Douglas DC-8-61

Service difficulty reports · 942

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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"

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SDR ABXA070086Access Panel · missingON POST FLIGHT FOUND FIRE BOTTLE ACCESS PNL ON PRESS GAGES MISSING. (CENTER INBOARD DOOR ASSEMBLY). INSTALLED TEMPORARY COVER PER REA D857-55548, DEFERRED PER REA D857-55548 FOR MAINT TRACKING IAW ABX GMM 01.07.04 TO BE REPLACED ON OR BEFORE MARCH 30, 2007. Mar 27, 2007 · N847AX · Doug DC861 · Service DoorsSDR ABXA060143Frame · corrodedFOUND CORROSION ON AFT SIDE OF FRAME CAP, STA 70, BETWEEN LONGERON 29 RIGHT AND LONGERON 30 RIGHT IS OUT OF LIMITS. REMOVED EXISTING EXTERNAL DOUBLER AT STA 70 - 101, LONGERON 28 RIGHT - 30 RIGHT. FABRICATED/INSTALLED NEW DOUBLER TO EXTEND PAST STA 70. FABRMar 11, 2006 · N842AX · Doug DC861 · Fuselage Main, FrameSDR ABXA060144Fitting · corrodedWHILE ADDRESSING CORROSION ON AFT SIDE OF FRAME CAP, STA 70, BETWEEN LONGERON 29 RIGHT AND 30 RIGHT, CORROSION WAS FOUND ON THE LONGERON 30 RIGHT END TIE FITTING. IT WAS OUT OF LIMITS. FABRICATED NEW FITTING IAW ABX REA D853-53464, ON ITEM VY-067. FITTING WMar 11, 2006 · N842AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA060135Floorbeam · corrodedFOUND STA 25, RIGHT BUTT LINE 55, MAIN CABIN FLOORBEAM HAD CORROSION. FLOORBEAM IN AREA OF STA 25, RIGHT BUTT LINE 55 REPLACED IAW DC8 SRM 51-1-21 AND 51-1-20D.Feb 28, 2006 · N842AX · Doug DC861 · Fuselage Main, Floor BeamSDR ABXA060133Skin · corrodedFOUND STA 1623 TO 1630, LONGERON 32 RIGHT TO 33 RIGHT, SKIN MATERIAL CORRODED OUT OF LIMITS 36% MATERIAL LOSS (NOTED ON ITEM YY-783, STEP 17). INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0, FIG 1D, 51-2-1, 51-1-8 AND 53-2-1, REF PARTIAL WORKSHEET NR 99.Feb 24, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060142Seat Track · corrodedFOUND CORROSION ON SEAT TRACK MAIN CARGO BAY AT STA 960 - 970, RIGHT BUTT LINE 24, AROUND FASTENERS. OUT OF LIMITS. FIT AND DRILLED TWO NEW SECTIONS OF SEAT TRACK FORM STA 890 TO 990 (PO# 1123125) AND STA 990 TO 1030 (PO# 1068063). TREATED, PRIMED AND INSTAFeb 24, 2006 · N842AX · Doug DC861 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA060115Skin · corrodedSTA 22, OUTBOARD OF LONGERON 31 RIGHT, SKIN AREA WAS OUT OF LIMITS DUE TO CORROSION BLEND OUT, 27% MATERIAL LOSS. FABRICATED SKIN DOUBLER. TREATED, PRIMED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-21, 51-1-8, 53-2-0 AND LWR 20030215.Feb 24, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060134Longeron · corrodedCORROSION FOUND LONGERON 31 RIGHT AROUND OUTBOARD RIVET ROW STA 21.5 WHILE OPENING AREA FOR ITEM YY-882. REMOVED LONGERON 31 RIGHT FROM STA. 10 TO 70. FABRICATED NEW, PO NR 112478, TREATED, PRIMED AND INSTALLED REF. DC8 SRM 51-1-21, 51-1-20D, 51-3-0, 51-1-8 Feb 20, 2006 · N842AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA060117Finger Doubler · corrodedFOUND FORWARD ACCESSORY COMPARTMENT, STA 20, LONGERON 31 RIGHT, FINGER DOUBLER CORRODED. CORROSION REMOVED FROM INTERNAL FINGER DOUBLER BY BLENDING, RESULTING IN LOCALIZED AREAS THAT EXCEEDED ALLOWABLE SRM LIMITS. REPAIR ACCOMPLISHED IAW REA D853-53187.Feb 16, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060104Frame · corrodedCORROSION ON FRAME IN AFT CARGO BAY AT STA 1020, LONGERON 35 LEFT. OUT OF LIMITS. FABRICATED T-BRACKET USING 7075-T6 0.120" X 0.090" THK. FABRICATED DOUBLER USING 7075-T6 0.100" THK. TREATED PRIMED REPAIR PARTS AND INSTALLED IAW DC8 SRM 51-2-0, PG 49, 53-4Feb 16, 2006 · N842AX · Doug DC861 · Fuselage Main, FrameSDR ABXA060139Fitting · corrodedWHILE REMOVING LONGERON 24 RIGHT AT STA 5 - 25 THE END FITTING AT STA 70 WAS NOTED TO HAVE CORROSION. REMOVED AND REPLACED END FITTING. FITTING FABRICATED IAW ABX REA D853-53189 ON ITEM YY-985.Feb 14, 2006 · N842AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA060138Stiffener · corrodedLONGERON STIFFENER INSIDE LONGERON 23 RIGHT, STA 5 - 25 CORRODED BEYOND LIMITS. REMOVED AND REPLACED STIFFENER. FABRICATED NEW STIFFENER FOR LONGERON 23 RIGHT, STA 5 - 25 IAW REA D853-53185 ON CARD YY-977.Feb 14, 2006 · N842AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA060140Stiffener · corrodedWHILE REMOVING LONGERON 24 RIGHT AT STA 5 - 25, A STIFFENER AT STA 8 WAS NOTED TO HAVE CORROSION. REMOVED AND REPLACED STIFFENER AT STA 8 STIFFENER FABRICATED IAW ABX REA D853-53186 ON ITEM YY-978.Feb 14, 2006 · N842AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA060145Skin · corrodedFOUND SHEARED RIVET HEADS STA 95 - 100, RIGHT SIDE ON LONGERON 29. FOUND CORROSION ON SKIN OUT OF LIMITS. REMOVED DAMAGED SKIN AREA, 3" WIDE CENTERED ON LONGERON 29 RIGHT AND FROM STA 84 TO 101. FABRICATED FILLER, DOUBLER AND FINGER DOUBLERS. TREATED AND PFeb 14, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060141Longeron · corrodedFOUND SHEARED RIVET HEADS STA 95 - 100, RIGHT SIDE ON LONGERON 29. FOUND CORROSION ON LONGERON OUT OF LIMITS. REMOVED LONGERON 29 RIGHT FROM STA 86 TO 107. REMOVED PREVIOUSLY REPAIRED SECTION FROM STA 72 TO 86. FIT NEW LONGERON SECTIONS FROM STA 72 TO 89.2Feb 14, 2006 · N842AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA060103Seat Track · corrodedSEAT TRACK SECTION, STA 1500, RIGHT BUTT LINE 46, CORRODED OUT OF LIMITS AROUND SCREW HOLES. REMOVED AND REPLACED SEAT TRACK SECTION IAW DC8 SRM 53-2-3, 51-3-0, 51-1-8, 53-2-0 AND LWR 200302015.Feb 11, 2006 · N842AX · Doug DC861 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA060114Support Fitting · corrodedFOUND STA 25, MAIN CABIN RIGHT SIDE, CUSP LINE, FRAME SUPPORT FITTING CORRODED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.Feb 9, 2006 · N842AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA060113Skin · corrodedFOUND CRACK ON AFT LOWER SKIN OF R1 DOOR CUTOUT, APPROXIMATE STA 190, RIGHT BUTT LINE 67. REMOVED DAMAGED AREA. FABRICATED FILLER 7075-T6 0.063". FABRICATED DOUBLERS, ONE FROM 7075-0, 0.063" AND THE OTHER FROM 7075-0, 0.080". HEAT TREATED DOUBLERS FROM -0 Feb 8, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060137Fitting · corrodedFOUND LOWER AFT CARGO, STA 1230, LONGERON 28 RIGHT, LONGERON BATHTUB FITTING CORRODED OUT OF LIMITS. REMOVED AND REPLACED BATHTUB FITTING IAW DC8 SRM 51-1-21, 51-1-20D, 51-1-8, 51-3-1 AND LWR 200302015.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA060136Longeron · corrodedFOUND CORROSION ON OUTER HORIZONTAL LEG OF LONGERON 33 LEFT AT STA 1240. AFTER REMOVING CORROSION BY LOCALIZED BLENDING, THE AREA WAS OUT OF LIMITS. CUT OUT DAMAGED SECTION AND APPLIED SPLICE REPAIR TO LONGERON 33 LEFT AT STA 1240 IAW REA D853-53188.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA060116Stiffener · gougedSTA 1160, LONGERON 32 RIGHT, AFT CARGO CROSS SLIDE DOOR, LOWER FORWARD DOOR JAMB STIFFENER GOUGED. REMOVED AND REPLACED STIFFENER IAW DC8 SRM 51-1-20D.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Miscellaneous StructureSDR ABXA060111Rib · corrodedTWO BROKEN RIVETS AND BULGED RIB ON TOP OF WING CENTER BOX SECTION STA 759, RIGHT BUTT LINE 50. WEB WAS DISCOVERED TO HAVE EXFOLIATION CORROSION AT 2 LOCATIONS BEHIND RIB. CUT OUT 2 AREAS OF CORROSION ON WEB STA 759, RIGHT BUTT LINE 50 AND RIGHT BUTT LINE 53Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, StructureSDR ABXA060112Frame · corrodedLOWER AFT CARGO, STA 1040, BUTT LINE 0, LOWER FRAME SURFACE CORRODED. REMOVED FASTENERS AND CARGO TRACK TO ACCESS CORROSION SITE. FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS FOR FRAME AND SHEAR TIE IAW DC8 SRM 53-4-1, 53-2-0 AND DC8 SSRM DRAWING K048Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, FrameSDR ABXA060102Frame · corrodedLOWER AFT CARGO STA 1100, LOWER FRAME RIGHT BUTT LINE 5 TO LEFT BUTT LINE 5, SURFACE CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8 AND 53-2-0. OUT OF LIMITS. INSTALLED DOUBLER IAW DC8 SRM 51-1-20.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, FrameSDR ABXA060100Clip · corrodedLOWER AFT CARGO STA 1000 BETWEEN LONGERON 33 RIGHT AND 32 RIGHT, FRAME CLIP CORRODED OUT OF LIMITS. REMOVED CORROSION IAW DC8 SRM 51-1-8. MADE REPAIR IAW REA D853-53274, AND INSTALLED FASTENERS IAW DC8 SRM 51-1-20.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA060101Seat Track · corrodedSEAT TRACK SECTION, STA 1580 TO STA 1620, LEFT BUTT LINE 42, CORRODED OUT OF LIMITS. REMOVED SEAT TRACK SECTION, FABRICATED AND INSTALLED NEW SECTION IAW DC8 SRM 53-2-3, 51-3-0 AND 51-1-11.Feb 7, 2006 · N842AX · Doug DC861 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA060110Doubler · corrodedHEAVY CORROSION IN FORWARD CARGO BILGE AT BASE OF FORWARD BULKHEAD STA. 70, BUTT LINE 0. REMOVED AND REPLACED NOSE JACK PAD DOUBLER AND VERTICAL FRAME ASSEMBLY FOR CORROSION AT STA 70, BUTT LINE 0 IAW DC8 SRM 53-0.Feb 6, 2006 · N842AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060099Fitting · corrodedCORROSION ON LEFT UPPER SIDE WING BOX SECTION, BUTTERFLY FITTING AT STA 683, LEFT BUTT LINE 62. CORRODED OUT OF LIMITS. REMOVED AND REPLACED LEFT UPPER SIDE WING BOX SECTION BUTTERFLY FITTING AT STA 683, LEFT BUTT LINE 62 IAW DC8 SRM 51-1-20D.Feb 6, 2006 · N842AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA060098Pressure Panel · corroded3 RIVET HEADS WERE SHEARED AND METAL WAS BULGING UNDER REINFORCEMENT STRAP, UPPER SURFACE OF RIGHT MAIN LANDING GEAR WHEEL WELL FORWARD OUTBOARD CORNER JUST OUTBOARD OF CEILING SERVICE LIGHT. WEB OUT OF LIMITS AFTER CORROSION REMOVAL MATERIAL LOSS 35%. REMOVFeb 2, 2006 · N842AX · Doug DC861 · Fuselage Main, BulkheadSDR ABXA060097Skin · corrodedCORROSION AROUND FASTENERS ON RIGHT WING, LEADING EDGE, UPPER SURFACE AT XFS 356.00. CORROSION OUT OF LIMITS. FABRICATED REPAIR DOUBLERS AND FILLERS IAW DC8 SRM 57-2-1. INSTALLED REPAIR IAW ABX SSRM K08002.Feb 2, 2006 · N842AX · Doug DC861 · Leading Edge DevicesSDR ABXA060076Longeron · crackedFORWARD CARGO, LONGERON 35 LEFT, CRACKED, FS 250 - 270. INSTALLED LONGERON REPAIR AT FORWARD CARGO FS 250 - 270, LONGERON 35 LEFT IAW RFTS 40033 AND PROJECT E-40463. SPLICE REPAIR INSTALLED IAW DC8 SRM 53-2-2 AT LONGERON 35 LEFT.Dec 9, 2005 · N847AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA050340Battery Pack · inoperativeEMERGENCY EXIT LIGHTS (UNDER GLARESHIELD, OVERHEAD AND CLOSET LIGHTS) VERY DIM. OPS CHECKED ALL LIGHTS, ALL OPS CHECKED GOOD AT THIS TIME IAW DC8 MM.Dec 7, 2005 · N842AX · Doug DC861 · Emergency LightingSDR ABXA050341Battery Pack · dischargedEMERGENCY EXIT LIGHTS STILL DIM AND EMERGENCY HORIZONTAL GYRO LIGHTS DON'T WORK. GYRO FLAGGED WITH BATTERY POWER ONLY. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK IAW DC8 MM. EMERGENCY EXIT LIGHTS OPS CHECKED GOOD. REMOVED AND REPLACED STANDBY Dec 7, 2005 · N842AX · Doug DC861 · Emergency LightingSDR ABXA060073Skin · corrodedFORWARD CARGO FUSELAGE SKIN BULGED, CRACKED, FASTENER SHEARED, EVIDENCE OF EXFOLIATION CORROSION AT PREVIOUS REPAIR, FS 620 - 640, LONGERON 35 LEFT - 36 LEFT. REMOVED CORROSION FORWARD CARGO COMPARTMENT FUSELAGE SKIN IAW DC8 SRM 51-1-8 AT LONGERON 36. INSTALDec 6, 2005 · N847AX · Doug DC861 · Fuselage Main, Plate/SkinSDR ABXA060075Longeron · crackedLEFT MAIN LANDING GEAR WHEEL WELL LONGERON 24, FS 879 HAD A CRACK AT LOWER FASTENER FORWARD SIDE. REMOVED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 53-2-0.Dec 6, 2005 · N847AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA060074Longeron · crackedRIGHT FS 879.375, LONGERON 24, HAD CRACK AT LOWER AREA. STOP DRILLED AND INSTALLED ANGLE REPAIR IAW DC8 SRM 53-2-2.Dec 1, 2005 · N847AX · Doug DC861 · Fuselage Main, Longeron/StringerSDR ABXA050090Indicator · defectiveON TAKEOFF AND CLIMB, NR 3 ENGINE OIL PRESSURE CLIMBED TO 75 - 80 PSI. TOOK THROTTLE TO IDLE, PRESSURE WENT TO 60 PSI. SECURED NR 3 ENGINE. AIR TURN BACK. AFTER SECURING THE ENGINE, THE PRESSURE READ 14 PSI STATIC ON TAXI. REPLACED NR 3 ENGINE OIL PRESSURApr 11, 2005 · N847AX · Doug DC861 · Engine Oil PressureSDR ABXA050068Panel · crackedDURING ROUTINE LINE MAINTENANCE AT ILN, FOUND A 2.250 INCH CRACK IN NR 2 PYLON OUTBOARD PLANK AT STA YN300. REPAIRED PYLON PLANK IAW ABX AIR REA D853-51551-MR USING 17-7 PH .080 INCH, PO 408448907.Mar 5, 2005 · N853AX · Doug DC861 · Nacelle/Pylon, Plate/SkinSDR ABXA040348Bracket · bentDECLARED EMERGENCY, DURING RT TURNS IN FLT AILERONS HARD TO MOVE IN POWERED MODE. WHEN AILERONS DEPOWERED, OPS NORM. FOUND RT FAIRLEAD BRACKET BENT & INTERFERRING WITH CABLE DUE TO BROKEN BUS AILERON CABLE RUNS. REPLACED BRACKET STA RW XRS 380. REPLACED DAOct 5, 2004 · N847AX · Doug DC861 · Aileron Control SystemSDR ABXA040328Compressor · damagedAFTER TURNING ON THE NR 4 CTC, THE AIRCRAFT FILLED WITH A BURNING OIL SMELL. TURNED NR 4 CTC OFF AND SMELL DISSIPATED. NOTE: DID NOT GET AN OVERHEAT LIGHT, RPM'S NORMAL. FOUND NR 4 CTC FAN BLADE DAMAGED. REMOVED AND REPLACED NR 4 CTC. OPS CHECKED GOOD IAWSep 17, 2004 · N847AX · Doug DC861 · Cabin Compressor SystemSDR ABXA040266Window · stickingFIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. REPLACED FIRST OFFICER'S SLIDING WINDOW IAW DC8 56-10-0.Jul 29, 2004 · N842AX · Doug DC861 · Flight Compartment WindowsSDR ABXA040265Spring · brokenDURING MAINTENANCE, FOUND FIRST OFFICER'S WINDOW WAS STUCK. REPLACED SPRING, OPS CHECKED WINDOW. WINDOW DID NOT STICK. PRESSURIZED AIRCRAFT TO 5 PSI DIFF. CHECKED WINDOW AFTER DEPRESSURIZATION. OPENED AND CLOSED NORMALLY.Jul 12, 2004 · N842AX · Doug DC861 · Flight Compartment WindowsSDR ABXA040210Engine · vibrationAT 2000 FEET AND LEVELING OFF, POWER ADVANCED TO MAINTAIN AIRSPEED, HAD SEVERE NR 3 ENGINE VIBRATION. AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT FROM IAD TO ILN. UPON ARRIVAL AT ILN, THE NR 3 ENGINE WAS REPLACED.Jun 17, 2004 · N847AX · Doug DC861 · Engine (Turbine/Turboprop)SDR ABXA040211Spring · brokenDURING MAINTENANCE INSPECTION, FOUND THE FIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. FOUND SPRING BROKEN ON AFT LOWER HOOK. REPLACED SPRING. WINDOW CHECKED GOOD PER DC8 MM 56-10-03.Jun 16, 2004 · N843AX · Doug DC861 · Flight Compartment WindowsSDR ABXA040135Linkage · lack of lubeCOULD NOT MOVE AILERON TRIM WHEEL DURING DESCENT INTO ILN. LUBED AND INSPECTED LT, RT AND WHEEL WELL AILERON LINKAGES. OPERATED AILERON TRIM THROUGH NUMBEROUS TIMES. OPERATED NORMAL.Apr 1, 2004 · N848AX · Doug DC861 · Aileron Control SystemSDR ABXA040117Downlock Switch · corrodedAFTER GEAR EXTENSION, NOSE GEAR GREEN LIGHT DID NOT COME ON. NO RED UNSAFE LIGHT ON. REPLACED BULBS, NO HELP. CREW PERFORMED A GO-AROUND, CYCLED GEAR. VISUALLY CHECKED NOSE GEAR DOWN AND LOCKED, MADE NORMAL LANDING. GEAR PINNED AFTER LANDING AND AIRCRAFT Mar 26, 2004 · N853AX · Doug DC861 · Landing Gear Position and WarningSDR ABXA040109Smoke Detector · defectiveUPPER CARGO FIRE SMOKE SOUNDED IN FLIGHT. ISOLATED TO NR 3 DETECTOR. TESTED NORMAL AFTER LANDING. REPLACED NR 3 SMOKE DETECTOR IAW DC-8 MM 26-10-05-2-0001. OPS CHECKED GOOD.Mar 18, 2004 · N847AX · Doug DC861 · Smoke DetectionSDR ABXA040088Spar Cap · crackedSTA 857 LEFT BUTTLINE 24, SPAR CAP CRACKED. REPAIRED SPAR CAP IAW DC-8 SRM 53-2-5, 51-1-8, 51-1-21, AND 51-3-1.Feb 28, 2004 · N842AX · Doug DC861 · Fuselage Main, StructureSDR ABXA040087Fitting · crackedNR 3 PIT, AFT LOWER CARGO COMPARTMENT AFT DOOR JAMB FITTING WAS FOUND CRACKED DURING A LINE INSPECTION. REPLACED FITTING IAW DC-8 SRM 51-1-20D.Feb 23, 2004 · N853AX · Doug DC861 · Fuselage Main, Attach FittingsSDR ABXA040089Fitting · crackedLEFT LONGERON 23 CRACKED AT STA 920. REPAIRED LONGERON IAW DC-8 SRM 53-2-2, 51-1-8, 51-1-20D, 51-3-1, AND 51-3-0.Feb 15, 2004 · N842AX · Doug DC861 · Fuselage Main, Longeron/Stringer
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