Douglas DC-8-62

Service difficulty reports · 2,778

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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"

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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 DAMAJul 9, 1998 · N995CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR IXXA9800061Retract Mech · malfunctionedAFTER TAKEOFF FROM MSP, EN ROUTE TO TOL, WHEN THE GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A LOUD NOISE AND SLIGHT VIBRATION COMING FROM THE NOSE WHEEL WELL AREA.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 COJul 9, 1998 · N61CX · Doug DC862 · Landing Gear Door Retract SectionSDR 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 DAJul 8, 1998 · N995CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR 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 DAMAGJul 8, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 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 DAMAGEJul 7, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA980247Rt Unit · failedIR TURN-BACK, WX RADAR INOP, NO RETURNS (GND OR WX). REMOVED AND REPLACED RADAR RT, OPS CHECK GOOD ON GROUND.Jul 7, 1998 · N993CF · Doug DC862 · Weather Radar SystemSDR 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 TJul 7, 1998 · N728PL · Doug DC862 · Flight Compartment LightingSDR 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 DCJul 6, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 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 DAJul 6, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 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. FABRJul 3, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 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. (CORROJul 3, 1998 · N995CF · Doug DC862 · Fuselage Main, Longeron/StringerSDR 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.Jul 3, 1998 · N802AX · Doug DC862 · Landing Gear Position and WarningSDR 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. (CORROJul 2, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 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)Jun 29, 1998 · N810BN · Doug DC862 · Brake Anti-Skid SectionSDR 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 INOJun 28, 1998 · N791AL · Doug DC862 · AC Power Distribution SystemSDR RRXA98321Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 834 AND LONGERON 15 RIGHT.Jun 25, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98329Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 822 AND LONGERON 3 LEFT.Jun 24, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98328Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 440 AND LONGERON 16 RIGHT.Jun 24, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98327Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 420 BETWEEN LONGERONS 7 RIGHT TO 8 RIGHT.Jun 24, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98326Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 280 BETWEEN LONGERONS 13 RIGHT TO 14 RIGHT.Jun 24, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98325Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 270 BETWEEN LONGERONS 12 RIGHT TO 14 RIGHT.Jun 24, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98324Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 640 AND LONGERON 7 LEFT.Jun 24, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98323Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FRAME WITH MISDRILLED HOLE, AT STA 580 AND LONGERON 9 LEFT.Jun 24, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98322Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 560 BETWEEN LONGERONS 7 LEFT TO 8 LEFT.Jun 24, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR 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 Jun 23, 1998 · N995CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR 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. (CORRJun 21, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 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 ANJun 21, 1998 · N8974U · Doug DC862 · Hydraulic Pump (Electric/Engine), MainSDR 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 Jun 20, 1998 · N995CF · Doug DC862 · Fuselage Miscellaneous StructureSDR RRXA98332Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 560 AND LONGERON 21 LEFT.Jun 18, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98331Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 540 AND LONGERON 21 LEFT.Jun 18, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98330Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 520 AND LONGERON 21 LEFT.Jun 18, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98320Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 759 BETWEEN LONGERONS 19 LEFT TO 20 LEFT.Jun 18, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98319Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 660 AND LONGERON 21 LEFT.Jun 18, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98318Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 640 AND LONGERON 21 LEFT.Jun 18, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98317Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 620 AND LONGERON 21 LEFT.Jun 18, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR 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 INDJun 18, 1998 · N728PL · Doug DC862 · Landing Gear ActuatorSDR RRXA98234Door · not latchedCARGO DOOR OPENED IN FLIGHT. DOOR SECURED PER DER INSTRUCTIONS. ACFT FERRIED TO MACON FOR REPAIRS.Jun 13, 1998 · N995CF · Doug DC862 · Cargo/Baggage DoorsSDR 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.Jun 12, 1998 · N805AX · Doug DC862 · Cabin Compressor SystemSDR 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 DISCREJun 9, 1998 · N61CX · Doug DC862 · Landing Gear Door Retract SectionSDR 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 OIJun 6, 1998 · N1804 · Doug DC862 · Fuel Control/Turbine EnginesSDR 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.Jun 3, 1998 · N802BN · Doug DC862 · Aileron Tab Control SystemSDR 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 TEMMay 30, 1998 · N993CF · Doug DC862 · Fire DetectionSDR 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.May 21, 1998 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 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.May 21, 1998 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 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.May 20, 1998 · N990CF · Doug DC862 · Fuselage Miscellaneous StructureSDR 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)May 19, 1998 · N1804 · Doug DC862 · Landing Gear Door Retract SectionSDR 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 DOUBLMay 16, 1998 · N990CF · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR 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. OPMay 13, 1998 · N826AX · Doug DC862 · Landing Gear Retraction/Extension SystemSDR 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. INSMay 12, 1998 · N804AX · Doug DC862 · Landing Gear Door Retract SectionSDR 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.May 12, 1998 · N802AX · Doug DC862 · Emergency Lighting
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