Douglas DC-8-73F

Service difficulty reports · 15,471

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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 = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR RRXA11369Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING MID L/E UPPER RIB TIP CRACKED STA 480. *** CORRECTIVE ACTION *** REMOVED FASTENER PER SRM 51-1-21. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. NDT DETERMINED CRACK TEMINATED AT STOP DRILL PER SPM 06-10-01.001, FABRICATJun 23, 2001 · N873SJ · Doug DC873F · Wing Main, Frame StructureSDR RRXA11368Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING MID L/E UPPER RIB TIP CRACKED STA XS 473.5. *** CORRECTIVE ACTION *** REMOVED FASTENER PER SRM 51-1-21 STOP DRILLED CRACK PER SRM 57-2-0 FIG 2, NDT DETERMINED CRACK TERMINATES AT STOP DRILL PER SRM 06-10-01.001. FABJun 23, 2001 · N873SJ · Doug DC873F · Wing Main, Frame StructureSDR RRXA11367Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING MID L/E UPPER RIB TIP CRACKED AT STA XS461. *** CORRECTIVE ACTION *** REMOVED FASTENER PER SRM 51-1-21. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2 PG 9 NOT VERIFIED CRACK TERMINATES AT STOP DRILL PER SPM0G10-01.001. FAJun 23, 2001 · N873SJ · Doug DC873F · Wing Main, Frame StructureSDR RRXA11319Doubler · chafedDURING A MAINTENANCE VISIT FOUND CHAFF DAMAGE TO NR 3 ENGINE I/B FAN COWL INNER DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 71-2-8 PAR.5C.Jun 23, 2001 · N606AL · Doug DC873F · Engine Cowling SystemSDR RRXA11318Vane · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LT WING NR 1 FLAP VANE FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTAKLLED IAW DC-8 MM 27-51-10.Jun 23, 2001 · N606AL · Doug DC873F · Trailing Edge FlapsSDR DHL2001801007Control Unit · malfunctionedAT CRUISE ALT IN BOTH MANUAL AND AUTO PRESSURIZATION AND AT ALL FLOW SETTINGS, CABIN CLIMBS AND DESCENDS UP TO 700 FPM AND WILL NOT STABILIZE AT CONSTANT PRESSURE. INSP OUTFLOW VALVE OPERATION, NO DEFECTS NOTED. PRESSURIZED A/C TO 7 PSI ON GROUND, DECAY CHECJun 22, 2001 · N801DH · Doug DC873F · Cabin Pressure Control SystemSDR RRXA11366Doubler · separatedDURING A MAINTENANCE VISIT FOUND RT WING L/E OB L/E HAS FASTENER PULLING THROUGH SKIN STA XW485. REPAIR DAMAGE AREA IAW DC8 SRM 51-1-21, 51-1-20 AND DHSK 873-917Jun 22, 2001 · N873SJ · Doug DC873F · Wing, Plate/SkinSDR RRXA11365Skin · corrodedDURING A MAINTENANCE VISIT FOUND R/H WING L/E SKIN DISBONDED & CORROSION AT XFS 300. *** CORRECTIVE ACTION *** REMOVED CORROSION, THICKNESS 0.82 - 0.88, MATERIAL LOSS WITHIN LIMITS. TREATED AND PRIMMED IAW SRM 51-1-8 AND 57-5-0 FIG 7 RESPECTIVELYJun 22, 2001 · N873SJ · Doug DC873F · Wing StructureSDR UPS01836166Slide · out of positionINSPECTION TYPE:N/A DEPARTURE-ESCAPE SLIDE GIRT BAR WOULD NOT LOCK IN PLACE. *S/D* REPACKED SLIDE, OPS CHECKS GOOD REF M217781.Jun 22, 2001 · N852UP · Doug DC873F · Escape SlideSDR UPS01836169Module · defectiveINSPECTION TYPE:N/A EMERGENCY LIGHT MODE PANEL UNARMED STAYS ON IN ARMED POSITION. FOUND PANEL DEFECTIVE REPLACED EMERGENCY LIGHTS MODULE AND OPS CHECKS NORMAL.Jun 22, 2001 · N840UP · Doug DC873F · Emergency LightingSDR RRXA11364Rib · crackedDURING A MAINTENANCE VISIT FOUND L/H WING CENTER L/E STA XFS 310 RIB CRACKED AFT UPPER END. *** CORRECTIVE ACTION *** REPAIRED RIB IAW DC8 SRM 57-2-0 FIG 2Jun 21, 2001 · N873SJ · Doug DC873F · Wing Main, Frame StructureSDR RRXA11325Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FITTING AT STA.270 AND L30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D.Jun 21, 2001 · N606AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11316Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H FLAP BASE FITTING AT STA.339, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 27-2-4Jun 21, 2001 · N606AL · Doug DC873F · Aileron Control SystemSDR RRXA11317Fitting · damagedDURING A MAINTENANCE VISIT FOUND ELONGATION DAMAGE TO A-PIT CROSS SLIDE TORQUE BOX BATH TUB FITTING HOLES AT STA.320 AND L29L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRJun 21, 2001 · N606AL · Doug DC873F · Fuselage Main, Attach FittingsSDR RRXA11315Doubler · damagedDURING A MAINTENANCE VISIT FOUND SCREWS PULLING THRU INBOARD END OF L/H INBOARD SLOT VANE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1Jun 21, 2001 · N606AL · Doug DC873F · Leading Edge Slat Control SystemSDR UPS01836175Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01, OPS CHECKS GOOD.Jun 21, 2001 · N866UP · Doug DC873F · Emergency LightingSDR UPS01836157Fan · failedINSPECTION TYPE:N/A, STRONG ELECTRICAL BURNING SMELL SUSPECTED PACK SMOKE. WITH LEFT PACK AND RECIRC FAN OFF SMELL DISSIPATED. RAN ALL 4 ENGINES, OPERATED BOTH PACKS PER MM 21-55-00. NO ABNORMALITIES NOTED. FOUND RECIRC FAN INOP AND TO BE SOURCE OF ODOR. Jun 21, 2001 · N880UP · Doug DC873F · Air Distribution FanSDR UPS01836161Access Panel · looseINSPECTION TYPE:N/A PASSING 12,000 FEET LOUD BANG FROM RT FRONT SIDE OF AIRCRAFT FOLLOWED BY AIRCRAFT DEPRESSURIZATION. SUSPECT HAIL STORM PRIOR TO TAKEOFF EMERGENCY ACCESS FOR F/O SLIDING WINDOW DISLODGED RE-INSTALLED ACCESS PNL, OK FOR CONTINUED SERVICE.Jun 21, 2001 · N840UP · Doug DC873F · Fuselage Main, Plate/SkinSDR DHL2001806002Mount · crackedASYMMETRICAL FLAP CONDITION ON APPROACH OUTER NEEDLE FAILED TO EXTEND, PASSED 23. ROLL TENDENCY FELT. EMERGENCY DECLARED. FOUND RT INBOARD ACT MOUNT LUG CRACKED. INSPECTED AREA, NO OTHER DAMAGE NOTED. REMOVED AND REPLACED ACT ASSY IAW 27-59-9. SERVICED AJun 21, 2001 · N806DH · Doug DC873F · Trailing Edge Flap ActuatorSDR RRXA11385Skin · crackedDURING A MAINTENANCE VISIT FOUND EMPENNAGE EXT SKIN CRACKED LT SIDE AT STA 1903, UPPER SIDE HORIZONTAL STAB. REMOVED AND REPLACED SKIN IAW SRM 51-1-20, 51-1-11, FABRICATED SKIN IAW SRM 53-5-3 FIG 2Jun 20, 2001 · N873SJ · Doug DC873F · Horizontal Stabilizer, Plate/SkinSDR RRXA11384Filler · crackedDURING A MAINTENANCE VISIT FOUND R/H O/B AILERON UPPER ACCESS FOR THE O/B DAMPERS HAS TORN SKIN AT CUTOUT PERIMETER. *** CORRECTIVE ACTION *** FABRICATED AND INSTALLED FILLERS IAW DHSK 873-670, SRM 51-1-5, 51-1-11, 51-1-21Jun 20, 2001 · N873SJ · Doug DC873F · Aileron Control SystemSDR RRXA11363Fitting · crackedDURING A MAINTENANCE VISIT FOUND C PIT FITTING FWD SIDE FRAME 1160 L35R IS CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED PN 3758496-2N PER 51-1-20DJun 20, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11362Fitting · crackedDURING A MAINTENANCE VISIT FOUND C PIT FITTING FWD SIDE OF FRAME 1172 L35L CRACKED AT TOP FLANGE. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW DWG 3758570, AND DC8 SRM 53-1-0 AND 51-1-20 D.Jun 20, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11361Skin · gougedDURING A MAINTENANCE VISIT FOUND FUSELAGE EXT SKIN STA 1690 L18L GOUGED. REPAIRED SKIN IAW 8110-3 APPROVED DH S/L 873-133Jun 20, 2001 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11314Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT BATH TUB FITTING AT STA.310 AND L32R-L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8Jun 20, 2001 · N606AL · Doug DC873F · Standard Practices/StructuresSDR RRXA11313Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO L/H WING LWR T/E PANEL INBOARD OF FLAP HINGE AT STA.219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLJun 20, 2001 · N606AL · Doug DC873F · Wing Main, Frame StructureSDR RRXA11312Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H UPPER SKIN FORWARD OF CENTER SPAR AT STA. XRS-6 TO XRS20, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSJun 20, 2001 · N606AL · Doug DC873F · Wing, Plate/SkinSDR RRXA11310Stiffener · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO HORIZONTAL STIFFNERS IN RT MLG W/W AT STA.980, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG 5640915.Jun 20, 2001 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA11309Stiffener · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO HORIZONTAL STIFFNERS IN RT MLG W/W AT STA.980, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG 5640915.Jun 20, 2001 · N606AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA11360Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING CENTER L/E XFS 393 RIB CRACKED UPPER AFT END. *** CORRECTIVE ACTION *** REPAIRED RIB IAW DC8 SRM 57-2-0 FIG 2Jun 19, 2001 · N873SJ · Doug DC873F · Wing Main, Frame StructureSDR RRXA11359Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING CENTER L/E STA XFS 372 CRACKED UPPER AFT END. *** CORRECTIVE ACTION *** REPAIRED RIB IAW DC8 SRM 57-2-0 FIG 2Jun 19, 2001 · N873SJ · Doug DC873F · Wing Main, Frame StructureSDR RRXA11358Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING CENTER L/E RIB STA XFS 397 CRACKED UPPER AFT END. *** CORRECTIVE ACTION *** REPAIRED RIB IAW DC8 SRM 57-2-0 FIG 2Jun 19, 2001 · N873SJ · Doug DC873F · Wing Main, Frame StructureSDR RRXA11357Angle · crackedDURING A MAINTENANCE VISIT FOUND R/H CABIN CUSP FWD END CUSP ANGLE CRACKED. *** CORRECTIVE ACTION *** REPAIRED CUSPANGLE IAW DC8 SRM 53-2-0 FIG 1B, LOWER SIDE STA 825 LONG 21R.Jun 19, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA011048Skin · corrodedAFTER LANDING DISCOVERED CORROSION ON OUTER FUSELAGE, LEFT LOWER SIDE AT FS 1320.Jun 19, 2001 · N791FT · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS01836268Splice · crackedINSPECTION TYPE:X2 FWD CARGO PIT AT FS 600-620 LONG 31R SPLICE FITTING CRACKED. REMOVED SPLICE FITTING DRILLED NEW FITTING IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.Jun 19, 2001 · N851UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836267Splice · crackedINSPECTION TYPE:C2 AFT PIT FS 1270 L35L SPLICE FITTING IS CRACKED. REMOVED SPLICE IAW DC8 SRM 51-1-20D, FOUND LONGERON SPLICE FITTING CRACKED. RCVD NEW SPLICE PN 3759253-1N LOCATED, DRILLED AND DEBURRED FITTING IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-Jun 19, 2001 · N851UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS01836262Frame · corrodedINSPECTION TYPE:C2 FWD CARGO PIT AT FS 200 ABOVE LONG 36 FRAME IS CORRODED AT LONGERON ATTACH FITTINGS. REMOVED CORROSION IAW DC8 SRM 51. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0.Jun 19, 2001 · N851UP · Doug DC873F · Fuselage Main, FrameSDR UPS01836218Hinge · crackedINSPECTION TYPE:C2 AFT PIT C3 RAMP PANEL FOLDING DOOR HINGE IS CRACKED. REMOVED AND REPLACED HINGE (REP) DC8 SRM 51-3-2, 51-3-0.Jun 19, 2001 · N851UP · Doug DC873F · Cargo/Baggage DoorsSDR DHL2001804011Autopilot Sys · malfunctionedA/P EXCEEDS 30 DEG BANK IN HEADING SELECT MODE ON F/O SIDE. PERFORMED OPS CHECK OF A/P HEADING SELECT MODE. CHECKS OK BOTH SIDES IAW 22-10-0 PG 206 STEP H.Jun 19, 2001 · N804DH · Doug DC873F · Autopilot SystemSDR DHL2001804010Autopilot Sys · malfunctionedA/P TRACKS 1-1/2 DOTS LOW COUPLED ON F/O SIDE ON G/S. PERFORMED OPS CHECK OF A/P LOCALIZER AND GLIDE PATH. CHECKS OK BOTH SIDES IAW 22-10-0 PG 207.Jun 19, 2001 · N804DH · Doug DC873F · Autopilot SystemSDR RRXA11356Skin · corrodedDURING A MAINTENANCE VISIT FOUND RT WING UPPER SURFACE CORROSION FWD O/B AILERON O/B END. XRS 763 TO XRS 764. REPAIR DOUBLER PER SRM 57-2-0 FIG 2A AND DWG 5763353Jun 18, 2001 · N873SJ · Doug DC873F · Wing, Plate/SkinSDR RRXA11308Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT CROSS SLIDE DOOR JAMB FLOOR SUPPORT AT STA.280 AND L32L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 5Jun 18, 2001 · N606AL · Doug DC873F · Fuselage Main, FrameSDR RRXA11307Splice · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA.1020 AND L30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0,Jun 18, 2001 · N606AL · Doug DC873F · Fuselage Structure (General)SDR RRXA11306Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATH TUB FITTING AT STA.315-340 AND L32R-L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SJun 18, 2001 · N606AL · Doug DC873F · Standard Practices/StructuresSDR RRXA11355Skin · corrodedDURING A MAINTENANCE VISIT FOUND WHILE REMOVING CORROSION N/R 85131 FOUND AREA OUT OF LIMIT IAW SRM51-1-8, 53-2-0 FIG 1F. FABRICATED REPLACEMENT PART AND INSTALLED IAW DHSK 873-702.Jun 17, 2001 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11354Skin · corrodedDURING A MAINTENANCE VISIT FOUND WHILE REMOVING CORROSION AT STA 1500 L21L, FOUND AREA OUT OF LIMITS IAW SRM 51-1-8, 53-2-0 FIG 1F. FABRICATED REPLACEMENT PART AND REPAIR PER DHSK 873-702Jun 17, 2001 · N873SJ · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA11353Skin · gougedDURING A MAINTENANCE VISIT FOUND EMPINNAGE SKIN L/H SIDE OF #60 PANEL HAS A GOUGE WITH FILLER IN PORTIONS OF IT. FROM LONG 26L TO 36 STA 1781 TO 1793. *** CORRECTIVE ACTION *** REMOVED FILLER AND FASTENER PER SRM 51-1-21, CUT OUT DAMAGE PER SRM 53-2-0 FIG 1DJun 17, 2001 · N873SJ · Doug DC873F · Fuselage Main, StructureSDR RRXA11305Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA.1100 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20A&D, 51-1Jun 17, 2001 · N606AL · Doug DC873F · Fuselage Main, StructureSDR RRXA11304Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BATH TUB FITTING AT STA.313 AND L33R-L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-Jun 17, 2001 · N606AL · Doug DC873F · Standard Practices/StructuresSDR UPS01836126Window · out of adjINSPECTION TYPE:N/A, F/O SLIDING WINDOW WOULD NOT OPEN. ADJUSTED WINDOW.Jun 17, 2001 · N894UP · Doug DC873F · Flight Compartment Windows
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