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 UPS06846403Fitting · crackedINSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 1160 L19R AFT SIDE. REMOVE AND REPLACE FITTING IAW SRM 51-1-20D.Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846395Fitting · crackedINSPECTION TYPE:C1 FITTING CRACKED AT STA 834.500 L22R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846355Fitting · crackedFOUND LONGERON END FITTING CRACKED AT STA 902.125 L4L. REMOVED AND REPLACED END FITTING AT STA 902.125 L4L IAW SRM 51-1-20D, 51-3-0 AND SRM 51-1-21.Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846354Fitting · crackedFOUND FITTING CRACKED AT STA 820 L18L . REMOVED AND REPLACED END FITTING AT STA 820 L18L IAW SRM 51-1-20D, 51-03-02-0 AND SRM 51-01-08-0.Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846339Fitting · crackedFOUND ATTACH FITTING CRACKED AT STA 1150 L18R. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-20D.Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846334Fitting · crackedFOUND LONGERON END FITTING CRACKED AT STA.857.125 L9L. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21 AND 51-1-20D.Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846331Fitting · crackedFOUND LONGERON END FITTING CRACKED AT STA 680 L5R. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L5R IAW SRM 51-01-21, 51-03-02-0 AND SRM 51-01-20D.Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846330Fitting · crackedFOUND LONGERON END FITTING AT STA 902.125 L8R IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 902.125 L8R IAW SRM 51-1-21, 51-1-20D, AND SRM 51-3-0.Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846329Fitting · crackedLONGERON END FITTING CRACKED AT STA 857.125 L7L. REMOVED AND REPLACED LONGERON END FITTING AT STA 857.125 L7L IAW 51-3-2 AND SRM 51-1-20D.Feb 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846440Skin · corrodedINSPECTION TYPE:C1 UPON REMOVAL OF D-PIT SCUFF PLATE FOUND LWR SKIN CORRODED IN SEVERAL AREAS BEYOND LIMITS. REMOVED AND REPLACED LWR BELLY SKIN AT STA 1350-1450 L31L TO L32R IAW SRM 51-01-20D, 51-01-21, AND DWG 5615572Feb 17, 2006 · N703UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846333Skin · crackedFOUND FUSELAGE SKIN CRACKED 1" LONG AT STA 1746 L17L. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7, 51-1-21 AND 51-1-20D.Feb 14, 2006 · N703UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846125Smoke · detectedSMOKE IN COCKPIT, CARGO AREA. A/C INCURRED EXTENSIVE DAMAGE FROM CARGO COMPARTMENT FIRE. AIRCRAFT REMOVED FROM UPS OPERATION SPECIFICATION.Feb 8, 2006 · N748UP · Doug DC871F · Air Distribution SystemSDR UPS06846059Windshield · crackedOUTER PANE WINDSHIELD ON F/O'S SIDE CRACKED. REMOVED AND REPLACED RT WINDSHIELD PER MM 56-10-02-2, OPS AND LK CKS OK.Jan 27, 2006 · N706UP · Doug DC871F · Flight Compartment WindowsSDR UPS06846194Clip · brokenINSPECTION TYPE:C1, T-BOLT BACKUP FITTING REPAIR BROKEN AT C-PIT DOOR JAMB, STA 1195 BETWEEN L33R AND L34R. REMOVED AND REPLACED BACKUP FITTING REPAIR CLIP IAW SRM 51-1-20D.Jan 25, 2006 · N702UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846057Window · leakingATB - PRESSURIZATION LEAK, STARTED AT 15,000'. LOCATED PRESS LEAKS AT CAPTAINS AND FO'S L1 AND R1 WINDOWS. SEALED WINDOWS IAW MM 56-10-02.Jan 25, 2006 · N755UP · Doug DC871F · Flight Compartment WindowsSDR IXXA0600105OActuator · inoperativeDURING CLIMB OUT FROM CAPTAINS AND FIRST OFFICERS YOKE TRIM SWITCHES STOPPED WORKING AT TOP OF CLIMB. THE CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITH OUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE TRIM SERVO ACTUATOR AND ALL WORK DONE WAS IAW APPLJan 25, 2006 · N825BX · Doug DC871F · Elevator Tab Control SystemSDR UPS06846159Frame · corrodedINSPECTION TYPE:C1 EXFOLIATION CORROSION UNDER FRAME 1000 ABOVE L36 AT SITE OF REMOVED NUTPLATE. REPAIRED FRAME AT STA 1000 L36 IAW EO DC-8 5310-11728-B.Jan 24, 2006 · N702UP · Doug DC871F · Fuselage Main, FrameSDR UPS06846081Fitting · crackedINSPECTION TYPE:C3 STA 680 BETWEEN LONG 36 AND 35L AFT SIDE OF BULKHEAD FOUND CRACKED FITTING, VIEWED THROUGH STRESS PANEL OPENING. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 21-1-20D.Jan 21, 2006 · N718UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS06846080Fitting · crackedINSPECTION TYPE:C3 STA 680 BETWEEN LONGERON 36 AND 35R AFT SIDE OF BULKHEAD FOUND CRACKED FITTING, VIEWED THROUGH STRESS PANEL OPENING. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND 51-1-20D.Jan 21, 2006 · N718UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS06846010Window · crackedCONSIDERABLE ARCING ON OUTER LAYERS OF CAPTAIN'S SIDE WINDSHILED. ACROSS ENTIRE TOP EDGE BUT CONCENTRATED AT TOP. REMOVED CAPTAIN'S WINDSHIELD PER MM 56-10-02-2. INSTALLED CAPTAIN'S WINDSHIELD IAW DC8 MM 56-10-022 THRU STEP 12.Jan 21, 2006 · N755UP · Doug DC871F · Flight Compartment WindowsSDR UPS06846045Window Frame · corrodedCAPTAIN'S WINDOW FRAME RUSTED PITTED ALONG LOWER I/B CORNER OF WINDOW FRAME. REMOVED CORROSION FROM WINDOW FRAME AND PRIMED AREA AS REQ. REMOVED Z ANGLE FROM CAPT LWR I/B CORNER OF WINDOW FRAME IAW 51-01-21A & 51-01-200. ORIG THICKNESS .090. MAT LOSS .013 TJan 21, 2006 · N755UP · Doug DC871F · Fuselage Main, StructureSDR UPS06846056A/C Pack · failedPACK TRIP OVERHEAT LIGHT ON LANDING ALTHOUGH WE HAD SECURED PACK WITH NORMAL CONFIGURATION. SMOKE IN COCKPIT. PACK TRIP DUE TO LOSS OF NR 4 GEN BUSS. RESET BATTERY POWER SWITCH. PERFORMED ADJ/TEST IAW MM 21-55-00-5. RAN ENGS SYSTEM OPS CK GOOD.Jan 20, 2006 · N755UP · Doug DC871F · Cabin Cooling SystemSDR UPS06846048Warning Light · illuminatedNR 4 GENERATOR "BUSS POWER FAIL" LIGHT ON CLIMB-OUT. V/F BECAME ERRATIC. ACCOMPLISHED CHECKLIST AND REGAINED POWER FOR 3 MINUTES WITHOUT TRYING PARALLELING. TRIPPED TWICE. MEGGED T1, T2, T3 FEED LINES ALL MORE THAN 20 MEGA OHMS. PLACED NR 2 GCU IN POS NR Jan 20, 2006 · N755UP · Doug DC871F · Central WarningSDR UPS06845986Clip · brokenEVAC SLIDE CONTAINER LOOSELY ATTACHED. FOUND CLIP BROKEN ON HOUSING, DEFERRED EVAC SLIDE INOP PER MEL 52-7-4. SLIDE REMOVED FROM DOOR AND SECURED IN COURIER SEATS PER MEL1 D318486. REPLACED LATCH ON EVAC SLIDE COVER. INSTALLED SLIDE AND CONTAINER ON FWD ENTJan 20, 2006 · N729UP · Doug DC871F · Escape SlideSDR UPS06846353Fitting · crackedFOUND STA 1180 L20R FITTING CRACKED. REMOVED AND REPLACED END FITTING AT STA 1180 L20R IAW SRM 51-1-20D, 51-3-2 AND 51-1-8.Jan 18, 2006 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846182Skin · corrodedINSPECTION TYPE:C1, CORROSION ON LOWER SKIN IN MULTIPLE AREAS AROUND 62 HOLE ENTRANCE INTERIOR, ESPECIALLY IN CORNERS OF EVERY RIB AROUND DOOR. REPAIRED LOWER SKIN AND RIBS AT 62 HOLE DOOR STA 1690 RBL30 TO LBL30 TO STA 1751 RBL12 TO LBL12 IAW SRM 51-1-8, 53Jan 18, 2006 · N702UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846122Skin · crackedINSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT STA 1726 L16R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-02-01-0, 51-1-21 AND 51-1-20D.Jan 18, 2006 · N702UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846121Skin · crackedINSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT STA 1746 L16L. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-02-01-0 FIG 007, 51-1-21 AND 51-1-20D.Jan 18, 2006 · N702UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06846120Fitting · crackedINSPECTION TYPE:C1 CRACK ON LONGERON 19L ATTACH BRACE AT STA 1240. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Jan 17, 2006 · N702UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846116Fitting · crackedINSPECTION TYPE:C1 L28R END FITTING CRACKED AT STA 1690-1700. REMOVED AND RPLACED END FITTING IAW SRM 51-1-21 AND 51-1-20D.Jan 17, 2006 · N702UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846072Seat Track · corrodedINSPECTION TYPE:C1 LBL 24 AT STA 680 HAS CORROSION UNDER SEAT TRACK AS VEIWED FROM LOWER ACCY COMPT. REMOVED, FABRICATED AND REPLACED SEAT TRACK IAW SRM 51-1-21, 51-3-0,5 AND 53-02-03.Jan 17, 2006 · N702UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06846022Fitting · crackedINSPECTION TYPE:C3 LONGERON 32L END FITTING CRACKED AT STA 1490. REMOVED SPLICE END FITTING IAW SRM 51-1-21, LOCATED AND DRILLED REPLACEMENT END FITTING IAW SRM 51-3-2, DWG 3619434 AND SRM 51-1-21.Jan 17, 2006 · N718UP · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA0600037OSensing Element · defectiveON FLIGHT ATN833 FROM KSJC TO KRFD, NR 3 ENGINE FIRE WARNING LIGHT AND BELL CAME ON DESCENT TO KRFD. COMPLY WITH COMPANY PROCEDURES WIND MILLING TIME 30 MINUTES AND OIL PRESSURE WAS 20 PSI. CREW ELECTED TO LAND AT KTOL AND LANDED WITHOUT INCIDENT. MAINTENANJan 17, 2006 · N828BX · Doug DC871F · Fire DetectionSDR UPS06846070Web · corrodedINSPECTION TYPE:C1 HEAVY CORROSION ON C-PIT TORQUE BOX WEB ALONG L33R AT STA 1190. FABRICATED AND INSTALLED DOUBLER IAW DWG 3753772 AND SRM TEMP REV. 53-166 (53-2-0 FIG 25).Jan 16, 2006 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06846119Fitting · corrodedINSPECTION TYPE:C1 HEAVY CORROSION ON FITTING IN OB UPPER AFT CORNER OF LT W/W STA 974 LBL66. REMOVED, FABRICATED AND INSTALLED FITTING IAW 51-1-20D, DWG 2647420,Jan 13, 2006 · N702UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846073Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING HAS A 3 INCH CRACK STA 680 L-7R. REMOVED AND REPLACED LONGERON END FITTING IAW SRM 51-1-20D AND 51-3-0.Jan 13, 2006 · N702UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06846033Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING HAS A 4" CRACK, STA 680 L8R. REMOVED END FITTING IAW SRM 51-1-20D, FABRICATED AND INSTALLED LONGERON END FITTING AT STA 680 L8R IAW SRM 51-01-20D.Jan 13, 2006 · N702UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS06846196Spar Cap · crackedINSPECTION TYPE:C1, NDT FOUND CRACK APPROX 8" LONG ON LT LOWER SPAR CAP AT BL 47-55 ON HORIZONTAL LEG STA 857. REPAIRED LT LWR SPAR CAP STA 857 BL47-55 IAW SRO 8530009 AND EA 008-5710-01-A0039.Jan 12, 2006 · N702UP · Doug DC871F · Wing SparSDR UPS06846071Rib · wornINSPECTION TYPE:C1 5TH RIB ON NR 1 PYLON WORN" CHECK LIMITS". BLENDED OUT WORN AREA. FABRICATED AND INSTALLED REPAIR STRAP IAW DC-8 SRM 54-3-1 FIG 3, 51-1-8,51-1-21 AND 51-1-20D.Jan 11, 2006 · N702UP · Doug DC871F · Nacelle/Pylon, Frame/Spar/RibSDR UPS06846051Splice · corrodedINSPECTION TYPE:C3 A-PIT LONGERON 36 STA 300-320 2 EA LONG SPLICES HAVE HEAVY CORROSION. REMOVED 2 EA SPLICES IAW 51-1-20D, FABRICATED AND INSTALLED SPLICE ANGLES IAW SRM 51-03-02, 51-1-8, 51-1-20D, AND SRM 53-02-02 FIG 10.Jan 11, 2006 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06846050Splice · corrodedINSPECTION TYPE:C3 A-PIT AT LONG 36 BETWEEN STA 280-300 LONGERON SPLICE HAS HEAVY CORROSION. REMOVED SPLICE IAW SRM 51-1-20, FABRICATED AND INSTALLED LONG SPLICE FITTING AT STA 280-300 L36 IAW SRM 51-03-02, 51-1-8, 51-1-20D AND SRM 53-02-02 FIG 10.Jan 11, 2006 · N718UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS06846003Doubler · mismanufacturedINSPECTION TYPE:C3 FUSELAGE EXTERNAL SKIN DOUBLER REPAIR SEVERAL FASTENERS HAVE SHORT EDGE DISTANCE STA 215 L22R-L23R PER DC8- 5330-12800 REPAIR REF: NR 718-2R-11. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21 FABRICATED AND INSTALLED REPAIR 2EA FINGER DOUBJan 11, 2006 · N718UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06845943Battery Pack · inoperativeEMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS CKS GOOD. REF AMM 33-50-01-2.Jan 10, 2006 · N798UP · Doug DC871F · Emergency LightingSDR UPS06845926Light · inoperativeEMERGENCY LIGHTING INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND RELAY UNIT PER M/M 33-50-01-2.Jan 10, 2006 · N772UP · Doug DC871F · Emergency LightingSDR IXXA0600014OHydraulic System · leakingDURING FLIGHT 828 FROM KRFD TO KIAH MAIN SYSTEM HYDRAULIC FLUID LOST TO STANDPIPE AFTER GEAR RETRACTION BEFORE FLAPS WERE RETRACTED. AIR BRAKE WAS NOT USED. THE CREW ELECTED TO LAND AT KTOL AND LANDED WITHOUT INCIDENT. INSPECTION IS ON GOING AND MORE INFORMJan 10, 2006 · N820BX · Doug DC871F · Hydraulic System, MainSDR UPS06845928Smoke Goggles · scratchedF/O SMOKE GOGGLES SCRATCHED. REPLACED F/O SMOKE GOGGLES. OPS NORMAL.Jan 9, 2006 · N705UP · Doug DC871F · Emergency EquipmentSDR UPS06845960Skin · crackedINSPECTION TYPE:C3 CARGO DOOR UPPER AFT CORNER HAS AN 1/2" CRACK WHICH RUNS FROM EDGE OF DOOR CORNER RIVET. CUT OUT DAMAGED AREA IAW SRM 53-2-O FIG 21, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLERS AT D-PIT DOOR UPPER AFT CORNER IAW SRM 53-2-0 FIG 21Jan 8, 2006 · N718UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS06845925Skin · corrodedFUSELAGE HAS A BULGED AREA 25" FWD OF PIT 31 LWR FWD CORNER MARKED AND ADVISED BY MX. GAINED ACCESS TO THE BACKSIDE OF AREA NO CORROSION OR DEFECTS FOUND AT THIS TIME AS PER SRM 51-1-0. OK FOR SERVICE, AREA FOUND TO BE FREE AND SMOOTH.Jan 7, 2006 · N705UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS06845922Light · weakINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ARE DIM. REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CHECK NORMAL IAW MM 33-50-01.Jan 7, 2006 · N772UP · Doug DC871F · Emergency LightingSDR UPS06846054Shear Tie · corrodedINSPECTION TYPE:C3 HEAVY CORROSION ON SHEAR TIE AT STA 1460 L32L AND L34R. REMOVED SHEAR TIE IAW SRM 51-1-21, FABRICATED AND INSTALLED SHEAR TIE AT STA 1460 BETWEEN L32L AND L34R IAW DWG 5640323 AND SRM 53-4-1, 51-1-8, AND SRM 51-1-20D.Jan 6, 2006 · N718UP · Doug DC871F · Fuselage Main, Structure
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