IXXA9800061Retract Mech · malfunctionedAFTER TAKEOFF FROM MSP, EN ROUTE TO TOL, WHEN THE GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A LOUD NOISE AND SLIGHT VIBRATION COMING FROM THE NOSE WHEEL WELL AREA. THE CREW PERFORMED A GEAR UPLATCH CHECK WHICH PASSED, THEN CYCLED THE GEAR. THE VIBRATION COSDR RRXA99225Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 24 RIGHT AT STA 880, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (CORROSION DASDR RRXA99220Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1420 AND LONGERON 21 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0. (CORROSION DAMAGSDR RRXA99211Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 29 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGESDR RRXA980247Rt Unit · failedIR TURN-BACK, WX RADAR INOP, NO RETURNS (GND OR WX). REMOVED AND REPLACED RADAR RT, OPS CHECK GOOD ON GROUND.SDR IXXA9800060Ballast · failedEN ROUTE FROM KWA TO HIK, SMOKE EMANATED FROM THE FIRST OFFICERS RIGHT PEDESTAL CONSOLE. THE CREW EXTINGUISHED THE MAIN INSTRUMENT GLARESHIELD WHITE LIGHTING, THE SMOKE STOPPED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE FOUND THAT TSDR RRXA99216Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN DOUBLER AT STA 1570 TO STA 1578 AND BETWEEN LONGERONS 32 LEFT 33 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DCSDR RRXA99198Intercostal · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INTERCOSTAL AT STA 1385 AND LONGERON 26 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 53-2-0. (CORROSION DASDR RRXA99218Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT AND RIGHT WHEEL WELL PRESURE PANEL FINGER DOUBLER AT STA 920 TO STA 940 BETWEEN BL 66 LEFT TO BL 66 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED , TREATED AREA IAW DC-8 SRM 51-1-8. FABRSDR RRXA99204Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 26 LEFT BETWEEN STA 1440 TO STA 1480, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2. (CORROSDR ABXA9800601Switch · inoperativeON GEAR EXTENSION RT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE. RECYCLED GEAR, LIGHT ILLUMINATED. REPLACED RIGHT MAIN LANDING GEAR INDICATION SWITCH IAW DC8 MM 32-60-00.SDR RRXA99201Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME ATTACHMENT ANGLE AT STA 1080 AND LONGERON 35 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 53-1-0. (CORROSDR ARWA980609Brake · out of adjustKRDU - FLT 810 - AFTER TAKEOFF AND GEAR RETRACTION LOUD NOISE AND VIBRATION COMING FROM NOSE GEAR AREA. INSPECTED NOSE, WHEEL SKIN BRAKE, FOUND IN IDLE POSITION, REPOSITION PER DC-8 MM 32-41-3. (M)SDR ARWA980611Fuse · blownLIGHTING BOLT STRUCK NEAR AIRCRAFT ON GROUND. GROUND POWER WENT OFF AIRCRAFT. AFTER ONE HOUR (STORM) POWERED AIRCRAFT. SMOKE CAME UP BETWEEN CABIN PRESS CONTROL PANEL. LEFT DC INOPERATIVE. SEVERAL AIRCRAFT SYSTEMS INOPERATIVE. ALL FOUR FIRE DETECTION INOSDR RRXA98321Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 834 AND LONGERON 15 RIGHT.SDR RRXA98329Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 822 AND LONGERON 3 LEFT.SDR RRXA98328Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 440 AND LONGERON 16 RIGHT.SDR RRXA98327Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 420 BETWEEN LONGERONS 7 RIGHT TO 8 RIGHT.SDR RRXA98326Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 280 BETWEEN LONGERONS 13 RIGHT TO 14 RIGHT.SDR RRXA98325Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 270 BETWEEN LONGERONS 12 RIGHT TO 14 RIGHT.SDR RRXA98324Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 640 AND LONGERON 7 LEFT.SDR RRXA98323Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FRAME WITH MISDRILLED HOLE, AT STA 580 AND LONGERON 9 LEFT.SDR RRXA98322Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 560 BETWEEN LONGERONS 7 LEFT TO 8 LEFT.SDR RRXA99196Skin · corrodedDURING A MAINTENANCE VISI, FOUND CORROSION DAMAGE TO HORIZONTAL STABILIZER SKIN PANEL AT XE 181, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN PANEL IAW SK8550002. (CORROSION DAMAGE SDR RRXA99224Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT WHEEL WELL PRESURE PANEL AT STA 940 AND BETWEEN BL 63 LEFT TO BL 66 LEFT, DAMAGE BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW FAA APPROVED COTNEY DER ENGINEERING SKETCH E84-R55. (CORRSDR IXXA9800058Pumps · defectiveEN ROUTE, THE MAIN HYDRAULIC SYSTEM FAILED AND HYDRAULIC PRESSURE DROPPED TO ZERO. THE FLIGHT CONTROL MANUAL REVERSION LIGHTS ILLUMINATED CONFIRMING THE FAILURE. THE FLIGHT WAS DIVERTED TO DNA FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT ANSDR RRXA99194Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 759 AND BL 66, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN SDR RRXA98332Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 560 AND LONGERON 21 LEFT.SDR RRXA98331Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 540 AND LONGERON 21 LEFT.SDR RRXA98330Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 520 AND LONGERON 21 LEFT.SDR RRXA98320Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 759 BETWEEN LONGERONS 19 LEFT TO 20 LEFT.SDR RRXA98319Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 660 AND LONGERON 21 LEFT.SDR RRXA98318Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 640 AND LONGERON 21 LEFT.SDR RRXA98317Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 620 AND LONGERON 21 LEFT.SDR IXXA9800057Actuator · misriggedEN ROUTE, THE GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCH WARNING LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR WITH THE INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED TO SUU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEAR AND INDSDR RRXA98234Door · not latchedCARGO DOOR OPENED IN FLIGHT. DOOR SECURED PER DER INSTRUCTIONS. ACFT FERRIED TO MACON FOR REPAIRS.SDR ABXA9800520Ctc Duct · looseON TAKEOFF AND CLIMBOUT, GEAR RETRACTION HAD RUMBLING FROM NOSE GEAR AREA. RECYCLED GEAR, NOISE STOPPED ON DOWN CYCLE BUT RETURNED ON THE RETRACTION. AIR TURNBACK TO MHR. FOUND LOOSE NR 2 CTC DUCT. ADJUSTED AND SECURED DUCT. NO OTHER DEFECTS NOTED.SDR IXXA9800055Retract Mech · lack of lubeAFTER TAKEOFF WHEN THE GEAR WAS RETRACTED, THE FORWARD NOSE GEAR DOORS REMAINED OPEN. THE CREW CYCLED THE GEAR WITH NO HELP. THE FLIGHT CONTINUED TO TOL, MAKING AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE NOSE GEAR DOOR LATCH MECHANISMS, WITH NO DISCRESDR ARWA980602Fuel Contl Unit · failedAIR TURNBACK, AFTER DEPARTURE NR 3 ENGINE UNSPOOLED AND WHEN POWER LEVER WAS ADVANCED ENGINE WOULD NOT ACCELERATE. RETURNED TO TUS WITHOUT INCIDENT. INSPECTED ENGINE INLET, TAILPIPE, OIL AND FUEL FILTERS. NO DEFECTS NOTED. REMOVED AND REPLACED FCU, MAIN OISDR ARWA980508Swivel · leakingON LANDING ROLL, NOTICED HYD QUANTITY DECREASING DOWN TO STAND PIPE. REMOVED AND REPLACED AILERON TAB LOCK OUT CYLINDER SWIVEL GLAND IAW MM 27-11-7, OPERATION LEAK CHECK NORMAL.SDR RRXA98222Detector · malfunctionedAT FL 330, CREW EXPERIENCE BRIEF FIRE WARNING OF 2 RINGS AND LIGHT IN HANDLE ON NR 1 FIRE HANDLE. WARNING WAS OUT BEFORE RESET WAS PUSHED ON FIRE WARNING LIGHT. FIRE WARNING TEST WAS DONE TO ALL 4 ENGINES TO CONFIRM NO FIRE PRESENT. AT THE TIME NR 1 OIL TEMSDR RRXA98280Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT FITTING CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 940. REMOVED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-1-0, PAGE 1.SDR RRXA98279Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT FITTING CORRODED BEYOND DC-8 SRM LIMITS, AT STA 920. REMOVED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW 53-1-0, PAGE 1.SDR RRXA98278Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT FITTING CORRODED BEYOND DC-8 LIMITS, AT STA 960. REMOVED DAMAGED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-1-20D.SDR ARWA980506Mechanism · out of adjustIN FLT RETURN DUE TO LOUD RATTLING NOISE FROM NOSE WHEEL WELL AREA. UNABLE TO PRESSURIZE AIRCRAFT AUTO OR MANUALLY. ADJUSTED NOSE GEAR DOOR PER MM 32-10-0. RUN UP ENGINES PRESSURIZED OK IN MANUAL, AUTO INOP OPEN DMI ON AUTO PRESS. (M)SDR RRXA98282Skin · corrodedDURING A MAINTENANCE VISIT, FOUND HORIZONTAL STABILIZER LEADING EDGE RIGHT SIDE WITH EXFOLIATION CORROSION BEYOND DC-8 SRM LIMITS, AT STA XFS 178 TO STA XFS 200. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLSDR ABXA9800450Valve Assy · bypassingAFTER TAKEOFF AND GEAR RETRACTED, GEAR UNSAFE LIGHT WAS ILLUMINATED. RECYCLED GEAR WITH SAME RESULTS. PERFORMED GEAR UPLATCH CHECK AND LEFT AND RIGHT MAIN GEAR AND DOORS, 'NOT LATCHED' LIGHT WAS ILLUMINATED. REPLACED SYSTEM SELECTOR VALVE FOR BYPASSING. OPSDR ABXA9800449Valve · defectiveON CLIMB-OUT, GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AND THE RIGHT MAIN LANDING GEAR DOOR NOT LATCHED LIGHT WAS ILLUMINATED. RECYCLED GEAR WITH THE SAME RESULTS. REPLACED RIGHT MAIN LANDING GEAR DOOR CONTROL VALVE AND UPLATCH ASSY. INSSDR ABXA9800448Light · looseDURING CRUISE EMERGENCY LIGHT ON CAPTAIN'S SIDE WAS ARCING BETWEEN LIGHT ASSEMBLY BRACKET AND BULB. LIGHT ASSEMBLY WAS LOOSE IN MOUNT. TIGHTENED MOUNT NUT. OPS CHECKED GOOD IAW DC8 MM 33-00.
Back to Douglas DC-8-62