Douglas DC-8-71F

Service difficulty reports · 8,938

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 = 'DC871F'
  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 UPS96820366Skin · crackedINSPECTION TYPE: CS2. RUDDER RT SIDE AT LEADING EDGE SKIN CRACKED AT SECOND HINGE POINT CUTOUT LOWER SKIN. REPLACED RUDDER ASSY PER T/C S55-682-44.Jun 3, 1996 · N705UP · Doug DC871F · Rudder, Plate/SkinSDR UPS96820365Skin · crackedINSPECTION TYPE: CS2. RUDDER LEADING EDGE LT SIDE CRACKED AT SECOND HINGE POINT CUTOUT LOWER SKIN. REPLACED RUDDER ASSY PER T/C S55-682-44.Jun 3, 1996 · N705UP · Doug DC871F · Rudder, Plate/SkinSDR UPS96820361T Fitting · crackedINSPECTION TYPE: C. KEEL BEAM LOWER SURFACE 3 EA T-FITTINGS CRACKED AT FS 900, FS 940 AND FS 950. REPLACED FITTINGS PER SRM 51-1-20D.Jun 3, 1996 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96820516Beltframe · corrosionINSPECTION TYPE CS2, HEAVY CORROSION ON BELTFRAME AT FS 1400 ABOVE LONGERON 35R. REPAIRED FRAME PER SRM 53-2-0.Jun 2, 1996 · N705UP · Doug DC871F · Fuselage Main, FrameSDR UPS96820513Angle · corrosionINSPECTION TYPE CS2, MAIN CABIN HEAVY INTERGRANULAR CORROSION ON LONG 21R, FS 1625 ON ANGLE. REPLACED ANGLE PER SRM 51-1-20D.Jun 2, 1996 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96820512Floor Beam · corrosionINSPECTION TYPE CS2, HEAVY CORROSION ON FLOOR BEAM FS 1280, LEFT TUNNEL AREA LBL 57. REPAIRED PER UPS EO.Jun 2, 1996 · N705UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS96820398Rib · crackedINSPECTION TYPE: CS2. LT HORIZONTAL STABILIZER LEADING EDGE INBOARD UPPER RIB IS CRACKED. REPAIRED RIB PER SRM 55-2-0.Jun 2, 1996 · N705UP · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR UPS96820472Doubler · corrosionINSPECTION TYPE CS2, HEAVY CORROSION ON FUSELAGE SKIN STA 1644 BETWEEN LONGERONS 29R AND 30R ON INNER DOUBLER. REPLACED INNER DOUBLER PER SRM 51-1-21.Jun 1, 1996 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96820470Skin · corrosionINSPECTION TYPE CS2, RUDDER LT SIDE HEAVY CORROSION JUST ABOVE THE TAB. REPLACED RUDDER ASSY ON N/R TASK NR 463759 AND ROUTINE T/C NR S55- 682-44.Jun 1, 1996 · N705UP · Doug DC871F · Rudder, Plate/SkinSDR UPS96820364Rib · crackedINSPECTION TYPE: CS2. RT WING LEADING EDGE 5 EA UPPER RIBS CRACKED AT STA XFS635, XFS641, XFS654, XFS660 AND XFS672. REPAIRED RIBS PER MM 57-00-00, PG 801.Jun 1, 1996 · N705UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS96820363Rib · crackedINSPECTION TYPE: CS2. RT WING LEADING EDGE 3 EA LOWER RIBS CRACKED AT STA XFS672, XFS804 AND XFS822. REPAIRED PER MM 57-00-00, PG 801.Jun 1, 1996 · N705UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS96820362Rib · crackedINSPECTION TYPE: CS2. RT WING LEADING EDGE 6 EA UPPER RIBS CRACKED AT STA XFS728, XFS766, XFS772, XFS804, XFS810, XFS816. REPAIRED PER MM 57-00-00, PG 801.Jun 1, 1996 · N705UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS96820399Doubler · crackedINSPECTION TYPE: CS2. DOUBLER CRACKED AT FUSELAGE SKIN MAIN CARGO DOOR AFT JAMB 20 FROM AFT UPPER CORNER. REPLACED DOUBLER PER SRM 51-1-21A.May 31, 1996 · N705UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96820507Skin · delaminatedINSPECTION TYPE CS2, RT WING NR 4 SPOILER DELAMINATED ON LOWER INBD AFT CORNER. REPLACED SPOILER ASSY PER MM 27-61-01.May 30, 1996 · N705UP · Doug DC871F · Drag Control SystemSDR RRXA96103Bulkhead Cap · corrodedLOWER BULKHEAD CAP AT Y=8, BETWEEN LONGERONS 32R AND 33R CORRODED AND CRACKED. LOWER BULKHEAD CAP REPAIRED BY DOUBLER REPAIR IAW REO 01903, SRM 51-1-20D AND TREATED IAW DC-8 SRM 51-1-8.May 16, 1996 · N8076U · Doug DC871F · Fuselage Main, BulkheadSDR RRXA96102Bulkhead Cap · corrodedLOWER BULKHEAD CAP AT Y=70, BETWEEN LONGERONS 31R AND 33R CORRODED AND CRACKED. LOWER BULKHEAD REPAIRED BY DOUBLER REPAIR SECURED WITH HL329-6 HI-LOCKS IAW REO 01903, SRM 51-1-20D, AND TREATED IAW SRM 51-1-8.May 16, 1996 · N8076U · Doug DC871F · Fuselage Main, BulkheadSDR UPS96820103Battery Pack · dischargedINSPECTION TYPE: C. COCKPIT EMERGENCY EXIT LIGHTS FAIL TO ILLUMINATE WHEN TESTED. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT BATTERY PACK.May 14, 1996 · N779UP · Doug DC871F · Emergency LightingSDR UPS96820091Skin · crackedINSPECTION TYPE 'B', 3 CRACKS IN SKIN PROTRUDING FROM RIVETS IN BELLY SKIN 3 INCHES AFT OF LT AFT NOSE WHEEL WELL DOOR. INSTALLED DOUBLER PER SRM 53-2-1.May 10, 1996 · N715UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS96820090Skin · crackedINSPECTION TYPE 'B', CRACK PROTRUDING FROM RIVET HEAD OUTBOARD AND FWD PANEL 523, FIRE BOTTLE ACCESS MARKED. REMOVED CRACKED AREA OF THE SKIN. INSTALLED FILLER AND DOUBLER PER SRM 57-2-1.May 10, 1996 · N715UP · Doug DC871F · Wing, Plate/SkinSDR UPS96820062Engine · flame-outINSPECTION, NR 1 ENGINE FLAMED OUT IN FLIGHT. NR 1 ENGINE OVER PRESSURE LIGHT REMAIN'S ILLUMINATED. PERFORMED TROUBLESHOOTING PROCEDURES PER MM 71-00-00 PAGE 153-169, NO ABNORMALITIES NOTED.May 8, 1996 · N730UP · Doug DC871F · Engine (Turbine/Turboprop)SDR IXXA9678Telescoping Link · not latchedON DEPARTURE OUT OF BFI, THE RIGHT NLG DOOR DID NOT CLOSE AFTER GEAR RETRACTION. THE GEAR WAS CYCLED, BUT THE PRESENCE OF THE BUFFETING FROM THE DOOR INDICATED THAT IT WAS STILL OPEN. THE AIRCRAFT RETURNED TO BFI FOR MAINTENANCE. AT BFI THE NOSE GEAR DOORS May 8, 1996 · N828BX · Doug DC871F · Landing Gear Door Retract SectionSDR RRXA96115Frame · corrodedFRAME AT Y=1440 AND LONGERON 33R CORROSION DAMAGE PAST LIMITATIONS AFTER BLEND-OUT. REPAIRED FRAME BY INSTALLING A SPLICE REPAIR IAW REO-01936 AND TREATED AREA DC-8 IAW SRM 51-1-8.May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA96114Longeron · corrodedLONGERON 34R BETWEEN Y=1040 AND Y=1445 CORROSION DAMAGE PAST LIMITATIONS. REPAIRED LONGERON 34R BY STRAP REPAIR IAW REO-01937 AND TREATED AREA IAW DC-8 SRM 51-1-8.May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA96113Skin · corrodedINTERNAL SKIN AT Y=1120 AND LONGERON 36 CORRODED PAST LIMITATIONS. REPAIRED INTERNAL SKIN BY BLEND-OUT IAW REO-01938 AND TREATED AREA IAW DC-8 SRM 51-1-8.May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA96112Skin · corrodedINTERNAL SKIN AT Y=1080 AND LONGERON 36 CORRODED PAST LIMITATIONS. REPAIRED SKIN BY BLEND-OUT IAW REO-01933 AND TREATED AREA IAW DC-8 SRM 51-1-8.May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA96111Frame · corrodedFRAME AT Y=980 BETWEEN LONGERONS 33L AND 33R CORROSION BLENDED OUT PAST LIMITATIONS. FRAME REPAIRED BY USING 2 ANGLES USED AS DOUBLER SUPPORTS AND ONE ANGLE DOUBLER FOR STIFFENER IAW RFTTS ENGINEERING DISPOSITION 24-28787, SRM 53-2-0 AND TREATED AREA IAW SRM May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA96110Frame · corrodedFRAME AT Y=600 AND LONGERON 31L CORROSION DAMAGE PAST LIMITATIOINS AFTER BLEND-OUT. FRAME REPAIRED BY SPLICE REPAIR IAW REO-01932 AND TREATED IAW DC-8 SRM 51-1-8.May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA96109Longeron · corrodedLONGERON 29L AT Y=500, CORRSION DAMAGE PAST LIMITATIONS AFTER BLEND-OUT. REPAIRED LONGERON 29L BY DOUBLER REPAIR IAW REO-01927, SRM 53-4-1 AND TREATED AREA IAW DC-8 SRM 51-1-8.May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA96108Frame · corrodedFRAME AT Y=319 AND LONGERON 29R CORROSION DAMAGE PAST LIMITATIONS. REPAIRED FRAME BY INSTALLING A STRAP REPAIR IAW REO-01935, SRM 53-4-1 AND TREATED AREA IAW DC-8 SRM 51-1-8.May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA96107Longeron · corrodedLONGERON 31L BETWEEN Y=70 AND Y=80 CORROSION DAMAGE PAST LIMITATIONS. REPAIRED LONGERON 31L BY REMOVING 10 INCHES OF DAMAGE AREA AND INSTALLED SPLICE, DOUBLER AND FILLER REPAIR IAW REO-01929 AND TREATED AREA IAW DC-8 SRM 51-1-8.May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA96106Skin · corrodedSKIN AT Y=980 AND Y=1020 BETWEEN LONGERONS 36 TO 35L CORROSION DAMAGE PAST LIMITATIONS. SKIN REPAIRED BY DOUBLER AND FILLER REPAIR IAW REO-01946 AND TREATED AREA IAW DC-8 SRM 51-1-8.May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA96105Bulkhead · corrodedBULKHEAD CAP AT Y=70 BETWEEN LONGERONS 28L TO 28R CORROSION DAMAGE. BULKHEAD CAP REPAIRED BY DOUBLER AND FILLER REPAIR IAW REO-01930 AND TREATED AREA IAW DC-8 SRM 51-1-8.May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, BulkheadSDR RRXA96104Skin · corrodedINTERNAL SKIN AT Y=1050 AND Y=1060 BETWEEN LONGERONS 35R AND35L CORROSION PAST LIMITATIONS. REPAIRED INTERNAL SKIN BY DOUBLER AND FILLER REPAIR IAW REO-01934 AND TREATED AREA IAW DC-8 SRM 51-1-8.May 3, 1996 · N8085U · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS96820092Longeron · crackedINSPECTION TYPE 'B', CRACK BEYOND STOP DRILL .5 INCH LONG AT LONGERON 24R FS 882. REPAIRED PER SRM 53-2-2.May 1, 1996 · N702UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS96820094Fitting · crackedINSPECTION TYPE 'B', B/T FITTING CRACKED AT FS 1200 LONGERON 28L AFT SIDE. REPLACED FITTING PER SRM 53-2-0.Apr 30, 1996 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96820093Fitting · crackedINSPECTION TYPE 'B', B/T FITTING CRACKED AT FS 1200 LONGERON 33R TO 34R FWD SIDE. REPLACED FITTING PER SRM 53-2-0.Apr 30, 1996 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96806060Battery Pack · dischargedMAINTENANCE REPORTED, EMERGENCY EXIT LIGHTS DO NOT TEST PROPERLY DURING PRE/FLT. REPLACED BATTERY AND RELAY UNIT WITH REF TO MM 33-50-01, GROUND CKS GOOD.Apr 25, 1996 · N705UP · Doug DC871F · Emergency LightingSDR SRAA49603Switch Wire · defectiveDOV - FLT AD01 - ON TAKEOFF AFTER GEAR RETRACTED, GEAR DOORS AND GEAR UNSAFE WARNING LIGHTS REMAINED ON, CYCLED GEAR THREE TIMES, PROBLEM REMAINS. DUMPED FUEL AND DIVERTED TO JFK. AIRCRAFT LANDED SAFELY. AIRCRAFT IS CURRENTLY ON JACKS, FOUND WIRING TO LT MAApr 22, 1996 · N872SJ · Doug DC871F · Landing Gear Position and WarningSDR UPS96820120Slide · low pressureFWD ENTRY DOOR SLIDE HAS LOW PRESSURE. REPLACED ESCAPE SLIDE ASSY PER MM 25-62-00.Apr 18, 1996 · N702UP · Doug DC871F · Escape SlideSDR UPS96805975Light · inopMAINTENANCE PRE-DEPARTURE CHECK, EMERGENCY EXIT LIGHT INOP. EMERGENCY LIGHT BATTERY PACK REPLACED.Apr 15, 1996 · N748UP · Doug DC871F · Emergency LightingSDR UPS96805960Escape Slide · failed to deployCREW REPORTED ESCAPE SLIDE FAILED TO DEPLOY. REPLACED SLIDE ASSY, DAMAGED LANYARD.Apr 11, 1996 · N713UP · Doug DC871F · Escape SlideSDR UPS96805957Control Valve · out of adjustWHILE IN FOR C-CHECK, MAINTENANCE REPORTED BLOCK TURN BACK RUDDER PEDAL STEERING STIFF TO THE RIGHT. ADJUSTED NOSE WHEEL STEERING CNTRL VALVE. OPS CHECKED GOOD PER MM 32-51-01.Apr 11, 1996 · N797UP · Doug DC871F · Landing Gear Steering SystemSDR UPS96805956Bogie Trim Line · rupturedAIR TURN BACK DUE TO LOSS OF HYD FLUID. FOUND BOGIE TRIM CYLINDER LINE RUPTURED, REPLACED LINE HYD SYS FILTERS, ALL BRAKES AND TIRES DUE TO HIGH ENERGY STOP AND SUBSEQUENT SOAKING WITH WATER BY C.F.R. DUE TO HEAVY SMOKE FROM LT GEAR.Apr 11, 1996 · N713UP · Doug DC871F · Hydraulic System, MainSDR UPS96805897Longeron · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 31R O/B SIDE HEAVY CORROSION AT FS 683. REPAIRED PER UPS EO DC8-53-1602.Mar 18, 1996 · N797UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS96805864Doubler · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON DOUBLER AROUND FASTENERS AT STA 683 TO 780 LBL 10 RBL 10. REPAIRED PER UPS EO.Mar 18, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805857Doubler · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON FUSELAGE INNER DOUBLER, FS 1600-1650, LONGERONS 21R-31R. REPLACED DOUBLER SECTION PER SRM 51-1-21.Mar 13, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805886Doubler · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1050 SPLICE FINGER DOUBLER HAS HEAVY CORROSION AND CRACKS ON LONGERONS 31R AND 31L. REPLACED DOUBLER PER SRM 51-1-20D AND 51-1-21.Mar 11, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805885Splice Strap · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED FS 1050 SPLICE STRAP DOUBLER HAS HEAVY CORROSION ON LONGERONS 31R AND 31L. REPLACED STRAP PER SRM 51-1-20D.Mar 11, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805894Fitting · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON KEEL TEE FITTING FS 683 LONG 36. REPLACED PER UPS EO DC8-53-1598.Mar 10, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805884Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED T-FITTING HEAVY CORROSION AT FS 1180 LONG 34R. REPLACED FITTING PER SRM 51-1-20D.Mar 10, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous Structure
Back to Douglas DC-8-71F