Douglas DC-8-61
Service difficulty reports · 942
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 = 'DC861' 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 = 'DC861' 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 ABXA9600193Doubler · corrodedDURING C-CHECK INSPECTION, DISCOVERED RIGHT WING LEADING EDGE HAS CORROSION UNDER RETAINER RING INSIDE PANEL 517B. REPAIRED RIGHT WING OUTBOARD LEADING EDGE INTERNAL DOUBLER ACCESS PANEL 517B, AT XFS 845 IAW ABX REA-D857-13486-MR.SDR ABXA9600192Beam · crackedDURING C-CHECK INSPECTION, DISCOVERED FORWARD CROSS-SLIDE DOOR AT NR 1 PIT LOCKING HOOK FITTING, 4TH HOOK FROM FORWARD END, FRAME BEAM IS CRACKED. REPAIRED BEAM AT FORWARD CROSS-SLIDE DOOR IAW ABX REA-D852-13484-MR.SDR ABXA9600191Panel · corrodedDURING C-CHECK INSPECTION, DISCOVERED RIGHT WING LEADING EDGE ALONG FORWARD RIB CORRODED AND SKIN PULLING UP OVER RIVETS AT STATION 329 INSIDE LEADING EDGE PANEL 522B. REPAIRED RIGHT WING LEADING EDGE LOWER ACCESS PANEL 522B IAW ABX REA-D857-13489-MR.SDR ABXA9600190Skin · corrodedDURING C-CHECK INSPECTION, DISCOVERED FUSELAGE SKIN CORRODED AT FUSELAGE STATION 1114 OUTBOARD OF LONGERON 36, JUST FORWARD OF EXISTING REPAIR. REPAIRED FUSELAGE CORRODED LOWER SKIN AT FUSELAGE STATION 1114, LONGERON 34L TO 34R IAW ABX REA-D853-13488.SDR ABXA9600109Control Cable · brokenNR 2 ENGINE FIRE SHUTOFF CABLE BROKEN IN PYLON. REPLACED PNEUMATIC SHUTOFF CABLE RUN 59.1 IN NR 2 PYLON AND OPS CHECK GOOD.SDR CKSA96008O-Rings · deterioratedKSEA - FLT 71431 - EN ROUTE TO KSEA LOST HYDRAULIC QUANTITY AND PRESSURE. RESEALED STABILIZER LOCK-OUT SWIVEL. OPS AND PRESSURE CHECK OK IAW 27-11-7. (X)SDR ABXA9600071Hyd Hose · failedDURING CRUISE, HYDRAULIC QUANTITY DROPPED TO STANDPIPE LEVEL. FOUND HYDRAULIC PRESSURE LINE BLOWN ON NR 2 ENGINE. REPLACED PRESSURE LINE AND THE NR 2/NR 3 HYDRAULIC PUMPS IAW DC8 MM, CHAPTER 29-10-12. OPS CHECK AND LEAK CHECK WERE GOOD.SDR CKSA96006Dnlock Switch · intermittentKSEA - ON APPROACH TO KSEA, HAD UNSAFE LANDING LEFT GEAR LIGHT INDICATION. RECYCLED GEAR SEVERAL TIMES. LEFT MAIN GEAR DOWNLOCK LIGHT ILLUMINATED, LANDED WITHOUT INCIDENT. VISUALLY INSPECTED LEFT MAIN LANDING GEAR UPLATCH ASSEMBLY, AND ALL MECHANICAL COMPONSDR ABXA9600007Control Valve · brokenLEFT BRAKES GO FULL TRAVEL WITH NO BRAKING ACTION. BRAKE PRESSURE AND FLUID QUANTITY ARE NORMAL. REPLACED BROKEN BRAKE CONTROL VALVE IAW DC8 MM. OPS CHECK GOOD.SDR ABXA9600003Bulb · defectiveEMERGENCY EXIT DISARM LIGHT ON OVERHEAD PANEL INOP. RELAMPED EMERGENCY EXIT DISARM LIGHT AND OPS CHECK GOOD.SDR BUFA9527Connector · looseFLT MIA/CAE (MIA/MIA) - F/O ART. HORIZ FAILED. TEST CAUSES NO REACTION EXCEPT RANDOM ATTITUDES. FOUND LOOSE CANNON PLUG AND RESET BREAKER, TIGHTEN CANNON PLUG. OPS CHK NORMAL IAW MM 34-23-0. (X)SDR 96ZZZM265Bogie Actuator · leakingIN CLIMB BAQ, RIGHT MAIN LANDING GEAR DOOR UNLATCHED LIGHT ON AND UNSAFE LIGHT ON RIGHT MAIN LANDING GEAR. RETURNED TO BAQ AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED HYDRAULIC FLUID LEAKAGE AT THE BOGIE TRIM ACTUATOR. REPLACED TRIM ACTUATOR AND RETURNSDR BUFA9525Pitot Tube · dirtyFLT EWW133 ELP-PIA ELP-ELP - CAPTAIN'S AIRSPEED INDICATOR INOP. DURING TAKEOFF ROLL, ZERO KNOTS, FIRST OFFICER 80 KNOTS. TAKEOFF ABORTED. FOUND OBSTRUCTION (SAND) IN CAPTAIN'S PITOT TUBE. CLEANED AND REMOVED SAND. OP CHECK OK PER MM 34-11. (X)SDR ABXA9500932Eel Lamp · failedDURING SERVICE CHECK, FOUND THE EMERGENCY LIGHTING INOP. RELAMPED POSITIONS AND EMERGENCY LIGHTING OPS CHECKED GOOD IAW ABX WORK CARD DC-8-1 ITEM NR 8.SDR BUFA9523Lines · leakingGGT/MIA - FLT CWC148 - LOSS OF HYDRAULIC FLUID TO STAND PIPE. COMPLETED EMERGENCY PROGRESS CHECK LIST. FOUND LEAK AT SEVERAL HYDRAULIC LINES. REMOVED AND REPLACED BAD HYDRAULIC LINES IAW MM 29-10. (X)SDR CKSA95105Connector · shortedKMIA - ON CLIMB-OUT, HAD ENGINE FIRE INDICATION ON NR 2 ENGINE. FIRED ONE BOTTLE, FIRE INDICATION PERSISTED. FIRED SECOND BOTTLE, FIRE INDICATION PERSISTED. REPLACED DAMAGED AND SHORTED CANNON PLUG. CONNECTOR AT LOWER FORWARD FIRE LOOP CONNECTION RAN ENGINSDR IXXA199586Smoke Detector · malfunctionedFLL/BNA - EN ROUTE, MAIN CARGO COMPARTMENT SMOKE DETECTORS 2, 4, 6, 8, AND 10 ILLUMINATED. THE LIGHTS WOULD EXTINGUISH FOR SHORT PERIODS OF TIME, AND ILLUMINATE AGAIN. THERE WAS NO EVIDENCE OF FIRE, BUT THE AIRCRAFT PRECAUTIONARILY DIVERTD TO ATL TO MAKE A CSDR BUFA9522Oil Cooler · malfunctionedMIA-MCI - SHUT DOWN NR 1 ENGINE, OIL TEMPERATURE 143 DEGREES AND RISING, CSD RISE TEMPERATURE PLUS 15 DEGREES, RETURNED TO MIA. REMOVED AND REPLACED NR 1 ENGINE OIL COOLER. OP CHECK GOOD IAW 79-00. (M)SDR 95ZZZM562Ballast · shortedON DESCENT INTO MIAMI, EXPERIENCED BURNING ODOR IN COCKPIT. ON GROUND INSPECTION FOUND GLARE SHIELD LIGHT BALLAST OVERHEATED. REPLACED BALLAST, SYSTEM CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR BUFA9521Oil Line · looseMROC-MIA - NR 1 ENGINE LOW OIL PRESSURE LIGHT CAME ON 15 MILES TO MIA. AT FLIGHT IDLE, OIL PRESSURE INDICATOR READ LOW RED LINE. PRECAUTIONARY ENGINE SHUT DOWN PROCEDURE COMPLETED BEFORE LANDING MIAMI. NO EMERGENCY DECLARED, LANDING UNEVENTFUL. FOUND LOOSESDR ABXA9500740Seat · lack of lubeFIRST OFFICER'S SEAT WOULD NOT REMAIN LATCHED IN POSITIONS SELECTED, FORWARD AFT POSITIONS. LATCH PINS NOT FULLY ENGAGING IN TRACK. LUBED TRACKS, LATCH PINS AND SEAT OPS CHECKED GOOD PER DC8 MM.SDR BUFA9720Oil Cooler · leakingFLT 0X0701 - TPP-GAS - NR 4 ENGINE HAD LOSS OF OIL PRESSURE AND QUANTITY, WIND MILL OK PRESSURE WAS 20 PSI. REMOVED AND REPLACED NR 4 ENGINE HEAT OIL COOLER. RUN ENGINE, OPS CHECK GOOD. LEAK CHECK GOOD IAW MM72-00. (M)SDR BUFA9719Oil Cooler · leakingFLT 0X0401 - MIA-POS - SHUT DOWN NR 4 ENGINE IN FLIGHT DUE TO LOW OIL PRESSURE AND LOW OIL QUANTITY. NO EMERGENCY DECLARED. REMOVED AND REPLACED NR 4 ENGINE FUEL HEAT OIL COOLER. RUN ENGINE, OPS CHECK GOOD. LEAK CHECK GOOD IAW MM 72-00. (M)SDR BUFA9718Wire · failedFLT GAC801 - MIA-CCS - STANDBY HORIZON TUMBLING 90 DEGREES NOSE UP 25 DEGREES BANK DURING INITIAL AND NORMAL CLIMB AFTER TAKEOFF, RETURNED TO MIA. REPAIRED WIRING AT PIN C OF STATIC INVERTER, SYSTEM OPS CHECK GOOD IAW DMM 34-28-0. (M)SDR 95ZZZM505Clamp · brokenAFTER TAKEOFF MIA, EXPERIENCED LOUD NOISE AND VIBRATION IN NOSE LANDING GEAR AREA. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED THE CONDENSER RAM AIR DUCT DISCONNECTED DUE TO A BROKEN CLAMP. RE-INSTALLED DUCT, REPLACED CLAMP, PERFORMED OSDR 95ZZZM445Link · stickingAFTER TAKEOFF SDQ, RIGHT NOSE GEAR DOOR WOULD NOT CLOSE. RETURNED TO SDQ AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED RELEASE PIN STICKING IN FORWARD RT DOOR LINK ASSY. REPLACED LINK EPR MM 32-22-2. RETURNED AIRCRAFT TO SERVICE.SDR ABXA9500672Brace · crackedDURING POST FLIGHT WALK-AROUND, FOUND A CRACK IN THE LEFT SIDE BRACE OF THE NOSE LANDING GEAR, JUST BELOW THE DOOR ATTACH POINT. REPLACED THE LEFT SIDE BRACE IAW DC-8 MM 32-21-3, OPS CHECKED NORMAL.SDR ABXA9500656Engine · failedNR 4 ENGINE SHUTDOWN IN FLIGHT DUE TO ENGINE FAILURE. EGT MAXIMUM TEMPERATURE WAS 760 DEGREES CELSIUS. NR 4 ENGINE WAS SECURED IAW EMERGENCY PROCEDURE CHECKLIST. AIRCRAFT RETURNED TO ILN. REMOVED AND REPLACED ENGINE. TRIMMED DURING GROUND RUN IAW DC 8 MM.SDR BUFA9717Door · not closedFLT MRX793 - SBKP-SPIM - UNABLE TO PRESSURIZE AIRCRAFT, RETURNED TO SBKP. FOUND AIRCRAFT AIR COND DOOR OPEN. OPS CHECKED DOOR AND CLOSED DOOR IAW MM 52-00. (M)SDR ABXA9500735Door Pan · corrosionDURING C - CHECK INSPECTION, FOUND CORROSION ON THE C-2 DOOR PAN. REPAIRED IAW ABX REA D852-11915-MR.SDR ABXA9500734Angle · corrodedDURING C - CHECK INSPECTION DISCOVERED CORROSION ON UPPER WEB ATTACH ANGLE AT STATION 810. REPAIRED IAW ABX REA D853-11911-MR.SDR ABXA9500733Doubler · corrodedDURING C - CHECK INSPECTION FOUND CORROSION ON DOUBLER AT STATION 852 AT XCW 4L AND XCW 6R ON CENTER WING SECTION. REPAIRED IAW ABX REA D857-11890-MR.SDR ABXA9500578Flex Line · leakingHYD SYS PRESS GAUGE READ ZERO WITH BOTH AILERON AND RUDDER REVERSION LIGHTS ON. HYD QTY READ FULL WITH LOW RESERVOIR, LOW PRESS, AND TEMP LIGHTS OUT. REPOWERED AILERONS WITH AUX PUMP; PRESS AND QTY CHECKED OK. AILERON LIGHT EXTINGUISHED, COULD NOT RESTORE NSDR ABXA9500574Packing · leakingON CLIMB-OUT OF ONT, HYDRAULIC QUANTITY LOSS AND PRESSURE OF ZERO WAS INDICATED. RESERVOIR LOW PRESSURE LIGHT ILLUMINATED AT 6 GALLONS HYDRAULIC QUANTITY. REPACKED SLOT CONTROL VALVE. ALSO, REMOVED AND REPLACED NR 1 AND NR 2 HYDRAULIC PUMPS AND FILTERS IAWSDR ABXA9500573Transmitter · defectiveENROUTE TO ILN, NR 1 ENGINE OIL PRESSURE PEGGED TO THE HIGH SIDE. CREW SHUT DOWN ENGINE AS PRECAUTIONARY PROCEDURE. OIL PRESSURE STILL READ PEGGED HIGH. WITH ENGINE SHUT DOWN, OIL PRESSURE READ 100 PSI; SHUT DOWN FOR APPROXIMATELY 20 MINUTES. ALL OTHER INDSDR CKSA95083B-Nut · looseSFO - ON TAKEOFF, HYDRAULIC CAME DOWN AND GEAR TOOK LONGER THAN NORMAL TO RETRACT. CONTINUED TO CLIMB OUT, THE HYD FLUID LEVEL CONTINUED TO COME DOWN CONFIRMING A LOSS OF HYD FLUID OR PRESS. CHECKLIST, THE LOSS STOPPED. DECLARED A HYD EMERGENCY, DUMPED FUELSDR ABXA9500736Doubler · corrodedDURING C - CHECK INSPECTION, FOUND CORROSION ON UPPER JOINT DOUBLER AT XWC-0.00, STRINGER 4L. REPAIRED IAW ABX REA D857-11900-MR.SDR ABXA9500732Angle · corrodedDURING C - CHECK INSPECTION FOUND CORROSION ON FLANGE SHEAR WEB ATTACH ANGLE AT STATION 857, LBL 28 AND RBL 28. REPAIRED IAW ABX REA D853-11888-MR.SDR CKSA95037Retract Mech · malfunctionedKBUF - FLT 64648 - AFTER TAKEOFF, LOUD NOISE WAS HEARD FROM NOSE GEAR. RECYCLED GEAR, NO CHANGE. RETURNED TO BUF. MAINTENANCE INSPECTED NOSE GEAR WHEELWELL DOORS. NO DEFECTS NOTED. RESET NOSE GEAR DOORS IAW MM CHAPTER 52. (X)SDR ABXA9500528Bulb · defectiveWHEN GEAR WAS LOWERED, NO DOWN AND LOCKED INDICATION ON RIGHT MAIN GEAR. PUT GEAR UP AND RELAMPED RIGHT MAIN GEAR INDICATION. LOWERED GEAR AND RIGHT MAIN SHOWED DOWN AND LOCKED. VERIFIED BOTH RIGHT MAIN GEAR DOWN AND LOCK INDICATION BULBS BURNED OUT. RELAMSDR ABXA9600009Drive Link · crackedDURING COMPLIANCE OF AD 88-10-07, ASB A27-269, FOUND THE LEFT FLAP DRIVE LINK CRACKED AT POINT-J USING ULTRASONIC METHOD OF INSPECTION. REPLACED LEFT FLAP DRIVE LINK IAW DC8 MM.SDR CKSA95035Bolt · looseRDU - NOSE GEAR DOWN WARNING LIGHT INTERMITTENT, CYCLED GEAR, WARNING LIGHT REMAINS INTERMITTENT. TIGHTENED LOOSE ATTACHING HARDWARE. OPS CHECK GOOD ON GROUND. INSPECTED AND FOUND NO DEFECTS PER DC-8, MM 32-60-0. (X)SDR 95ZZZM197Frame · corrodedDURING C-CHECK, CORROSION DAMAGE WAS FOUND ON THE FUSELAGE FRAME AT FS 1700 BETWEEN L34R AND L35L. REMOVED AND REPLACED FUSELAGE FRAME AT FS 1700. INSTALLED STRAP DOUBLER AND ACCOMPLISHED REPAIR SPLICE ON FUSELAGE FRAME IAW EO 9505191. AN 8110-3 ISSUED BY DSDR 95ZZZM196Doubler · corrosionDURING C-CHECK, CORROSION WAS FOUND ON THE FUSELAGE SKIN AROUND THE OPENING OF THE C-3 DOOR FS 1160. TRIMMED OFF CORROSION DAMAGE, INSTALLED .125 7075-T6 FILLER WITH .125 7075-T6 EXTERNAL DOUBLER IAW EO 9505061. AN 8110-3 ISSUED BY DER SW-713.SDR 95ZZZM195Skin · corrosionDURING C-CHECK, CORROSION AND DISBONDING WAS FOUND ON THE RIGHT OUTBOARD AILERON LOWER SKIN PANEL. REMOVED LOWER SKIN AND REPLACED WITH AN 040 2024-T3 SKIN PANEL IAW EO 9505072. AN 8110-3 ISSUED BY DER SW-713.SDR 95ZZZM194Jamb · crackedDURING C-CHECK, MAINTENANCE FOUND A CRACK ON FORWARD CARGO COMPARTMENT FORWARD DOOR UPPER AFT JAMB CORNER. CUTOUT CRACKED SKIN, INSTALLED FILLER AND INSTALLED EXTERNAL DOUBLERS IAW DOUGLAS SRO DRAWING 8530019.SDR 95ZZZM193Jamb · crackedDURING C-CHECK, MAINTENANCE FOUND A CRACK ON THE FORWARD CARGO COMPARTMENT FORWARD DOOR FORWARD LOWER JAMB CORNER. CUTOUT CRACKED SKIN, INSTALLED FILLER AND INSTALLED EXTERNAL DOUBLERS IAW DOUGLAS SRO DRAWING SR08530019 AND DOUGLAS LETTER NR MISC 2400/RKK.SDR 95ZZZM192Skin · corrosionDURING C-CHECK, CORROSION WAS FOUND LEFT SIDE OF THE AIRCRAFT IN THE FUSELAGE SKIN FS 1680 BETWEEN L-22L TO L-24L. TRIMMED OUT DAMAGED SKIN, INSTALLED A .071 7075-T6 FILLER AND INSTALLED A .080 7075-T6 EXTERNAL DOUBLER IAW EO 9505251. AN 8110-3 ISSUED BY DERSDR 95ZZZM191Skin · corrodedDURING C-CHECK, CORROSION WAS FOUND AFT LOWER SKIN FROM FS STATION 1350 TO FS 1450 BETWEEN LONGERONS 31L TO 31R. REMOVED AND REPLACED AFT LOWER SKIN FROM FS 1350 TO FS 1450 BETWEEN 31L TO LONGERON 31R IAW SRM 51-1-21.SDR 95ZZZM138Skin · corrosionDURING C-CHECK CORROSION WAS FOUND ON RIGHT SIDE OF THE AIRCRAFT IN THE FUSELAGE SKIN FS 1680. TRIMMED OUT DAMAGED SKIN. INSTALLED A .071 7075-T-6 FILLER AND INSTALLED A .080 7075-T6 EXTERNAL DOUBLER IAW EO 9505251.
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