Douglas DC-8-73F

Service difficulty reports · 15,471

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 = 'DC873F'
  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 RRXA000264Pressure Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO PRESSURE PANEL BETWEEN STA 880 TO STA 900 AND BL 69L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-4.Oct 6, 1999 · N605AL · Doug DC873F · Fuselage Main, Plate/SkinSDR RRXA003421Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LONGERON END FITTINGS AT STA 70 L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0.Oct 5, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR RRXA000275Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE AT STA 680 AND BETWEEN LONGERONS 22 RIGHT TO 23 RIGHT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ATTACHMENT Oct 5, 1999 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS99830961Skin · corrodedINSPECTION TYPE:C1, FUSELAGE SKIN AT FS 660 AND 710 WERE CORRODED BEYOND LIMITS. CUT OUT DAMAGED SKIN AND INSTALLED REPLACEMENT SECTION BETWEEN FS 610, FS 780, LONG 31L TO 31R IAW DH SK814-107.Oct 5, 1999 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99830915Angle · crackedINSPECTION TYPE:C1 RT WING L/E OTBD VERTICAL ANGLE AT XS 522.168 IS CRACKED PAST THE STOP DRILL. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 9753297 AND SRM 51-3-0.Oct 5, 1999 · N814UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99830912Tee Chord · crackedINSPECTION TYPE:C1 RT WING L/E AT XS 520.168, THE OTBD SLOT, UPPER TEE CHORD IS CRACKED AT THE OTBD END. STOP DRILLED THE CRACK AND REPAIRED THE TEE CHORD IAW SRM 57-2-0 FIG 2.Oct 5, 1999 · N814UP · Doug DC873F · Wing Miscellaneous StructureSDR UPS99830869Connector · failedINSPECTION TYPE:N/A, RIGHT PACK COMES ON BY ITSELF WITHOUT ANY COOLING. CREW DISCOVERED SMOKE IN THE COCKPIT. *S/D* REPLACED CONNECTOR P1-8001 AND REPAIRED BROKEN WIRE AR-7483255AO PER WDM 21-50, ALL OPERATIONAL CHECKS GOOD.Oct 5, 1999 · N866UP · Doug DC873F · Cabin Cooling SystemSDR RRXA000259Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 30 RIGHT AT STA 25, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON IAW DC-8 SRM 53-2-0.Oct 4, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR 20000522AP007Longeron · corrodedFOUND DURING D-CHECK, UPPER FUSELAGE CABIN, CORROSION AT L30R STATION 25. REMOVED CORROSION, REMOVED LONGERON IAW DC-8 SRM 51-1-8, 53-2-0. FABRICATED LONGERON. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 53-2-2, 51-1-8, 51-1-21. (M)Oct 4, 1999 · N605AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS99830958Skin · crackedINSPECTION TYPE:C1, THE FUSELAGE SKIN AT THE FWD UPPER CORNER OF THE FWD SERVICE DOOR WAS CRACKED. CUT OUT THE DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 53-2-0 FIG 14.Oct 4, 1999 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99830956Skin · crackedINSPECTION TYPE:C1, THE FUSELAGE SKIN AT FS 187, JUST ABOVE THE CUSP AT THE FWD SERVICE DOOR AFT LWR CORNER WAS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 53-2-0 FIG 14.Oct 4, 1999 · N814UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS99830914Doubler · corrodedINSPECTION TYPE:C1 SHEARED FASTENERS AND CORROSION UNDER THE FINGER DOUBLER AT FS 879 TO FS 902, BL 0. REMOVED THE FINGER DOUBLER, REMOVED LIGHT CORROSION FROM WEB IAW SRM 51-1-8, WEB WITHIN LIMITS IAW SRM 53-2-0 FIG 1F. FABRICATED REPLACEMENT FINGER DOUBLEROct 4, 1999 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830913Fitting · crackedINSPECTION TYPE:C1 INTERCOSTAL TO FRAME FITTING CRACKED, FWD SIDE FS 1280 AT LONGERON 33R. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-1-21.Oct 4, 1999 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830911Fitting · crackedINSPECTION TYPE:C1 LONGERON 31L SPLICE FITTING AT FS 470 IS CRACKED. REMOVED AND REPLACED THE SPLICE FITTING IAW SRM 51-1-20D.Oct 4, 1999 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830910Fitting · crackedINSPECTION TYPE:C1 LONGERON 31L SPLICE FITTING AT FS 390 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.Oct 4, 1999 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830954Jamb · crackedINSPECTION TYPE:C1, THE D-PIT DOOR JAMB WEB WAS CRACKED AND CORRODED AT SEVERAL FASTENER HOLES ACROSS THE BOTTOM. CUT OUT THE DAMAGED AREA, FABRICATED REPLACEMENT PARTS, INSTALLED REPLACEMENT PARTS IAW DWG 5641013 AND SRM 51-1-21A.Oct 3, 1999 · N814UP · Doug DC873F · Cargo/Baggage DoorsSDR UPS99830909Splice · corrodedINSPECTION TYPE:C1 LONGERON 32R END FITTING, FWD SIDE OF THE FS 1766 FRAME IS HEAVILY CORRODED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.Oct 3, 1999 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830902Fitting · corrodedINSPECTION TYPE:C1 HEAVY CORROSION ON LONGERON END FITTING, FWD SIDE OF FS 1690 AT LONGERON 22R. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-1-21.Oct 3, 1999 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830901Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 448.581 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0 FIG 2.Oct 3, 1999 · N814UP · Doug DC873F · Wing, Rib/BulkheadSDR UPS99830858Battery Pack · dischargedCOCKPIT EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED BATTERY PACK ASSY. EMERGENCY LIGHT OPS CHECK NORMAL PER MM 33-50-00.Oct 3, 1999 · N867UP · Doug DC873F · Emergency LightingSDR UPS99830823Battery Pack · dischargedW/E COCKPIT EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED BATTERY PACK ASSY, EMERGENCY LIGHTS OPS CKD NORMAL.Oct 3, 1999 · N867UP · Doug DC873F · Emergency LightingSDR RRXA003419Strap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR BEAMS METAL STRIP FOR GILL LINER AT STA 1390, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0.Oct 2, 1999 · N605AL · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000274Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME STA 781 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0.Oct 2, 1999 · N605AL · Doug DC873F · Fuselage Main, FrameSDR UPS99830908Fitting · crackedINSPECTION TYPE:C1 LONGERON 32R END FITTING AT FS 1690 IS HEAVILY CORRODED AND CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-21 AND 51-1-20D AND 51-3-0.Oct 2, 1999 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830900Skin · gougedINSPECTION TYPE:C1 RT WING L/E UPPER SKIN AT XS 246.6 IS GOUGED AND CORRODED AT THE FASTENER HOLE. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW EO DC8-5720-7767-A.Oct 2, 1999 · N814UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830899Fitting · corrodedINSPECTION TYPE:C1 MODERATE CORROSION ON THE LONGERON 18L INTERCOSTAL TO FRAME 822 ATTACH FITTING. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.Oct 2, 1999 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR RRXA000303Frame · crackedDURING A MAINTENANCE VISIT FOUND LEFT HORIZONTAL STABILIZER LEADING EDGE FRAME CRACKED AT XFS 53.75. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-4.Oct 1, 1999 · N605AL · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR 20000424AP033Spar · crackedFOUND DURING D-CHECK, LEFT INBOARD HORIZ STAB L/E CRACK AT FRAME XFS 53.75 UNDER SKIN EXTENDED PAST STOP DRILL. STOP DRILLED CRACK IAW DC-8 SRM 55-2-0. FABRICATED ANGLE REPAIR. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-4 AND 51-1-20D.(M)Oct 1, 1999 · N605AL · Doug DC873F · Horizontal Stabilizer, Spar/RibSDR UPS99830984Skin · corrodedINSPECTION TYPE:C1, LEFT WING L/E UPPER SKIN AT XFS 766.25 & 785.0 WAS CORRODED BEYOND LIMITS. CUT OUT THE DAMAGED AREA AND REPAIRED THE SKIN IAW DH SK814-312.Oct 1, 1999 · N814UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830983Skin · crackedINSPECTION TYPE:C1 L/H WING L/E UPPER SKIN CRACKED AT STA. XFS735.00. REPAIRED AREA I.A.W. SRM 57-2-1 FIG.38.Oct 1, 1999 · N814UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830953Skin · crackedINSPECTION TYPE:C1, LT WING LWR L/E SKIN AT EXTERNAL DOUBLER ABOVE THE NR 2 PYLON WERE CRACKED. REMOVED CRACKED EXTERNAL DOUBLER, NDT VERIFIED SKIN CRACK WAS TERMINATED BY THE EXISTING STOP DRILL. FABRICATED AND INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW SOct 1, 1999 · N814UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830952Skin · crackedINSPECTION TYPE:C1, LT WING L/E UPPER SKIN BETWEEN XFS 703.75 AND 710 WAS CRACKED. STOP DRILLED THE CRACKS AND REPAIRED THE SKIN IAW SRM 57-2-1 FIG 38.Oct 1, 1999 · N814UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830898Fitting · crackedINSPECTION TYPE:C1 CUSP FITTING CRACKED INSIDE RT TORQUE BOX BETWEEN FS 1160 AND 1180. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.Oct 1, 1999 · N814UP · Doug DC873F · Fuselage Miscellaneous StructureSDR UPS99830897Frame · crackedINSPECTION TYPE:C1 FUSELAGE FRAME AT FS 220, JUST ABOVE LONGERON 21R IS CRACKED AT A FASTENER HOLE. CUT OUT DAMAGED AREA AND REPAIRED THE FRAME IAW SRM 53-2-0 FIG 1F.Oct 1, 1999 · N814UP · Doug DC873F · Fuselage Main, FrameSDR UPS99830896Skin · crackedINSPECTION TYPE:C1 LT INBD FLAP OTBD T/E WEDGE SKIN IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FLAP WEDGE SKIN IAW DWG 5642960 AND SRM 51-1-21 AND 51-1-21A.Oct 1, 1999 · N814UP · Doug DC873F · Trailing Edge FlapsSDR UPS99830895Skin · crackedINSPECTION TYPE:C1 RT WING L/E SKIN, AT THE L/E, AT XW 761.5, HAS MODERATE INTERGRANNULAR CORROSION AND IS CRACKED AT 2 FASTENERS. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-0 FIG 2H.Oct 1, 1999 · N814UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830894Skin · crackedINSPECTION TYPE:C1 RT WING L/E UPPER SKIN AT XFS 610.0, 2 FWD OF THE SPAR IS CRACKED. STOP DRILLED CRACK AND REPAIRED THE SKIN IAW EO DC8-5720-7767.Oct 1, 1999 · N814UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830893Skin · crackedINSPECTION TYPE:C1 RT WING L/E LWR SKIN AT XW 257.75, JUST AFT OF THE L/E IS CRACKED AT 2 FASTENERS. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-1 FIG 2H.Oct 1, 1999 · N814UP · Doug DC873F · Wing, Plate/SkinSDR UPS99830892Skin · crackedINSPECTION TYPE:C1 RT WING L/E UPPER SKIN AT XFS 210, 29 FWD OF THE SPAR IS CRACKED. STOP DRILLED THE CRACK AND REPAIRED THE SKIN IAW EO DC8-5720-7767.Oct 1, 1999 · N814UP · Doug DC873F · Wing, Plate/SkinSDR RRXA000284Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 400 BETWEEN LONGERON 22 LEFT TO 23 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RETURN TO SERVICE, LIMITS ACCEPTABLE IAW FAA DER APPROVESep 30, 1999 · N605AL · Doug DC873F · Fuselage Main, Attach FittingsSDR 20000522AP026Fairing · crackedFOUND DURING D-CHECK, D PIT AFT DOOR FRAME FAIRING CRACKED. REMOVED FAIRING. FABRICATED FAIRING IAW DC-8 SRM 51-1-4. TREATED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-8, 51-3-0. (M)Sep 30, 1999 · N605AL · Doug DC873F · Aerodynamic FairingsSDR UPS99830951Frame · crackedINSPECTION TYPE:C1, FUSELAGE FRAME AT FS 55 WAS CRACKED AT THE ATTACH ROD AT LONG 24R. CUT OUT DAMAGED AREA AND REPAIRED THE FRAME IAW SRM 53-2-0 FIG 2.Sep 30, 1999 · N814UP · Doug DC873F · Fuselage Main, FrameSDR UPS99830891Frame · crackedINSPECTION TYPE:C1 FUSELAGE FRAME AT FS 55 AT LONGERON 24L IS CRACKED AT THE ATTACH ROD. CUT OUT DAMAGED AREA AND REPAIRED THE FRAME IAW SRM 53-2-0 FIG 2.Sep 30, 1999 · N814UP · Doug DC873F · Fuselage Main, FrameSDR RRXA991478Fitting · crackedDURING A POST-FLIGHT, FOUND RIGHT WING INBOARD AILERON HINGE FITTING CRACKED BEYOND LIMITS. REMOVED CRACKED FITTING, RECEIVED NEW FITTING AND INSTALLED IAW DC-8 MM CHAPTER 57. OPERATIONS CHECKS GOOD.Sep 30, 1999 · N604AL · Doug DC873F · Trailing Edge FlapsSDR RRXA000271Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SHEAR TIE AT STA 60 AND LONGERON 6 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FRAME TIE IAW DC-8 SRM 53-2-2.Sep 29, 1999 · N605AL · Doug DC873F · Fuselage Internal Mounting StructureSDR 20000427AP003Fairing · crackedFOUND DURING D-CHECK, D PIT FORWARD DOOR FRAME, FAIRING CRACKED. REMOVED FAIRING. FABRICATED FAIRING IAW DC-8 SRM 51-1-4. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-3-0. (M)Sep 29, 1999 · N605AL · Doug DC873F · Aerodynamic FairingsSDR UPS99830804Smoke Detector · inopNR 6 CARGO SMOKE DETECTOR IS INOP. REPLACED NR 6 SMOKE DETECTOR TEST LAMP WITH PRO PER CM327AS15 LAMP TESTS GOOD.Sep 29, 1999 · N809UP · Doug DC873F · Smoke DetectionSDR UPS99830815Air Dist · smokeUPON TAXI, CREW DETECTED SMOKE IN COCKPIT AFTER PREF CHECK WAS ACCOMPLISHED, SUSPECT ELECTRICAL. PERFORMED A/C GENERATOR MAINT PRACTICES IAW MM 24-20-00. ALL CHECKS GOOD, NO EVIDENCE OF SMOKE IN COCKPIT. AIRCRAFT OK FOR SERVICE.Sep 28, 1999 · N868UP · Doug DC873F · Air Distribution SystemSDR UPS99830748Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK.Sep 28, 1999 · N866UP · Doug DC873F · Emergency LightingSDR RRXA000270Bracket · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO 2 EACH BRACKETS AT STA -131 AND LONGERON 23 LEFT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0.Sep 27, 1999 · N605AL · Doug DC873F · Fuselage Main, Attach Fittings
Back to Douglas DC-8-73F