Douglas DC-8-63F

Service difficulty reports · 1,883

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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 = 'DC863F'
  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.

SDR ABXA030228Longeron · corrodedLONGERON 32 LEFT OB CHANNEL AT STA. 370 WAS CORRODED. REMOVED CORRODED SECTION OF LONGERON, FABRICATED LONGERON AND SPLICES. INSTALLED IAW SRM 51-1-20D, 51-1-24, AND 53-2-2.Jul 20, 2002 · N816AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA030230Longeron · corrodedLONGERON 35 RIGHT INBOARD CHANNEL WAS CORRODED AT STA 340. CUT AND REMOVED DAMAGED SECTION, FABRICATED NEW SECTION AND REPAIR SPLICES. INSTALLED IAW DC-8 SRM 53-2-2 AND 51-1-20D.Jul 20, 2002 · N816AX · Doug DC863F · Fuselage Main, Longeron/StringerSDR ABXA030226Skin · corrodedREMOVE AND REPLACE FORWARD LOWER CARGO SKIN FROM F.S. 190 - 450 LONGERON 31 LEFT - 31 RIGHT. (COI NR 41207-001). REPLACED FORWARD LOWER CARGO SKIN IAW DC-8 SRM.Jul 19, 2002 · N816AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA030225Door Frame · corrodedAFT CARGO, BS 1220, FUSELAGE FRAME CORRODED JUST INBOARD OF SLIDING DOOR, LOWER AFT CUTOUT. REPLACED DOOR FRAME ZEE FITTING, FABRICATED REPAIR SPLICE ANGLES AND FILLERS. INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, AND 51-3-0.Jul 17, 2002 · N816AX · Doug DC863F · Fuselage Main, StructureSDR ABXA030218Structure · crackedFORWARD SERVICE DOOR UPPER FORWARD CORNER HAD A CRACK IN OUTER SKIN. CUT OUT CRACKED AREA, FABRICATED DOUBLER, TRIPLER, FILLER, AND INSTALLED EACH IAW SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D, 51-3-0 AND 51-1-14.Jul 16, 2002 · N816AX · Doug DC863F · Fuselage Main, Attach FittingsSDR ABXA030216Frame · corrodedAFT CARGO BS 1010, BETWEEN LONGERON 35 LEFT AND 35 RT, FUSELAGE FRAME CORRODED ON UPPER CAP, UPPER AND LOWER SURFACES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED (1 EA) FRAME CAP, (6 EA) GUSSETS, CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLE, FILLERJul 16, 2002 · N816AX · Doug DC863F · Fuselage Main, FrameSDR ABXA030224Shear Tie · corrodedAFT LOWER CARGO, SHEARTIE CORRODED AT STA. 1200, LONGERON 28 - 29 LEFT. REMOVED CORROSION, OUT OF LIMITS. REMOVED FITTING AND FABRICATED SPLICE, INSTALLED NEW FITTING IAW DC-8 SRM 51-1-8, 53-2-0, AND 51-1-20D.Jul 15, 2002 · N816AX · Doug DC863F · Fuselage Main, StructureSDR ABXA020058Warning System · malfunctionedGEAR UNSAFE LIGHT REMAINED ILLUMINATED ON RETRACTION. LEFT GEAR DOWN INDICATED NOT LATCHED. RECYCLED ONCE, NO HELP. RUNNING ABNORMAL TO UPLATCH CHECK POSITION LIGHT EXTINGUISHED.Jul 13, 2002 · N816AX · Doug DC863F · Landing Gear Position and WarningSDR ABXA020221Floorbeam · bentAFT CARGO, STATION 1320, RIGHT BUTT LINE 33, FLOORBEAM WAS BENT. REPAIRED AREA IAW ABX REA D853-43921MR AND DC-8 SRM 51-1-8.Jul 12, 2002 · N826AX · Doug DC863F · Fuselage Main, Floor BeamSDR ABXA020057Fire Detector · false indicationON ONE MILE FINAL, THE LOWER CARGO FIRE LIGHT ILLUMINATED. MX DISPLAY SHOWED "FWD A FIRE". EMERGENCY DECLARED INTO KILN BY CREW. LANDED AND CLEARED RUNWAY, TOWER AND CRASH CREW OBSERVED NO EVIDENCE OF FIRE. APPROXIMATELY 5 MINUTES AFTER, CARGO FIRE INDICATED LJul 10, 2002 · N815AX · Doug DC863F · Smoke DetectionSDR ARWA20020806Spar · crackedDURING C-CHECK, LEFT WING FRONT LOWER SPAR WITH CRACKS, STA XFS 526.7 (0.125 INCH) AND STA XFS 518 (1.25 INCH). ACCOMPLISHED REPAIR OF LEFT WING FRONT SPAR LOWER OUTBOARD CAP IAW RED SKETCH 02-07-11-001 SHEET 1 TO 6. BOEING MESSAGE ARW-MIA-02-00016H. THIS RJul 5, 2002 · N661AV · Doug DC863F · Wing SparSDR ARWA20020805Bulkhead · crackedDURING C-CHECK, AFT PRESSURE BULKHEAD UPPER LEFT SIDE WITH 0.125 INCH, 0.050 INCH, 0.375 INCH, & 0.580 INCH CRACKS, STA 1766. CUT OUT DAMAGE AREA AND FABRICATED FILLER, DOUBLER AND FINGER DOUBLER IAW DRAWING SRO8530007; INSTALLED PARTS IAW DRAWING SRO8530007.Jul 1, 2002 · N661AV · Doug DC863F · Fuselage Main, BulkheadSDR ARWA20020804Bulkhead · crackedDURING C-CHECK, AFT PRESSURE BULKHEAD UPPER RIGHT SIDE WITH 1.5 INCH CRACK STA 1766. CUT OUT DAMAGE AREA AND FABRICATED FILLER, FINGER DOUBLER AND DOUBLER IAW DRAWING SR08530007; INSTALLED PARTS IAW DRAWING SR08530007.Jul 1, 2002 · N661AV · Doug DC863F · Fuselage Main, BulkheadSDR ABXA020032Fitting · crackedRIGHT WHEEL WELL AREA, STATION 920, FITTING WAS CRACKED AT CENTER KEEL. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-21 AND 51-1-20.Jun 25, 2002 · N816AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ABXA020031Skin · corrodedSKIN CORROSION OUT OF LIMITS JUST AFT OF GYRO COMPARTMENT. INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0.Jun 25, 2002 · N816AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA020030Skin · corrodedCORROSION OUT OF LIMITS ON FUSELAGE SKIN, STATION 280, LONGERON 35 LEFT AND STATION 335, LONGERON 35 RIGHT. INSTALLED REPAIR DOUBLER IAW REA D853-44492.Jun 25, 2002 · N816AX · Doug DC863F · Fuselage Main, Plate/SkinSDR ABXA020003Pump · sheared#2 engine driven fuel pump was inop. Found spline shaft sheared on #2 engine driven fuel pump. Replaced pump IAW 73-10-2. Ops and leak checked good IAW 71-00.Jun 24, 2002 · N812AX · Doug DC863F · Engine Fuel PumpSDR ABXA010915Connector · looseAIR RETURN TO MIA DUE TO LOSS OF HYDRAULIC FLUID. AIRCRAFT DUMPED FUEL IN PREPARATION FOR RETURN TO MIA. FOUND CONNECTOR ON HYDRAULIC QUANTITY TRANSMITTER LOOSE. CLEANED AND RESECURED. SYSTEM OPS CHECKED GOOD. CHECKED FUEL DUMP SYSTEM AFTER USE, FOUND ALLJun 20, 2002 · N811AX · Doug DC863F · Hydraulic Pressure SensorSDR ARWA20020601B-Nut · looseABORTED TAKEOFF DUE TO NR 4 ENGINE WOULD NOT GO TO MAX POWER. FOUND COMPRESSOR BLEED ACTUATOR TO CONTROL CLOSED TUBE B-NUT LOOSE; TIGHTENED B-NUT IAW MM 75-30-2; PERFORMED FLAG CHECK ENGINE RUN UP OPS CHECKED NORMAL IAW MM 75-30-3 AND 71-00 MAX TAKEOFF POWER Jun 14, 2002 · N441J · Doug DC863F · Compressor Bleed ControlSDR ARWA20020509Mount · brokenDURING A-CHECK AT MIA THE FOLLOWING WAS FOUND, NR 4 ENGINE AFT MOUNT BROKEN. REPLACED FORWARD LT, FORWARD RT AND AFT ENGINE MOUNT ASSEMBLY IAW MM 71-20-2. AFT MOUNT SENT OUT FOR ANALYSIS.May 29, 2002 · N661AV · Doug DC863F · Engine Mount SectionSDR ABXA010889Battery Pack · dischargedDURING MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHTS DIM. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK IAW DC-8 MM 33-50-01.May 29, 2002 · N816AX · Doug DC863F · Emergency LightingSDR ABXA010888Battery Pack · dischargedEMERGENCY LIGHTS WERE COMING ON INTERMITTENTLY. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC-8 MM.May 28, 2002 · N816AX · Doug DC863F · Emergency LightingSDR ARWA20020508Engine · malfunctionedAFTER TAKEOFF, CLIMBING THROUGH 12 THOUSAND OIL QUANTITY CAME DOWN TO 2 GALLONS, FOLLOWED BY OIL PRESSURE LIGHT. PERFORMED ABNORMAL CHECK LIST NR 4 ENGINE OFF (SHUTDOWN). CAME BACK TO SAN SALVADOR WITHOUT ANY MORE ABNORMALITIES. PREPARED NR 4 ENGINE FOR FERMay 25, 2002 · N345JW · Doug DC863F · Engine (Turbine/Turboprop)SDR ABXA010900Nut · missingUPON FLAP EXTENSION FOR LANDING, SPLIT FLAPS WERE INDICATED. CONFIRMED BY ROLL TENDENCY. LEFT FLAP WAS APPROXIMATELY 6 DEGREES BEHIND RIGHT FLAP. RIGHT FLAP AT 35 DEGREES, LEFT FLAP AT 29 DEGREES. FOUND LEFT INBOARD FLAP ACTUATOR IDLER ARM TRACK MISSING NUMay 23, 2002 · N816AX · Doug DC863F · FastenersSDR ABXA010897Flap · out of rigON TAKEOFF WITH FLAPS SELECTED TO 18 DEG, THE INDICATOR INDICATED 15 DEG, THEN INCREASED TO 20 DEGREES. ON APPROACH, FLAP INDICATION WAS AS FOLLOWS, 12 SELECTED, 10 INDICATED - 23 SELECTED, 23 INDICATED - 35 SELECTED, 40 INDICATED. AIRCRAFT WAS FERRIED FROM May 23, 2002 · N811AX · Doug DC863F · Trailing Edge Flap Control SystemSDR ABXA010911Actuator · brokenRED GEAR UNSAFE LIGHT ILLUMINATED IN CRUISE FLIGHT. LANDING GEAR AND DOOR LATCHING SYSTEM ILLUMINATED IN LEFT MAIN GEAR POSITION. ALTERNATE METHOD USED TO EXTINGUISH THE GEAR UNSAFE INDICATION. FOUND THE LEFT MAIN LANDING GEAR ACTUATOR ATTACHING PIN BROKEN.May 18, 2002 · N828AX · Doug DC863F · Landing Gear ActuatorSDR ARWA20020401Cylinder · leakingAFTER LANDING, LOSS OF HYD PRESSURE WITH LOW PRESSURE LIGHT, AILERON & RUDDER POWER LIGHTS ON, QUANTITY NORMAL. ACFT WAS STOPPED ON THE TAXIWAY & TOWED TO THE RAMP. REMOVED AND REPLACED RIGHT HAND MLG BOGIE TRIM CYLINDER ASSY IAW MM 32-33-1. LEAK CHECK ACCOApr 2, 2002 · N661AV · Doug DC863F · Landing Gear Retraction/Extension SystemSDR U2RB040202Floorbeam · corrodedDURING CPCP 18 MONTH INSPECTION, AFT ACCESSORY COMPARTMENT INTERIOR. DETECTED LEVEL 2 CORROSION OF UPPER TEE OF FORWARD FLANGE OF FLOORBEAM 11.5 INCHES INBOARD OF RIGHT FUSELAGE CUSP LINE 1.75 INCHES LONG.Apr 2, 2002 · N865F · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA20020310Hydraulic Line · leakingWHEN READY TO TAXI, HYDRAULIC QUANTITY GAUGE INDICATED LOSS OF FLUID, HYDRAULIC PRESSURE GAUGE INDICATED LOSS OF PRESS. ACCOMPLISHED APPROPRIATE CHECKLIST, RETURNED TO RAMP. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE FROM NR 3 ENGINE HYDRAULIC PUMP, OPS CHMar 21, 2002 · N441J · Doug DC863F · Hydraulic System, MainSDR ABXA010781Bushing · defectiveUNABLE TO RETRACT GEAR ON FIRST ATTEMPT. GROUND COOLING AND BLOWAWAY JET RETRACTED NORMALLY. REMOVED THE RIGHT MAIN LANDING GEAR, REPLACED GEAR BUSHING IAW DC-8 MM. REINSTALLED RIGHT MAIN LANDING GEAR. SWING AND OPS CHECKED GOOD. REPLACED BLOW AWAY JET SWMar 18, 2002 · N815AX · Doug DC863F · Landing Gear Retraction/Extension SystemSDR IXXA0200009OConnector · contaminatedAFTER TAKEOFF FROM PDX, THE TAKEOFF WARNING HORN SOUNDED WHEN THE LANDING GEAR AND FLAPS WERE RETRACTED AND COULD NOT BE SILENCED. THE FLIGHT RETURNED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE FLAP LIMIT SWITCH CMar 7, 2002 · N867BX · Doug DC863F · Trailing Edge Flap Control SystemSDR ARWA20020305Engine · malfunctionedWITH THROTTLE SET FOR MAX TAKEOFF NR 4 ENGINE GOT UP TO 1.70 EPR, N1-100, N2-100, AND THROTTLE FULL FORWARD. TAKEOFF ABORTED AND RETURNED TO THE RAMP.Mar 6, 2002 · N441J · Doug DC863F · Engine (Turbine/Turboprop)SDR IXXA0200008OStriker · wornENROUTE FROM BFI TO PDX, THE LANDING GEAR NOT LATCH LIGHT ILLUMINATED DURING THE GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECMar 6, 2002 · N867BX · Doug DC863F · Landing Gear Position and WarningSDR ARWA20020303Fuse · blownIN CRUISE NR 1 MAIN & ALT TANK FUEL BOOST PUMPS POPPED C/B'S, WITH ASSOCIATED INDICATION OF NR 1 & 2 CSD TEMP INOP, NR 1 & 2 ENGINE OIL TEMP AND QTY INOP, GEAR LIGHTS INOP AND SPOILER PRESS ZERO, WITH OVERRIDE POSITION INOP. ALL OTHER C/B'S CHECK NORMAL AND NMar 6, 2002 · N441J · Doug DC863F · Drag Control SystemSDR IXXA0200007OWarning Light · illuminatedENROUTE FROM TOL TO LAX, AFTER THE LANDING GEAR WAS RETRACTED THE DOOR UNSAFE LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR, PERFORMED A SUCCESSFUL GEAR UP LATCH CHECK, BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TMar 5, 2002 · N867BX · Doug DC863F · Landing Gear Position and WarningSDR ABXA010761Spring · defectiveDURING TAXI, ELEVATOR FELT LIKE IT WAS BINDING AND COULD NOT GET A GOOD TEST. DID BLOCK TURNBACK. REPLACED THE ELEVATOR LOAD SPRING ASSEMBLY IAW DC-8 MM 27-30-04. OPS CHECKED GOOD.Feb 19, 2002 · N816AX · Doug DC863F · Elevator Control SystemSDR ABXA010721Battery · dischargedEMERGENCY EXIT LIGHTS INTERMITTENTLY INOPERATIVE WHEN POWER WAS REMOVED FROM AIRCRAFT. REPLACED EMERGENCY LIGHT BATTERY RACK ASSEMBLY. OPS CHECKED GOOD IAW DC-8 AMM 33-50-01-2-0001.Feb 15, 2002 · N816AX · Doug DC863F · Emergency LightingSDR ABXA010705Bolt · brokenON APPROACH TO MIA, LOWERED FLAPS TO 23 DEGREES AT APPROXIMATELY 15 - 20 DEGREES, FLAPS HUNG UP ON INDICATION AND DISPLAYED A SLIGHT ASYMMETRY AND POPPED LOOSE WITH A BANGING EFFECT. TRAVEL OKAY TO 35 DEGREES. REPLACED BROKEN BOLT AND BEARING SECURING ROLLERFeb 10, 2002 · N816AX · Doug DC863F · Trailing Edge FlapsSDR ABXA010707Fuel Control · failedDURING DESCENT, THE NR 4 ENGINE FAILED TO ACCELERATE. EPR, EGT, RPM AND F/F DECAYED. OIL PRESSURE WAS NORMAL (WINDMILLING). PERFORMED CHECKLIST - NO HELP. DURING LEVEL OFF WITH INCREASED AIRSPEED - NEGATIVE RELIGHT. PERFORMED ENGINE SHUTDOWN ACTIONS CHECKFeb 8, 2002 · N811AX · Doug DC863F · Fuel Control/Turbine EnginesSDR ARWA20020201SwitchLOG PAGE 107381. DISCREPANCY: TAKE OFF WARNING HORN SOUNDS WHEN POWER ADVANCED WITH FLAP SETTINGS 12, 18, AND 23 DEGREES FOR TAKE OFF. CORRECTIVE ACTION: REMOVED AND REPLACED RIGHT HAND SPOILER RELAY SWITCH IAW MM 27-63-1 OPERATIONAL CHECK NORMAL IAW MM 27-63-Feb 5, 2002 · N441J · Doug DC863F · Drag Control SystemSDR ARWA20020115Pressure SwitchLOG PAGE 109685. DISCREPANCY: AFTER TAKE OFF ENGINE #3 OIL PRESS LIGHT CAME ON, OIL PRESS 50 Psi, PRESS 40 Psi WITH POWER LEVER @ IDLE, OIL TEMP INCREASED TO 128 C ENGINE SHUT DOWN IAW AOM ABNORMAL PROCEDURE. ENGINE SHUT DOWN AT 2352Z. AIRCRAFT RETURNED TO KMIJan 29, 2002 · N441J · Doug DC863F · Engine Oil PressureSDR ABXA010694Link · brokenRIGHT INBOARD FLAP DRIVE LINK BROKEN. REPLACED RIGHT STATION 98 FLAP DRIVE LINK ASSEMBLY IAW DC8 MM 27-51-04-3-0001. OPS CHECKED GOOD.Jan 26, 2002 · N826AX · Doug DC863F · Trailing Edge Flap Control SystemSDR ABXA010859Attach Angle · crackedLEFT MAIN WHEEL WELL INSIDE KEEL BEAM, STATION 910, VERTICAL ATTACH ANGLE, LOWER END CRACKED WITH STOP DRILL HOLE. INSTALLED REPAIR ANGLES IAW REA D853-41947.Jan 21, 2002 · N819AX · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA20020114Switch · failedLINE UP FOR TAKEOFF ADVANCED POWER AND GOT CONFIGURATION TAKEOFF WARNING HORN. AIRCRAFT RETURNED TO BLOCKS. REMOVED AND REPLACED RT SPOILER SWITCH IAW MM 27-63-01, OPS CHECK NORMAL IAW MM 27-63-00. AIRCRAFT RETURNED TO SERVICE.Jan 20, 2002 · N441J · Doug DC863F · Drag Control SystemSDR ARWA20020113SensorLOG PAGE 107160. DISCREPANCY: #4 ENGINE OIL TEMP @ 150 @ 15 MINUTES ENGINE SHUT DOWN AS PER AOM. AIRCRAFT RETURNED TO KMIA AND LANDED OVERWEIGHT UNEVENTFUL. CORRECTIVE ACTION: TROUBLESHOOTING INDICATED OPENED RESISTANCE AT TEMP BULB. REMOVED AND REPLACED #4 ENJan 20, 2002 · N661AV · Doug DC863F · Engine Oil TemperatureSDR ARWA20020112Wire · damagedDURING CLIMB NR 2 ENGINE OIL TEMP INDICATION READ 150. SWAPPED GAUGES FOR TROUBLESHOOTING, NO HELP. AFTER RETARDING NR 2 POWER LEVER, OIL TEMPERATURE DECREASED, ADVANCE POWER LEVER, TEMPERATURE INCREASED. NEVER EXCEEDED THE 15 MINUTES LIMIT. AIRCRAFT RETURJan 18, 2002 · N661AV · Doug DC863F · Engine Oil System WiringSDR ABXA010862Door Frame · crackedLEFT FORWARD ENTRY DOOR MADE A BINDING NOISE WHEN MOVED FROM FULL OPEN POSITION. FOUND SNUBBER SUPPORT WEB CRACKED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED NEW SPLICE AT BOTH ENDS IAW REA D853-41451MR.Jan 15, 2002 · N819AX · Doug DC863F · Fuselage Main, StructureSDR ABXA010858Skin · crackedRIGHT WING LEADING EDGE SKIN HAD CRACK WITH STOP HOLES AT XLS 710, OUTBOARD SIDE OF NR 4 ENGINE. INSTALLED DOUBLER REPAIR IAW DC-8 SRM 57-2-1.Jan 14, 2002 · N819AX · Doug DC863F · Wing, Plate/SkinSDR ABXA010659Cap · looseLOSS ALL ENGINE OIL QUANTITY FROM NR 1 ENGINE OIL SYSTEM INFLIGHT. PRECAUTIONARY SHUTDOWN, CSD DISCONNECTED. ENGINE MAINTAINED OIL PRESSURE GREATER THAN 5 PSI AFTER SHUTDOWN. FOUND CSD INPUT SPLINE OVER FILL STANDPIPE CAP LOOSE. SECURED CAP AND PERFORMED ENJan 4, 2002 · N816AX · Doug DC863F · Alternator-Generator DriveSDR ABXA010860Skin · crackedLEFT WING LEADING EDGE LOWER SKIN, JUST OUTBOARD OF THE NR 1 PYLON HAD 4 EACH CRACKS AT STATION XRS 525. INSTALLED DOUBLER REPAIR AND REPAIRED AREA IAW DC-8 SRM 57-2-1 AND 51-1-8.Jan 3, 2002 · N819AX · Doug DC863F · Wing, Plate/Skin
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