Douglas DC-8-63F
Service difficulty reports · 1,883
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 = '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.
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
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 ABXA010184Splice · crackedFITTING AT PRODUCTION SPLICE FS 1690 32R WAS CRACKED.SDR ABXA010183Longeron · corrodedLONGERON 24 IN LEFT MAIN LANDING GEAR WHEEL WELL HAS CORROSION ON UPPER SURFACE, BETWEEN STA 879 AND 902.SDR ABXA010182Longeron · corrodedCORROSION FOUND ON UPPER SURFACE OF LONGERON 24 AT FS 920. CORROSION EXTENDS UNDER FITTING IN LEFT MAIN LANDING GEAR WHEEL WELL.SDR ABXA010150Fitting · crackedTHE LEFT WING LOWER TRAPEZOID FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 57-5-2.SDR ABXA010554Pressure Panel · corrodedCORROSION ON THE UPPER SURFACE OF THE PRESSURE WEB AND ON FINGER DOUBLER. ALSO RIVET HEADS WERE SHEARED OFF BETWEEN FS 920-980. REPAIRED AREA AND REPLACED THE DOUBLER IAW DC-8 SRM 51-1-8, 53-2-0, AND REA D853-40413-MR, AND DAC DRAWING NR 5645332.SDR ABXA010555Pressure Panel · corrodedCORROSION AND SEVERAL RIVET HEADS SHEARED OFF BETWEEN FS 900-940, ON UPPER SURFACE OF PRESSURE WEB AT BUTT LINE 00. REPAIRED AREA AND REPLACED DOUBLER AND GUSSET IAW DC-8 SRM 51-1-20, 51-1-11, 51-3-0, 51-1-21, 51-1-8, 53-20, AND DAC DRAWING NR 5645332, AND REASDR ABXA010552Doubler · bulgedBULGING FINGER DOUBLER AND RIVET HEADS WERE SHEARED ON THE UPPER SURFACE OF THE PRESSURE WEB BETWEEN FUSELAGE STATION 880 AND BUTT LINE 00. REPAIRED AREA AND INSTALLED NEW FINGER DOUBLER IAW DC-8 SRM 51-1-21, 51-1-8, 53-2-0, 51-9-0, 51-1-20D, 51-1-11, AND DRAWSDR ARWA0010308Warning Light · erraticABORT TAKEOFF BELOW IAS AT BGI DUE THE ANTI-SKID LIGHT FLICKERING ON/OUT. FOLLOW CHECKLIST FOR ATO. CHECKED ANTI-SKID SYSTEM, CONTROL MONITOR, AND RESET ANTI-SKID SWITCH. LIGHT CHECK NORMAL. COULD NOT DUPLICATE, CONTINUE WITH SCHEDULE DEPARTURE WITHOUT FURSDR ABXA010139Structure · leakingA FASTENER WAS FOUND TO BE LEAKING FUEL AT STA 795. MAINTENANCE REPAIRED THE AREA IAW REA D857-40312MR AND DC-8 SRM.SDR ARWA0010306Swivel · leakingAT 1245Z ON CLIMBOUT HYD SYS QTY LOSS FLUID DOWN TO 5 GALLONS. HYD EMERGENCY CK LIST COMPLETED, ABNORMAL LANDING CK LIST COMPLIED WITH AND COMPLETED. FOUND RT AILERON SWIVEL GLAND PORT LEAKING, REPACKED IAW MM 20-60-0 SERVICED FLUIDS IAW MM 12-00-1, OPERATIOSDR ARWA0010305Bolt · brokenDURING PREFLIGHT INSPECTION FOUND LT INBOARD FLAP TRACK BROKEN HANGER BOLT. REMOVED AND REPLACED LT INBOARD FLAP STA 97 TRACK HANGER BOLT IAW MM 27-51-3. OPERATIONAL CHECK OF THE FLAP SYSTEM FOUND NORMAL IAW MM 27-53-1.SDR ABXA010142Fitting · corrodedCORROSION WAS FOUND ON END FITTING AT FUSELAGE STATION 8-28 LONGERON 27R IN THE FORWARD AIR-CONDITIONING COMPARTMENT. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 51-1-8, 51-2-0 AND DAC DRAWING 4711722.SDR ABXA010144Fitting · corrodedCORROSION WAS FOUND AT THE FORWARD AIR-CONDITIONING PRESSURE COMPARTMENT AT THE RIGHT CUSP FITTING. CORROSION WAS FOUND UNDER AND AROUND THE NUT PLATES. MAINTENANCE INSTALLED A NEW FITTING IAW DC-8 SRM 51-1-20 AND 51-3-0.SDR ABXA010151Fitting · crackedTHE RIGHT WING LOWER FORWARD TRAPEZOID FITTING WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 57-2-7.SDR ABXA010141Fitting · corrodedCORROSION WAS FOUND ON FITTING AT THE LEFT MLG WHEEL WELL AT FUSELAGE STATION 857. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D853-40267-MR AND DC-8 SRM 53-2-0.SDR ABXA010147Longeron · corrodedCORROSION WAS FOUND ON LONGERON 33L BETWEEN FUSELAGE STA 320 - 340 IN LOWER CARGO PIT. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 53-2-0.SDR ABXA010148Longeron · corrodedCORROSION WAS FOUND AT THE FORWARD LOWER CARGO PIT BETWEEN STA 280 AND 300, LONGERON 28L. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 51-1-8 AND DAC DRAWING 9754931.SDR ABXA010145Skin · crackedTHE FUSELAGE EXTERIOR SKIN AT STATION 1750 LONGERON 15R-16R WAS FOUND TO BE CRACKED BETWEEN FASTENERS. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 53-2-1.SDR ABXA010146Skin · crackedTHE FUSELAGE EXTERIOR SKIN WAS FOUND TO BE CRACKED AT STA 1720 LONGERON 17-18R. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW DC-8 SRM 53-2-1.SDR ABXA010149Seat Track · corrodedTHE MAIN CARGO COMPARTMENT SEAT TRACK AT RBL 30, STATION 1723 - 1746 WAS CORRODED. MAINTENANCE INSPECTED AND INSTALLED A NEW SEAT TRACK IAW DC-8 SRM 51-3-0 AND ZANTOP DRAWING 86302.SDR ABXA010140Stiffener · corrodedTHE RIGHT MLG WHEEL WELL HORIZONTAL PRESSURE WEB WAS FOUND TO BE CORRODED. A STIFFENER WAS FOUND TO BE BULGING AT STA 902 RBL 56 THROUGH 65. MAINTENANCE REPAIRED THE AREA IAW REA D853-40284, DAC DRAWING 5645332 AND DC-8 SRM 51-1-8.SDR ABXA010138Frame · crackedA CRACK 4.5 INCH LONG WAS FOUND ON THE NOSE WHEEL WELL AFT DOOR FORWARD HINGE FRAME. MAINTENANCE REPAIRED THE CRACK IAW REA D853-40280MR.SDR ABXA010417Structure · leakingSPAR CAP LEAKED FUEL JUST INBOARD OF NR 1 PYLON AT S - 64 DOUBLER. REMOVED DOUBLER AND TRIPLER. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW ABX REA D857-40311MR AND DAC DWG SRO8570013.SDR ABXA010143Structure · leakingTHE SPAR CAP WAS FOUND TO BE LEAKING FUEL JUST INBOARD OF THE NR 1 PYLON AT WS 444. MAINTENANCE INSPECTED AND REPAIRED THE AREA IAW ABX REA D857-40311MR.SDR ABXA010152Seat Track · corrodedTHE SEAT TRACK AT FUSELAGE STATION 920 HAD A CORRODED FASTENER HOLE. MAINTENANCE INSPECTED AND INSTALLED A NEW SEAT TRACK AT STATION 870 - 940 IAW DC-8 SRM 51-3-0 AND 51-1-21.SDR U2RB030101Spar Cap · crackedDURING COMPLIANCE OF MCDONNELL DOUGLAS DC-8 S/B 57-90 R5 (NPRM 99-NM-60-AD) DETECTED CRACK ATLOWER FORWARD SPAR AT ATTACH FASTENERS STA XFS 524. CRACK BEYOND S/B 57-90 R5 REPAIR LIMITS.SDR ABXA010415Skin · gougedLEFT WING LEADING EDGE STAB WING ABOVE #2 ENGINE, OUTBOARD END OF VANE HAD SEVERAL HOLES WITH VERY DEEP GOUGES CAUSED BY DIMPLE WASHERS, APPROXIMATELY W/STA. 225.0 REMOVED SEAL ASSEMBLY, FABRICATED REPAIR DOUBLER IAW REA D857-39765MR. ALODINED AND PRIMED IAW SDR ABXA010040Rudder · bindingDURING TAXI WHILE PERFORMING THE FLIGHT CONTROL CHECK, THE RUDDER WAS REPORTED TO BE BINDING NEAR THE LAST 1/3 OF RIGHT INPUT TRAVEL. MAINTENANCE INSPECTED AND CYCLED THE RUDDER NUMEROUS TIMES. THE RUDDER POWER CONTROL UNIT AND PRESSURE REDUCER VALVE WAS INSSDR ABXA0100040Control Unit · failedDURING TAXI WHILE PERFORMING THE FLIGHT CONTROL CHECK, THE RUDDER WAS REPORTED TO BE BINDING NEAR THE LAST 1/3 OF RIGHT INPUT TRAVEL. MAINTENANCE INSPECTED AND CYCLED THE RUDDER NUMEROUS TIMES. THE RUDDER POWER CONTROL UNIT AND PRESSURE REDUCER VALVE WAS INSSDR ARWA0010202O-Ring · damagedCLIMBOUT A LOSS OF HYDRAULIC FLUID DOWN TO STAND PIPE. AFTER LANDING MIA, FOUND HEAVY HYDRAULIC LEAK COMING FROM RT WING AILERON SWIVEL. INSPECTED SWIVEL AND FOUND BOTH O-RINGS DAMAGED. REMOVED AND REPLACED O-RINGS AS REQUIRED. FOUND NORMAL, NO LEAKS IAW DSDR ABXA010416Frame · crackedFORWARD LOWER CARGO, STATION 420, CRACK ON FRAME AT LONGERON 31 LEFT.SDR ABXA010414Skin · crackedEXTERIOR FUSELAGE, BULGING SKIN NEAR FLAPPER AT STATION 110, LONGERON 36. REMOVED FLAPPER VALVE IAW REA D853-39745MR. FABBED FILLER AND FINGER DOUBLER IAW REA D853-39745MR. ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED FILLER, FINGER DOUBLER AND FLAPPER VSDR 20010403CW001Wire · brokenAFTER TAKEOFF, PILOT NOTICED ODD SMELL, FOLLOWED BY SMOKE. HE DECLARED AN EMERGENCY AND RETURNED TO AIRPORT WITHOUT INCIDENT. TROUBLE SHOT SYSTEM, FOUND OLD DEAD END GALLEY WIRE LAYING ON RES R4-35. REMOVED OLD WIRE. CHECKED WIRING TO SWITCHES 51-403, 51-3SDR 20010124SG002Compressor · overservicedON TEST FLIGHT, SMOKE IN COCKPIT. FOUND NR 2 AND NR 3 TURBO COMPRESSORS OVERSERVICED. SERVICED PROPERLY IAW MM 21-10-01. (M)SDR RRXA001091Compressor · stalledON CLIMBOUT WITH ENGINE ANTI-ICE ON NR 3 ENG COMPRESSOR STALLED, OIL PRESSURE WAS 59 PSI. DURING B-CHECK INSP FOUND PRBC LOCKED UP. REMOVED AND REPLACED PRBC IAW 75-30-3. BORESCOPE NR 3 ENG IAW DC-8 MM 72-00 431453082, PRBC CHECKS GOOD, NO COMPR STALL ON ENSDR ABXA000528Seal · cutTWENTY MINUTES AFTER TAKEOFF FROM EWR, THE NR 3 ENGINE OIL PRESSURE FLUCTUATED AND OIL QUANTITY DROPPED TO APPROX. ZERO GALLONS. THE CREW SHUT THE ENGINE DOWN IN FLIGHT, IAW ABX PROCEDURES. MAINTENANCE INSPECTED AND FOUND THE NR 3 FRONT ACCESSORY HOUSING O-RINSDR ABXA000521Engine · seizedON TAKEOFF FROM PHL, THE NUMBER TWO ENGINE SIEZED. THE CREW SECURED THE ENGINE AND CONTINUED TO ILN. ILN MAINTENANCE INSPECTED AND REPLACED THE NUMBER TWO ENGINE IAW ABX JOBCARD 8090507.SDR ARWA0001229Fitting · corrodedAFT CARGO COMPARTMENT FITTING SHOWS CORROSION AT STA 1220 BETWEEN LONG 35L AND 36L. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED AND REPLACED FITTING IAW SRM 53-2-0, FIG 2D AND 51-1-20D.SDR ARWA0001228Fitting · corrodedFORWARD CARGO COMPARTMENT LONG 28L FITTING WITH CORROSION AT STA 80. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. INSTALLED RIVETS IAW SRM 51-1-21.SDR ARWA0001227Fitting · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FWD CARGO COMPARTMENT FITTING SHOWS CORROSION LEVEL 2 AT STA 340 BETWEEN LONG 34L AND LONG 35L. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 AND SRM 51-1-20D.SDR ARWA0001226Fitting · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: AFT CARGO COMPARTMENT FITTING WITH CORROSION BETWEEN STA 1220 AND STA 1240 AND BETWEEN LONG 35R AND LONG 36R. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED FITTING IAW SRSDR ARWA0001225Fitting · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: AFT CARGO COMPARTMENT FITTING SHOWS CORROSION AT STA 1220, LONG 36L. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED FITTING IAW SRM 51-1-20D. CUT NEW FITTING AND FABRICATSDR ARWA0001224Floor Support · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: AFT CARGO COMPARTMENT FLOOR SUPPORT WITH CORROSION AT STA 1260. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED SUPPORT IAW SRM 51-1-21. FABRICATED NEW SUPPORT IAW SRM 51-SDR ARWA0001223Longeron · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: AFT CARGO COMPARTMENT SKIN SHOWS CORROSION AT STA 1540 LONG 25R. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED LONGERON SECTION IAW SRM 51-1-20D. CUT NEW LONGERON SECTIONSDR ARWA0001221Fitting · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: AFT CARGO COMPARTMENT LONGERON FLANGE AND INTERNAL FITTING SHOW CORROSION AT STA 1160, LONG 34R. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE WITHIN LIMITS LONGERON FLANGE AND OUT OF LIMITS FITTINGS IAW SRM 5SDR ARWA0001222Fitting · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: AFT CARGO COMPARTMENT INTERNAL SKIN AND FITTING SHOW CORROSION BETWEEN LONG 33R AND LONG 34R, STA 1160. REMOVED CORROSION IAW SRM 51-1-8, FOUND TO BE WITHIN LIMITS INTERNAL SKIN AND OUT OF LIMITS FITTING IAW SRSDR ARWA0001220Splice · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: AFT CARGO COMPARTMENT FITTING WITH CORROSION AT STA 1152 AND LONG 35L. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED SPLICE IAW SRM 51-1-20D. FABRICATED NEW SPLICE IAW SSDR ARWA0001206Skin · damagedN/R 268 - DURING C CHECK INSPECTION FOUND THE FOLLOWING: EXTERIOR FUSELAGE SKIN SHOWS TEMPORARY REPAIR AT STA. -32.00 LONG. 31 RT.REMOVED TEMPORARY REPAIR AND INSTALLED REPAIR IAW BOEING MESSAGE INW-LIM-00-00144H AND ROD SKETCH 00-10-10-004.SDR ARWA0001205Skin · crackedN/R 0026 - DURING C CHECK INSPECTION, FOUND THE FOLLOWING: CRACKED RT WING UPPER SKIN SURFACE STA.XRS 107 10 INCHES BELOW REAR SPAR. REPAIR CRACK IAW BOEING MESSAGE INW-LIM-00-00130H, DATED 09/18/00SDR ARWA0001211Panel · corrodedN/R 251 - DURING C CHECK INSPECTION FOUND THE FOLLOWING: LEVEL I CORROSION AT LT HORIZONTAL STABILIZER LOWER PANEL AT STA.XE 312.500.REMOVED AND REPLACED SKIN PANEL IAW DRAWING # AS11210, DATED 10/07/00, SEALED AREA IAW SRM 51-1-15.
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