Douglas DC-8-61

Service difficulty reports · 942

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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 = '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.

SDR ABXA040090Skin · corrodedFORWARD LOWER CARGO CORROSION FUSELAGE SKIN AT LONGERON 35 LEFT, FS 620. REPAIR ACCOMPLISHED IAW REA D853-48847MR AND DC-8 SRM 53-2-1, 51-1-20D, AND 51-1-8.Feb 14, 2004 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA040063Plate · misrepairedFOUND MAIN ENTRY DOOR SCUFF PLATE DID NOT MEET REQUIREMENTS OF SERVICE REWORK DRAWING SRO8530021. TEMPORARY REPAIRED MAIN ENTRY DOOR SCUFF PLATE IAW REA D853-49056MR. PLACED ON CARRY OVER NR COI 46070. PROPER FASTENERS TO BE INSTALLED ON OR BEFORE 9-6-2005.Feb 14, 2004 · N847AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA040035Battery Pack · defectiveDURING MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. OPS CHECKED EVERY EXIT LIGHT IAW DC8-1, STEP 7. OPS CHECKED GOOD. OPS CHECKED AGAIN, NO GOOD. REPLACED EMERGENCY LIGHT POWER PACK IAW DC8 WDM 33-51-01. OPS CHECKED GOOD IAW DC8-1, STEJan 15, 2004 · N842AX · Doug DC861 · Emergency LightingSDR ABXA040034Battery Pack · defectiveDURING MAINTENANCE INSPECTION, FOUND BATTERIES FOR THE EMERGENCY LIGHT EXPLODED W/O 600187843. REPLACED BATTERY PACK AND OPS CHECKED GOOD IAW DC-8 MM 33-50-02-2.Jan 6, 2004 · N842AX · Doug DC861 · Emergency LightingSDR ABXA040013Longeron · corrodedFORWARD CARGO STA 300 TO 320, LONGERON 32 LEFT, ATTACH ANGLE HAD CORROSION. REMOVED CORROSION AND REPAIRED LONGERON IAW REA D853-48497MR AND DC-8 SRM 53-2-0.Dec 8, 2003 · N848AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA030462Fastener · looseCAPTAIN'S EMERGENCY LIGHT UNDER GLARESHIELD WAS LOOSE AND INTERMITTENTLY INOPERATIVE. TIGHTENED LOOSE MOUNTING HARDWARE FOR CAPTAIN'S EMERGENCY LIGHT UNDER GLARESHIELD REF DC-8 MM 20-00.Dec 5, 2003 · N843AX · Doug DC861 · FastenersSDR ABXA040004Longeron · corrodedAFT CARGO AT STA 1180, LONGERON 26 LEFT, LONGERON HAD CORROSION. REMOVED CORROSION, CUT OUT DAMAGED LONGERON, FABRICATED AND INSTALLED REPAIR ANGLES AND WEB SPLICE, ALODINED, AND PRIMED IAW DC-8 SRM 51-1-8, 53-2-0, 53-2-2, 51-1-21, 51-1-20D, AND REA D853-4848Dec 3, 2003 · N848AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA040007Skin · corrodedLEFT WING UPPER XRS 519 - 624 CORROSION AROUND FASTENER HEADS (24 EACH). REPAIRED AREA IAW REA D857-48493MR.Dec 3, 2003 · N848AX · Doug DC861 · Wing, Plate/SkinSDR ABXA040011Skin · crackedL1 FORWARD PAX DOOR, LOWER AFT CORNER HAD A CRACK IN EXTERNAL SKIN. REMOVED DAMAGED AREA, REPAIRED SKIN / DOUBLER TRIM OUT IAW SRM 53-2-0 AND REA D853-48470MR.Dec 3, 2003 · N848AX · Doug DC861 · Passenger/Crew DoorsSDR ABXA040006Skin · crackedCRACK IN OUTER SKIN AT LOWER FORWARD CORNER OF AFT PASSENGER DOOR. REMOVED CRACKED OUTER SKIN, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D AND REA D853-48472MR.Dec 1, 2003 · N848AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA040010Skin · crackedR1 FORWARD SERVICE DOOR, LOWER AFT CORNER HAD A CRACK ON EXTERNAL SKIN. REPAIRED AREA BY FABRICATING REPAIR DOUBLER, FILLERS AND TRIPLERS, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, 53-2-0 AND REA D853-48471MR.Nov 29, 2003 · N848AX · Doug DC861 · Service DoorsSDR ABXA040005Longeron · corrodedAFT CARGO AT STA 1200 - 122 AND LONGERON 28 LEFT HAD CORROSION. REMOVED CORROSION, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 51-1-8, 51-1-20D AND REA D853-48483MR.Nov 28, 2003 · N848AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA040012Frame · corrodedA/C ACCESS COMPARTMENT AT FS 56, BETWEEN LONGERON 35 LT AND 35 RT, FRAME LOWER FLANGE WAS CORRODED. REMOVED CORROSION, FABRICATED REPAIR ANGLE, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 53-2-0 AND REA D853-48484MR.Nov 27, 2003 · N848AX · Doug DC861 · Fuselage Main, FrameSDR ABXA040008Skin · misrepairedL2 DOOR LOWER AFT CORNER HAD A REPAIR THAT DID NOT RESEMBLE SERVICE ENGINEERING SKETCH ES00863. REMOVED DISCREPANT REPAIR, FABRICATED REPAIR DOUBLERS AND FILLER, ALODINED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21, 53-2-0 AND REA D853-48474MR.Nov 26, 2003 · N848AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA040009Skin · damagedR1 DOOR UPPER FORWARD CORNER HAD A REPAIR THAT DID NOT RESEMBLE REWORK DRAWING SR08530021 OR ENGINEERING SKETCH ES00863. REMOVED DOUBLER AND TRIPLER, FABRICATED DOUBLER REPAIR, PRIMED, ALODINED AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0, 51-1-8, 51-1-20D, 51-Nov 25, 2003 · N848AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA040014Skin · crackedR2 AFT SERVICE DOOR, UPPER AFT CORNER HAD CRACK INDICATION. REPAIRED CRACKED AREA, INSTALLED REPAIR DOUBLERS IAW DC-8 SRM 53-2-0 AND REA D853-48479MR.Nov 24, 2003 · N848AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA030417Skin · damagedL1 DOOR FORWARD UPPER CORNER HAD A B-CLASS REPAIR IAW ABX JC NEA 53100102-002. REMOVED EXISTING REPAIR, PERFORMED X-RAY INSPECTION TO CUTOUT. NO CRACKS NOTED. FABRICATED DOUBLERS AND FILLER IAW DC-8 SRM 53-2-0. INSTALLED REPAIR AND REPAIRED AREA IAW DC-8 SNov 5, 2003 · N847AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA030421Skin · damagedL2 LOWER AFT DOOR CORNER HAD A REPAIR THAT DID NOT CONFORM TO SERVICE REWORK DWG SR08530021 OR ENG SKETCH ES00863. REMOVED EXISTING REPAIR AND STRUCTURAL COMPONENTS TO FOM. FABRICATED REPAIR DOUBLERS, ALODINED, PRIMED AND REINSTALLED COMPONENTS IAW DC-8 SRM Nov 4, 2003 · N847AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA030420Skin · crackedL2 AFT PASSENGER LOWER FORWARD DOOR JAMB CORNER HAD CRACKS ON EXTERNAL SKIN AND INTERNAL DOUBLERS, LENGTH RANGE FROM 2 - 4 INCHES APPROXIMATELY. REMOVED DAMAGE FROM AREA, PERFORMED HFEC ON EXTERNAL SKIN AND TITANIUM DOUBLER, NO CRACKS PAST CUTOUT. FABRICATEDNov 3, 2003 · N847AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA030422Skin · damagedR1 DOOR UPPER FORWARD CORNER HAD A REPAIR THAT DID NOT CONFORM TO SERVICE REWORK DRAWING SR08530021 OR ENG SKETCH ES00863. REMOVED EXISTING DOUBLER AND TRIPLER, PERFORMED X-RAY AND ELC INSPECTION, NO CRACKS. FABRICATED DOUBLER AND TRIPLER REPAIR, ALODINED, POct 29, 2003 · N847AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA030419Skin · crackedR1 FORWARD SERVICE DOOR LOWER AFT CORNER HAD CRACK INDICATION ON EXTERNAL SKIN. CUT OUT DAMAGED AREA, PERFORMED HFEC AFTER DAMAGE REMOVAL. NO CRACKS NOTED. FABRICATED DOUBLERS AND FILLER, ALODINED, PRIMED, AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-20DOct 29, 2003 · N847AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA030425Frame · crackedFORWARD CARGO BILGE AREA HAD CRACK ON FRAME FS 240, LONG 34 RIGHT - LONG 35 RIGHT. CUT OUT DAMAGE AND FABRICATED REPAIR ANGLE AND FILLER IAW DC-8 SRM STD5310-02. ALODINED AND PRIMED ANGLE AND FILLER IAW DC-8 SRM 51-1-8. INSTALLED DOUBLER AND FILLER IAW DC-8Oct 26, 2003 · N847AX · Doug DC861 · Fuselage Main, FrameSDR ABXA030424Structure · corrodedVERTICAL STABILIZER REAR SPAR RIGHT CHORD HAD CORROSION AT ZR 270. REMOVED CORROSION AT REAR SPAR RIGHT CHORD, FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 55-2-0 AND REA D855-48068MR.Oct 25, 2003 · N847AX · Doug DC861 · Vertical Stabilizer Miscellaneous StructureSDR ABXA030423Structure · corrodedVERTICAL STABILIZER REAR SPAR LEFT CHORD HAD CORROSION ON AFT LEG BETWEEN ZR 262 AND ZR 268. REMOVED CORROSION ON REAR SPAR LEFT CHORD, FOUND OUT OF LIMITS. FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 55-2-0 AND REA D855-48Oct 25, 2003 · N847AX · Doug DC861 · Vertical Stabilizer Miscellaneous StructureSDR ABXA030379Longeron · crackedRT MAIN LANDING GEAR WHEEL WELL LONGERON 24 AT STA. 875 TO 900 TRIPLER SHOWED EVIDENCE OF CRACK. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-2-2, AND REA D853-48-35MR.Oct 2, 2003 · N853AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA030380Skin · crackedAFT SERVICE DOOR JAMB UPPER AFT CORNER 3 INCHES X 8 INCHES AREA OF LIGHT SURFACE CORROSION AND A .1875 INCH CRACK AT FASTENER HOLE ON EXTERIOR FUSELAGE SKIN. REPAIRED AREA (REMOVED LIGHT SURFACE CORROSION, TRIMMED OUT CRACK, FABRICATED DOUBLERS -19, -21 AND FIOct 2, 2003 · N853AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA030384Bushing · corrodedRIGHT MAIN LANDING GEAR ATTACH FITTING (TRUNION) HAD BROWN GREASE EMITTING FROM LUGS AT FORWARD AND AFT ATTACH POINTS. REMOVED RIGHT MAIN LANDING GEAR IAW DC-8 MM 32-11-01. REMOVED AND REPLACED TRUNION BUSHINGS IAW DC-8 OHM 13-1-6 AND DAC SB 57-45, DC-8 SRM 51Oct 1, 2003 · N853AX · Doug DC861 · Wing, Landing Gear Attach FittingsSDR ABXA030383Strut · corrodedRT MAIN LANDING GEAR CYLINDER FORWARD LUG AFT SIDE HAD EVIDENCE OF CORROSION. CORROSION ON RIGHT MAIN LANDING GEAR CYLINDER WAS OUT OF LIMITS. REPLACED RIGHT GEAR WITH A SERVICEABLE ASSEMBLY. TRANSFERRED BRAKE ASSEMBLY 4 EA. IAW DC-8 MM 32-42-01. TRANSFERRED WOct 1, 2003 · N853AX · Doug DC861 · Main Landing Gear Strut/Axle/TruckSDR ABXA030382Bushing · corrodedLEFT MAIN LANDING GEAR ATTACH FITTING HAD BROWN GREASE EMITTING FROM LUGS AT BOTH ATTACH POINTS. REMOVED LEFT MAIN LANDING GEAR IAW DC-8 MM 32-11-01. REMOVED AND REPLACED TRUNION BUSHINGS IAW DC-8 OHM 13-1-6 AND DAC SB 57-45 AND DC-8 SRM 51-1-8. REINSTALLED LEOct 1, 2003 · N853AX · Doug DC861 · Wing, Landing Gear Attach FittingsSDR ABXA030381Skin · cracked11 EACH HOLES HAD CRACK INDICATION ON RIGHT WING 505F PANEL. REMOVED -19 CLIP, FABRICATED NEW CLIP, ALODINED, PRIMED, INSTALLED IAW DC-8 SRM 51-1-8 AND DWG NR 5613609. FABRICATED EXTERNAL DOUBLER AND INNER DOUBLER IAW REA D857-48044MR, ALODINED, PRIMED AND INSOct 1, 2003 · N853AX · Doug DC861 · Wing, Plate/SkinSDR ABXA030378Support Fitting · corrodedCORROSION ON UPPER CHORD OF CENTER WING REAR SPAR AT PRESSURE BULKHEAD F.S. 855, LEFT BUTT LINE 11 - 21. REMOVED AND INSTALLED BLOWOUT PANEL 3 EA. VERTICAL STIFFENERS, WEB ATTACH ANGLE, DOUBLER, FITTING AND SHEAR WEB ATTACH ANGLE IAW DC-8 SRM 51-30-0 AND 51-1-Oct 1, 2003 · N853AX · Doug DC861 · Wing, Center BoxSDR ARWA20030908Spar Cap · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 4 PYLON LT LOWER SPAR CAP WITH CRACK STA YOP 251 BY ACCESS DOOR NR 411.Sep 8, 2003 · N29UA · Doug DC861 · Nacelle/Pylon, Frame/Spar/RibSDR ARWA20030906Spar Cap · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 2 PYLON LT CENTER SPAR CAP WITH CRACK STA YIP 235.Sep 6, 2003 · N29UA · Doug DC861 · Nacelle/Pylon, Frame/Spar/RibSDR ARWA20030905Angle · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 2 PYLON STUB WING BELOW LT SPAR CAP (Z) ANGLE WITH CRACK.Sep 6, 2003 · N29UA · Doug DC861 · Nacelle/Pylon Miscellaneous StructureSDR ARWA20030904Angle · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON STATION YIP NR 227 RT SIDE ANGLE WITH CRACK.Sep 5, 2003 · N29UA · Doug DC861 · Nacelle/Pylon Miscellaneous StructureSDR ARWA20030903Fitting · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON UPPER SECTION, FRONT SPAR AND FOOT STOOL SPLICE FITTING WITH 3 INCH CRACK.Sep 5, 2003 · N29UA · Doug DC861 · Nacelle/Pylon, Attach FittingsSDR ARWA20030902Web · crackedNR 188. DURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 1 PYLON BETWEEN STATION YOP NR 226 AND STATION YOP NR 243 UPPER WEB DOUBLER WITH CRACKS. CORRECTIVE ACTION:Sep 5, 2003 · N29UA · Doug DC861 · Nacelle/Pylon Miscellaneous StructureSDR ARWA20030907Spar Cap · damagedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 4 PYLON INTERIOR STA YOP 225 LT LOWER SPAR CAP WITH STACK, BY ACCESS DOOR NR 426.Sep 3, 2003 · N29UA · Doug DC861 · Nacelle/Pylon, Frame/Spar/RibSDR ARWA20030804Proximity Sensor · out of adjustDURING FINAL APPROACH, AFTER GEAR EXTENSION, NOSE LANDING GEAR LIGHT DID NOT ILLUMINATED. RETARDING POWER LEVERS CAN'T GET THE AURAL WARNING TO COME ON. EXECUTED GO-AROUND, DURING GO AROUND NOSE LANDING GEAR LIGHT STARTED TO FLICKER. VISUAL INSPECTION OF THAug 19, 2003 · N29UA · Doug DC861 · Landing Gear Position and WarningSDR ABXA030330Element · missingENROUTE , NR 3 ENGINE FIRE WARNING CAME ON. ONLY OTHER INDICATION WAS HIGH OIL TEMP. CREW ELECTED TO USE RT WING OB ENGINE FIRE BOTTLE. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE NR 3 ENGINE. NO EVIDENCE OF FIRE OR FIRE DAMAGE FOUND. DURING INSPECTION, Aug 18, 2003 · N847AX · Doug DC861 · Fire DetectionSDR ABXA030281Battery Pack · dischargedON PREDEPARTURE CHECK FOUND EMERGENCY LIGHT BATTERY RACK DEAD. REPLACED EMERGENCY LIGHT BATTERY RACK ASSSEMBLY. GROUND OPS CHECKED OK IAW AMM 33-50-02.Jul 10, 2003 · N848AX · Doug DC861 · Emergency LightingSDR ARWA20030704Wire · chafedAFTER TAKE-OFF NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED ACCOMPLISHED APPROPRIATE CHECKLISTS, AND RETURNED TO SJU. REMOVED AND CHECKED NR 1 ENGINE MAIN OIL FILTER, FOUND OK. RE-INSTALLED FILTER, FOUND TWO WIRES WERE CHAFING WITH COWLING SPLICE AND RE-ROUTEDJul 9, 2003 · N29UA · Doug DC861 · Engine Oil System WiringSDR ARWA20030604Line · leakingLOSS OF HYDRAULIC FLUID DOWN TO STAND-PIPE. LOSS OF HYDRAULIC CHECK LIST COMPLETED. INSPECTED NR 3 PYLON FOR EVIDENCE OF HYDRAULIC LEAK, FOUND RIGID LINE DAMAGED INSIDE PYLON AREA; REMOVED AND REPLACED RIGID LINE ASSEMBLY AS REQUIRED IAW MM 20-12-0; OPERATIOJun 11, 2003 · N29UA · Doug DC861 · Hydraulic System, MainSDR ARWA20030504Line · leakingDURING CRUISE, LOST HYDRAULIC QUANTITY FOLLOWED THE LOSS OF HYDRAULIC FLUID OR PRESSURE. ABNORMAL OR EMERGENCY CHECKLIST. REMOVED AND REPLACED FLEX HYDRAULIC LINE ON NR 2 ENGINE PER MM 29-10-12. RUN UP CHECK ACCOMPLISHED AS PER MM 71-00-0 NO LEAK FOUND ITMay 14, 2003 · N29UA · Doug DC861 · Hydraulic System, MainSDR ABXA030201Frame · corrodedAFT CARGO STATION 1240, LONGERON 36 FRAME CORRODED. REPAIRED STATION 1240, LONGERON 36 IAW REA D853-46706. INSTALLED INTERCOSTAL, SHEAR TIE, GILLINER ATTACH ANGLE AND GUSSETTS IAW DC-8 SRM 51-1-20D.Apr 21, 2003 · N843AX · Doug DC861 · Fuselage Main, FrameSDR ABXA030202Attach Fitting · crackedTAIL SKID UPPER ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-8 SRM 51-1-20 AND 51-1-21. REMOVED AND REPLACED GILLINER IAW DC-8 SRM 51-1-21.Apr 21, 2003 · N843AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA030199Longeron · crackedAFT CARGO STATION 1270, STRINGER 36, CRACKED. CUT OUT DAMAGED SECTION OF LONGERON, FABRICATED AND INSTALLED LONGERON REPAIR IAW REA D853-46699MR. REMOVED AND REPLACED DAMAGED 3759222-1 SPLICE FITTING IAW REA D853-46699MR.Apr 15, 2003 · N843AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA030200Skin · crackedRIGHT AFT SERVICE DOOR UPPER AFT CORNER HAD CRACK INDICATION. CUT OUT CRACK IAW REA D853-46692MR. FABRICATED REPAIR IAW REA D853-46692MR. INSTALLED REPAIR IAW REA D853-46692MR, DC-8 SRM 51-1-21, 51-1-20D, AND 51-1-11.Apr 15, 2003 · N843AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA030130Controller · defectiveWINDSHIELD HEAT, SPARKS CAME FROM FORWARD RIGHT WINDSHIELD. SPARKS WERE COMING FROM LOWER RIGHT. CIRCUIT BREAKERS WERE PULLED. REPLACED RIGHT WINDSHIELD TEMP. CONTROL DUE TO WINDOW REPLACEMENT IAW DC-8 AMM 30-41-0-1-2-0001. OPS CHECKED GOOD. REPLACED RIGApr 3, 2003 · N849AX · Doug DC861 · Windshield/Door Rain/Ice RemovalSDR ABXA030115Door · missingLEFT MAIN LANDING GEAR LOWER COVER PANEL (FOR STRUT) MISSING ON BPO WALK AROUND. INSTALLED NEW LEFT MAIN LANDING GEAR CENTER DOOR IAW DC-8 MM.Mar 11, 2003 · N848AX · Doug DC861 · Landing Gear Doors
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