Douglas DC-8-61F

Service difficulty reports · 82

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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 = 'DC861F'
  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 ABXA9800666Fitting · crackedLONGERON 31L SPLICE FITTING CRACKED AT STATION 1040-1060. REPAIRED IAW DC8 SRM 51-1-20D.Jun 13, 1998 · N849AX · Doug DC861F · Fuselage Miscellaneous StructureSDR TC8A98030Line · failedDURING APPROACH, EXPERIENCED LOSS OF HYDRAULIC FLUID AND PRESSURE. COMPLIED WITH EMERGENCY CHECKLIST. FOUND AND REPLACED 2 PRESSURE HARD LINES FROM ENGINE HYDRAULIC PUMP THAT WERE SPLIT W/FLEX LINES. HYDRAULIC CASE DRAIN FILTERS FOUND OK. CHECKED ON RUN IAMay 21, 1998 · N184SK · Doug DC861F · Hydraulic System, MainSDR TC8A98020Cover Plate · loosePRECAUTIONARY SHUTDOWN NR 3 ENGINE ON SHORT FINAL. OIL PRESSURE STARTED FLUCTUATING BETWEEN 45 PSI AND YELLOW ARC. SHUT IT DOWN WHEN ITWENT BELOW THE RED LINE. REMOVED, INSPECTED AND REPLACED OIL FILTER PER MM 79-20-7, NO METAL FOUND IN FILTER, LEAK CHECKS Apr 30, 1998 · N184SK · Doug DC861F · Turbine Engine Accessory DriveSDR ABXA9800104Skin · corrodedLEFT WING LEADING EDGE SKIN CORRODED AT STA XFS 710.5. REPAIRED IAW SRM 57-2-1.Feb 8, 1998 · N846AX · Doug DC861F · Wing, Plate/SkinSDR ABXA9800103Slot Vane · corrodedLEFT OUTBOARD SLOT VANE AT INBOARD END ON LEADING EDGE CORRODED BEYOND LIMITS. REPAIRED IAW SRM 57-3-10 FIG 20.Feb 8, 1998 · N846AX · Doug DC861F · Trailing Edge FlapsSDR ABXA9800102Tie Fitting · crackedINTERCOSTAL TIE FITTING CRACKED AT STA 1138 ABOVE LONGERON 33R. REPAIRED IAW DACO DWG 4758514 AND SRM 51-18.Feb 8, 1998 · N846AX · Doug DC861F · Fuselage Miscellaneous StructureSDR ABXA9800101Angle · crackedUPPER L-ANGLE CRACKED ON LEFT HORIZONAL STABILIZER OUTBOARD TIP. FABRICATED AND INSTALLED REPAIR PER REA D855-2265-MR.Feb 8, 1998 · N846AX · Doug DC861F · Horizontal Stabilizer StructureSDR TC8A98005Switch · failedTRIP NR 1259, SLOT DISAGREEMENT LIGHT STAYED ON ON TAXI-OUT, RETURNED TO RAMP. ENTERED ON DMI 8052 CAT C, REMOVED AND REPLACED INBOARD RT SWITCH, OPS CHECKED NORMAL IAW M/M 27-52-3, CLEARED DMI8052.Jan 29, 1998 · N184SK · Doug DC861F · Leading Edge Slat Position Indicating SystemSDR TC8A98002Compressor · stalledNR 2 ENGINE COMPRESSOR STALLED ON TAKEOFF, ABORTED TAKEOFF. INSPECTED ENGINE IAW 72-00, PERFORM GROUND RUN IAW TCA MIP VOL 2, OPS CHECK NORMAL, NO STALLS NOTED.Jan 21, 1998 · N184SK · Doug DC861F · Turbine Engine Compressor SectionSDR ABXA9800145Doubler · corrodedINTERNAL FINGER DOUBLER CORRODED AT STATION 450 BETWEEN LONGERONS 31L TO 31R. REPAIRED IAW DC8 SRM 51-1-8.Jan 5, 1998 · N846AX · Doug DC861F · Fuselage Miscellaneous StructureSDR CKSA97480Uplatch Mech · lack of lubeNOSE GEAR EXTENDED ON UPLATCH CHECK, TWICE, THEN STAYED UP. CHECKED UPLATCH MECHANISM FOR CONDITION/SECURITY FOUND OK. GREASED UPLOCK UNIT AND ROLLER JACKED AIRCRAFT NOSE AND ACCOMPLISHED NOSE GEAR FUNCTIONAL CHECK, UPLOCK CHECK SATISFACTORY.Aug 21, 1997 · N813CK · Doug DC861F · Landing Gear Retraction/Extension SystemSDR TC8A97040Oil Line · looseDUE TO LOW OIL QUANTITY AND PRESSURE FLUCTUATION SHUT DOWN NR 1 ENGINE IN FLIGHT AT 15:45PER ABNORMAL CHECKLIST PAGE 3-122 (HALF GALLON AND BELOW 40 PSI). DUE TO LOW OIL QUANTITY AND PRESSURE FOUND RETURN LINE TO OIL TANK LOOSE. RESECURED LINE, FILLED OIL TAAug 5, 1997 · N184SK · Doug DC861F · Turbine Engine Oil SystemSDR TC8A97033Hyd Press Trans · failedDURING THE TAXI CHECKLIST UNABLE TO VERIFY SPOILER DROP / RISE, NO DEFLECTION ON GAUGE. REMOVED AND REPLACED SPOILER PRESSURE TRANSMITTER IAW MM 29-30-3, OPS AND LEAK CHECKS OK.Jul 11, 1997 · N184SK · Doug DC861F · Hydraulic Pressure SensorSDR TC8A97024Starter · failedNR 4 ENGINE STARTER FAILED ON STARTUP. REMOVED AND REPLACED PNEUMATIC STARTER, ENGINE OPS CHECKS OK IAW MM 80-10-1.May 9, 1997 · N184SK · Doug DC861F · Engine StarterSDR 97ZZZX2006Bulkhead Web · crackedDURING 'C' CK INSPECTION ACCOMPLISHED VISUAL AND DYE PENETRANT INSPECTION OF THE AFT PRESS BULKHEAD WEB IAW SB 53-73 REV 1. FOUND A CRACK AT RT FWD SIDE OF THE APB WEB AT I/B SIDE OF VERTICAL STIFFENER ABOVE FASTENER ROW. ACCOMPLISHED TERMINATING ACTION BY RApr 25, 1997 · N27UA · Doug DC861F · Fuselage Main, BulkheadSDR TC8A97018Actuator · leakingTNCC-KMIA, FLT 00024. DISCREP: UNSATISFACTORY UPLATCH CHECK OUT OF TNCC. ABNORMAL CH 3, P.111, CONTINUE FLIGHT NORMALLY. REMOVED AND REPLACED LT MAIN GEAR DOOR LEAKING ACTUATOR IAW MM 32-32-7, LEAK AND OPS CHECKS OK. PERFORMED LANDING GEAR RETRACTION/EXTEMar 13, 1997 · N184SK · Doug DC861F · Landing Gear Door ActuatorSDR TC8A97014Engine · out of trimNR 2 ENGINE WOULD NOT GO TO TAKEOFF POWER. RETURNED TO RAMP. TRIMMED NR 2 ENGINE, SYSTEM OPS GOOD ON RUN-UP IAW MM 76-10.Feb 9, 1997 · N184SK · Doug DC861F · Fuel Controlling SystemSDR TC8A97013Engine · out of trimNR 1 ENGINE WOULD NOT GO TO TAKEOFF POWER, RETURNED TO RAMP. TRIMMED NR 1 ENGINE, SYSTEM OPS GOOD ON RUN-UP IAW MM 76-10.Feb 9, 1997 · N184SK · Doug DC861F · Fuel Controlling SystemSDR TC8A97009Compressor · stalledNR 4 ENGINE COMPRESSOR STALLED WITHIN 3 TO 4 SECONDS AFTER FULL TAKEOFF POWER APPLIED, 1.87 EPR / 22 DEGREES CELCIUS TEMP / ALTIMETER 30.17 AT SEA LEVEL.Jan 17, 1997 · N184SK · Doug DC861F · Turbine Engine Compressor SectionSDR TC8A97008Bleed Valve · failedNR 4 ENGINE COMPRESSOR STALLED WITHIN 3 TO 4 SECONDS AFTER FULL TAKEOFF POWER APPLIED, 1.87 EPR / 26 DEGREES CELSIUS TEMP / ALTIMETER 30.01 AT SEA LEVEL. REMOVED AND REPLACED NR 4 ENGINE SURGE BLEED VALVE AS PERMM 75-30-3, OPS CHECKS NORMAL ON ENGINE RUN-UP.Jan 17, 1997 · N184SK · Doug DC861F · Compressor Bleed ValveSDR TC8A97007Compressor · stalledNR 4 ENGINE COMPRESSOR STALLED WITHIN 3 TO 4 SECONDS AFTER FULL TAKEOFF POWER APPLIED, 1.87 EPR / 21 DEGREES CELCIUS TEMP / ALTIMETER 30.1 AT SEA LEVEL. SECURED LOOSE SENSE LINE AT PRBC, PERFORMED GROUND RUN AT 1.87EPR, GROUND OPS CHECKS GOOD IAW DC8 M/M 71-0Jan 17, 1997 · N184SK · Doug DC861F · Turbine Engine Compressor SectionSDR TC8A97003Circuit Breaker · trippedKMIA - FLT NR 01501. ON PUSHBACK, NR 4 MAIN FUEL PUMP BREAKERS (3) POPPED. CORRECTIVE ACTION: SUMPED TANK AND CLEANED BOOST AND FEED PUMP, SYSTEM CHECKS NORMAL PER MM, CH. 28.Jan 15, 1997 · N184SK · Doug DC861F · Fuel Boost PumpSDR TC8A97002Smoke Detector · malfunctionedON PUSHBACK, CARGO SMOKE DETECTOR LIGHT ILLUMINATED. REPAIRED NR 2 SMOKE DETECTOR, SYSTEM OPS CHECKS NORMAL IAW MM 26.Jan 15, 1997 · N184SK · Doug DC861F · Smoke DetectionSDR TC8A97001Crossfeed Valve · malfunctionedPNEUMATIC CROSSFEED VALVE WON'T OPEN. REMOVED AND REPLACED CROSS FEED VALVE, SYSTEM OPS CHECKS GOOD IAW MM 36.Jan 15, 1997 · N184SK · Doug DC861F · Pneumatic Distribution SystemSDR CKSA96162Insulator · out of positionIN FLIGHT, NR 3 FIRE WARNING WENT OFF. COMPLETED ALL APPROPRIATE CHECKLISTS, VISUALLY INSPECTED NR 3 ENGINE AND NO DEFECTS NOTED. FOUND INSULATOR NR 3 ENGINE FIRE LOOP OUT OF PLACE. REINSTALLED INSULATOR PER DACO DC-8 MM 26-10-1. NR 3 ENGINE FIRE WARNING TOct 18, 1996 · N813CK · Doug DC861F · Fire DetectionSDR ABXA9600643Transmitter · defectiveNR 3 OIL PRESSURE FLUCTUATES BETWEEN 46 AND 51 PSI WITH CRUISE POWER SET. FLUCTUATION STOPS AS THROTTLE IS RETARDED TO IDLE IN DESCENT BUT FLUCTUATION BEGINS AS POWER IS APPLIED. AT INTERMEDIATE LEVEL OFF OIL TEMP WAS 45 DEGREES CELSIUS, OIL QUANTITY 8.9 GALOct 7, 1996 · N849AX · Doug DC861F · Engine Oil PressureSDR ABXA9600635Relief Valve · stickingDURING DESCENT, NR 3 OIL PRESSURE DROPPED TO 25 PSI WITH NR 3 OIL PRESSURE LIGHT ILLUMINATED. ENGINE SECURED, OIL QUANTITY 9 GALLONS, OIL TEMPERATURE 75 DEGREES CELSIUS AT SHUTDOWN. WIND MILLED APPROXIMATELY 12 MINUTES, OIL PRESSURE DID NOT GO BELOW 24 PSI. Oct 4, 1996 · N849AX · Doug DC861F · Engine Oil PressureSDR CKSA95131Strut · brokenMIA - FLT 61556 - REFERENCE MRR NR 95-002, DATED 1-15-95. IN THE PROCESS OF TOWING AIRCRAFT, THE NOSE GEAR LOWER STRUT BROKE OFF APPROXIMATELY 12 INCHES FROM THE BOTTOM OF THE STRUT. UPON DISASSEMBLY AND INVESTIGATION, FOUND CRACK INITIATION WAS ATTRIBUTED TNov 1, 1995 · N813CK · Doug DC861F · Nose/Tail Landing Gear Strut/AxleSDR ABXA9500572Spring · wornFIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. FOUND SPRING ON LOWER AFT LOCKING HOOK STRETCHED AND INOPERATIVE. REPLACED LOWER LOCK HOOK SPRING IAW DC-8 MM 56-10-3, WINDOW OPS CHECKED GOOD.Jun 29, 1995 · N849AX · Doug DC861F · Flight Compartment WindowsSDR CKSA95060Floor Beam · crackedKYIP - DURING 'C-3' CHECK INSPECTION, FOUND FLOOR BEAM AT STA 798.00 BETWEEN SEAT TRACKS 3 AND 4 WITH END CLIPS CRACKED. REMOVED AND REPLACED END CLIP STA 798.00 BETWEEN SEAT TRACKS 3 AND 4 PER SKA95110-3. INSTALLED PANELS AS REQUIRED. REPAIRED END CLIP STAJun 20, 1995 · N813CK · Doug DC861F · Fuselage Main, Floor BeamSDR CKSA95059Angle · corrosionKYIP - DURING 'C-3' CHECK INSPECTION, FOUND CORROSION AT STA 280.0 BETWEEN LONGERONS 32L AND 33L. REMOVED AND REPLACED CORRODED ANGLE IAW EA NR 95-168. (X)Jun 20, 1995 · N813CK · Doug DC861F · Fuselage Miscellaneous StructureSDR CKSA95058Panel · corrodedKYIP - DURING 'C-3' CHECK INSPECTION, FOUND GALLEY FLOOR CORRODED. REMOVED AND CUT OUT CORRODED PORTION OF GALLEY FLOOR AND REPAIRED PER EA NR 95-168.C. (X)Jun 20, 1995 · N813CK · Doug DC861F · Fuselage Floor Panel
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