Douglas DC-8-71F

Service difficulty reports · 8,938

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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 IXXA0200047OSeal · defectiveEN ROUTE FROM LRD TO TOL, THE NUMBER TWO ENGINE FLAMED OUT DURING CLIMBOUT FROM LRD. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE WHICH REVEALED THE FUEL FLOW TRANSMITTER LEAKINGAug 1, 2002 · N823BX · Doug DC871F · Engine Fuel DistributionSDR UPS02839138Longeron · crackedINSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D.Jul 30, 2002 · N715UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02839126Longeron · crackedINSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D.Jul 30, 2002 · N715UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02839125Longeron · crackedINSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB, LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D.Jul 30, 2002 · N715UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02839124Skin · damagedINSPECTION TYPE:C1 REPAIR DOUBLER 715-3L-12 STA 1690-1698 AND LONG 28L IS CLASSIFIED AS CAT D ONLY 2 ROWS OF FASTENERS BEYOND CUTOUT AND 3 OF 4 CORNERS OF CUTOUT ARE SQUARE. REMOVED EXISTING REPAIRS AND FITTINGS, FABBED, LOCATED & DRILLED DOUBLER & FILLER IAWJul 30, 2002 · N715UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXAA0200084SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AT FUSELAGE STATION 45 LONGERON 29L LOWER AREA. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IAW THE DOUGLAS SRM.Jul 29, 2002 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02839142Floor Panel · delaminatedINSPECTION TYPE:C1 FLOOR PANEL STA 759-879 PANEL A DELAMINATED. FABBED NEW PANEL IAW UPS EO DC8 5320-9691C.Jul 29, 2002 · N715UP · Doug DC871F · Fuselage Floor PanelSDR UPS02839149Fitting · corrodedINSPECTION TYPE:C1 FWD PIT STA 278 ABOVE LONGERON 31R LOWER SURFACE OF FITTING CORRODED. REMOVED FITTING FOUND CORROSION OUT OF LIMITS IAW DC8 SRM 51-1-8 AND 51 -1-21 AND INSTALLED IAW DC8 SRM 51-1-20D.Jul 27, 2002 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839148Fitting · crackedINSPECTION TYPE:C1 CABIN INTERCOSTAL ATTACH FITTING HAS CRACK STA 902 L19L. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-24 AND 51-1-20D.Jul 27, 2002 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839147Skin · crackedINSPECTION TYPE:C1 LT SIDE FWD OVERWING EMERGENCY EXIT DOOR HAS CRACK INDICATION AT LOWER AFT CORNER, FOUND BY NDT INSPECTION. REPAIRED AREA IAW REO G08714.Jul 27, 2002 · N715UP · Doug DC871F · Emergency ExitsSDR UPS02839152Door Frame · crackedINSPECTION TYPE:C1 FWD CARGO AFT DOOR FRAME FWD LWR INNER SURFACE AT LIGHTENING HOLE MULTIPLE CRACKS, DOUBLER IS UNTREATED METAL AND FASTENERS ARE IMPROPERLY INSTALLED. REPAIRED WEB IAW DAC DWG 5616520.Jul 26, 2002 · N715UP · Doug DC871F · Fuselage Main, StructureSDR UPS02839151Floorbeam · crackedINSPECTION TYPE:C1 FLOORBEAM STA 879 RBL 60 IS CRACKED AT O/B LIGHTENING HOLE. SPLICED IN NEW SECTION OF FLOORBEAM IAW REO G08713.Jul 26, 2002 · N715UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS02839122Floorbeam · crackedINSPECTION TYPE:C1 FLOORBEAM STA 879 RBL 60 IS CRACKED AT O/B LIGHTENING HOLE. SPLICED IN NEW SECTION OF FLOORBEAM IAW REO G08713.Jul 26, 2002 · N715UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS02839089Intercostal · corrodedINSPECTION TYPE:C2 STA 272 TO 280 LONG 35R INTERCOSTAL LOWER FLANGE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9754020 AND SRM 51-1-20D.Jul 26, 2002 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839087Fitting · corrodedINSPECTION TYPE:C2 STA 340 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 36 AND 35R. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.Jul 26, 2002 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838977Longeron · crackedINSPECTION TYPE:C2 LONG 24L IS CRACKED AT STA 978. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATES AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-2 FIG 5.Jul 26, 2002 · N772UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02838975Splice · crackedINSPECTION TYPE:C2 STA 440-460 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.Jul 26, 2002 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839154Bulkhead · crackedINSPECTION TYPE:C1 RT APB CRACKED STA 1766 L11R OUTBOARD OF EXISTING DOUBLER. REPAIRED AREA IAW REO-G08719.Jul 25, 2002 · N715UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS02839132Bulkhead · crackedINSPECTION TYPE:C1 LT AFT PRESSURE BULKHEAD CRACKED AT FS 1766 L11L. REPAIRED AREA IAW DC8 SRM 53-2-5 FIG 14A AND DAC DWG SRO8530007.Jul 25, 2002 · N715UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS02839039Fitting · corrodedINSPECTION TYPE:C2 STA 1152 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 34L TO 35L. REMOVED AND REPLACED FITTING IAW DWG 3755845, AND SRM 53-2-0 FIG 2D.Jul 25, 2002 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839024Doubler · corrodedINSPECTION TYPE:C2 STA 190 DOUBLER CORRODED BEYOND LIMITS BETWEEN LONGERONS 31L & 31R. REMOVED, FABRICATED & INSTALLED REPLACEMENT DOUBLER IAW DWG 5779925 & SRM 51-1-21.Jul 25, 2002 · N772UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838985Finger Doubler · corrodedINSPECTION TYPE:C2 INTERNAL FINGER DOUBLER IS CORRODED BEYOND LIMITS STA 70-210 AT LONG 31R. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5779916, AND SRM 51-1-20D, 51-1-21.Jul 25, 2002 · N772UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200087SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT OUTBOARD SLOT LEADING EDGE AREA ON THE MOUNTING SURFACE WING STATION XFS422.750. REPAIR ACCOMPLISHED, REMOVAL OF CORROSION, FABRICATION AND INSTALLATION OF REPAIR DOUBLERS AND SHIMS IAW THEJul 24, 2002 · N825BX · Doug DC871F · Wing, Plate/SkinSDR UPS02839038Door Frame · corrodedINSPECTION TYPE:C2 CARGO PIT C DOOR CORNER CLIPS CRACKED INSIDE LIGHTENING HOLES FS STA 1170 TO 1210 AT LONG 22R APPROX. FOUND DOOR PAN/FRAME CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED CLIPS, DOUBLERS, AND DOOR PAN SECTION IAW DWG 5894025 AND Jul 24, 2002 · N772UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS02839040Gusset · corrodedINSPECTION TYPE:C2 STA 131 TO 121 AT LBL 45 ANGLE FITTING/GUSSET IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED GUSSET IAW DWG 5597992, AND SRM 51-1-20D.Jul 23, 2002 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839041Web · corrodedINSPECTION TYPE:C2 STA 89 DOUBLER, FINGER DOUBLER AND WEB ARE CORRODED BEYOND LIMITS AT RBL 30. CUT OUT CORRODED AREA ON WEB, FABRICATED AND INSTALLED FILLER, DOUBLER, AND FINGER DOUBLER IAW DWG 5612298, AND SR08530026.Jul 23, 2002 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839034Stiffener · crackedINSPECTION TYPE:C2 LEFT WING T/E INBOARD VERTICAL STIFFENER AT FLAP HINGE 98 IS CRACKED AT BOTTOM. REMOVED, FABRICATED, AND INSTALLED STIFFENER IAW DWG 3643320, AND SRM 51-3-0.Jul 23, 2002 · N772UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS02838979Finger Doubler · corrodedINSPECTION TYPE:C2 AFT SIDE OF STA -99 FINGER DOUBLER IS CORRODED BEYOND LIMITS AT RBL 60. REMOVED, FABRICATED AND INSTALLED DOUBLER DWG 5612298.Jul 23, 2002 · N772UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838976Rib · crackedINSPECTION TYPE:C2 LEFT HORIZONTAL STAB L/E UPPER RIB IS CRACKED AT FASTENER END AT XFS 166.250. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 55-3-0 FIG 8.Jul 22, 2002 · N772UP · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR UPS02838978Skin · damagedINSPECTION TYPE:C2 R-1 DOOR UPPER FWD CORNER HAS A REPAIR THAT DOES NOT CONFORM TO THE SRM AT STA 160 AT LONG 11R. REMOVED DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 14.Jul 20, 2002 · N772UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838797Battery Pack · dischargedINSPECTION TYPE:C2 EMERGENCY EXIT LIGHTS FAILED OPS CHECK. RANG OUT WIRING PER WDM 33-50-01, WIRING CHECKED OUT GOOD. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, AND OPS CHECKED GOOD IAW DC8 M/M 33-50-01.Jul 14, 2002 · N730UP · Doug DC871F · Emergency LightingSDR IXXA0200046OCylinder · defectiveENROUTE FROM BFI TO PDX, THE LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING THE LANDING UPLATCH CHECK. THE FIIGHT CREW CYCLED THE LANDING GEAR TO EXTINGUISH THE WARNING INDICATION. THE FLIGHT CONTINUED TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE Jul 12, 2002 · N823BX · Doug DC871F · Landing Gear Retraction/Extension SystemSDR IXXA0200086SDoor Frame · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FORWARD CARGO COMPARTMENT C1 DOOR JUST BELOW THE AFT LOCK BRACKET. REPAIR ACCOMPLISHED, REMOVAL OF EXISTING REPAIR AND CORROSION, FABRICATION AND INSTALLATION OF NEW EXTENDED FRAME IAW THE DOUGLJul 10, 2002 · N825BX · Doug DC871F · Cargo/Baggage DoorsSDR IXXA0200085SDoor · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LEFT HAND SIDE OF THE AFT PASSENGER DOOR SKIN IN THE FORWARD LOWER CORNER BELOW AN EXISTING REPAIR AT FUSELAGE STATION 1640 LONGERON 22L. REPAIR ACCOMPLISHED, REMOVAL OF EXISTING DOUBLER, REMOVAL Jul 9, 2002 · N825BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA0200044OUplock · sticksEN ROUTE FROM RFD TO TOL, THE LANDING GEAR UPLATCH CHECK FAILED AND THE LANDING GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR SEVERAL TIMES BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND THE FLIGHT CONJul 9, 2002 · N821BX · Doug DC871F · Landing Gear Retraction/Extension SystemSDR IXXA0200083SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FORWARD CARGO COMPARTMENT AFT DOOR SKIN TOP REAR AREA AT FUSELAGE STATION 557.5 AND LONGERON 27R. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DJul 7, 2002 · N825BX · Doug DC871F · Cargo/Baggage DoorsSDR UPS02838753Skin · crackedINSPECTION TYPE: N/A SKIN CRACK L/T FUSELAGE STATION 1500 ITEM DEFERRED D240904. INSTALLED REPAIR DOUBLER PER EO DC8-5330-17101A.Jul 7, 2002 · N729UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838778Fitting · corrodedINSPECTION TYPE:C2 FITTING IN TORQUE BOX AT STA 1150 IS CORRODED BEYOND LIMITS AT LONG 31R. REMOVED AND REPLACED FITTING IAW DWG 3754914, AND SRM 51-3-0.Jul 7, 2002 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02838747Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHTS DO NOT TEST. REPLACED EMERGENCY BATTERY PACK.Jul 5, 2002 · N752UP · Doug DC871F · Emergency LightingSDR IXXA0200082SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DISCOVERED ON THE FUSELAGE SKIN AT FUSELAGE STATION 35 LONGERON 33R. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER IAW THE DOUGLAS SRM AND EA 28276-5384Jul 4, 2002 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200081SDoor · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT FUSELAGE STATION 60 LONGERON 21L.REPAIR ACCOMPLISHED, REMOVED DAMAGED AREA AND INTERNAL DOUBLER AND TRIPLER, FABRICATION AND INSTALLATION OF FILLER AND REPAIR DOUBLER AND TRIPLER IN ACCORDANCE WITH THEJul 3, 2002 · N825BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA0200078SSkin · dentedDURING ROUTINE C-CHECK INSPECTION, A DENT WAS DISCOVERED ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 1560 LONGERON 25R. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER AND FILLER IAW THE DOUGLAS SRM.Jul 2, 2002 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200077SSkin · gougedDURING ROUTINE C-CHECK INSPECTION, GOUGES WERE DETECTED ON THE FUSELAGE SKIN ABOVE THE FORWARD UPPER CORNER OF THE AFT PIT DOOR CUT OUT, FUSELAGE STATION 1400, LONGERON 24 RT. REPAIR ACCOMPLISHED, BLENDING OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAJul 2, 2002 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200080SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE SEAM LONGERON 11L F/S 1620. REMOVED CORROSION, SEALED AREA, IAW THE DOUGLAS SRM.Jul 2, 2002 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200079SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CRACKS AND CORROSION WERE DETECTED ON THE FUSELAGE AFT RIGHT DOOR UPPER AFT CUT OUT FUSELAGE STATION 1660 LONGERON 11R. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA AND INTERNAL DOUBLERS. FABRICATION AND INSTALLATION OF REPAIJul 2, 2002 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02838711Skin · crackedINSPECTION TYPE:C2, RIGHT WING CENTER LEADING EDGE LOWER SKIN IS CRACKED INBOARD OF XW408. STOP-DRILLED CRACKED, NDT VERIFIED CRACK TERMINATES AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087 FIG 1 APPX C.Jun 28, 2002 · N730UP · Doug DC871F · Wing, Plate/SkinSDR UPS02838858Spar Cap · damagedINSPECTION TYPE:C2 RIGHT WING REAR SPAR UPPER CAP HAS ELONGATED HOLES BETWEEN XRS 456 AND XA 500. OVERSIZED HOLES, NDT VERIFIED NO CRACKS AT HOLES, FABRICATED AND INSTALLED BUSHINGS IAW 8110-3 APPROVED SAA SK 730-143, AND UPS ENGINEERING FILE NUMBER DC8-57-20Jun 26, 2002 · N730UP · Doug DC871F · Wing SparSDR UPS02838854Shear Tie · crackedINSPECTION TYPE:C2 STA 540 SHEAR TIE IS CRACKED BETWEEN LONG 31L AND 32L. CUT OUT DAMAGE, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-2-0 FIG 2B.Jun 22, 2002 · N730UP · Doug DC871F · Fuselage Main, StructureSDR UPS02838853Shear Tie · crackedINSPECTION TYPE:C2 STA 540 SHEAR TIE IS CRACKED BETWEEN LONG 35R AND 36. CUT OUT DAMAGE, FABRICATED AND INSTALLED SHEAR TIE REPAIR IAW SRM 53-2-0 FIG 2B.Jun 22, 2002 · N730UP · Doug DC871F · Fuselage Main, StructureSDR UPS02838795Web · corrodedINSPECTION TYPE:C2 CORROSION BETWEEN LONGERON AND FRAME ATTACH PLATE AFT OF TORQUE BOX STA 1160 AT LONG 35R TO 33R WEB IS CORRODED BEYOND LIMITS. REMOVED EXISTING DOUBLER, CUT OUT CORRODED SECTION OF WEB, FABRICATED AND INSTALLED WEB SECTION, SPLICE PLATES, FJun 22, 2002 · N730UP · Doug DC871F · Fuselage Miscellaneous Structure
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