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 IXXA0200129SDoubler · inadequateDURING ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR AT FUSELAGE STATION 45 LONGERON 29L WAS DETECTED. REPAIR ACCOMPLISHED, REMOVAL OF TEMPORARY REPAIR, DAMAGE. FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MAAug 27, 2002 · N828BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA0200128SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED UNDER AND EXISTING REPAIR DOUBLER AFT OF THE C-1 DOOR LONGERON 36, FS 333 TO FS 450. REPAIR ACCOMPLISHED, REMOVAL OF REPAIR DOUBLER, CORROSION AND SKIN PANEL, FABRICATION AND INSTALLATION OF NEW SKIN PAug 27, 2002 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200127SDoubler · dentedDURING ROUTINE C-CHECK INSPECTION, A DENT WAS DISCOVERED UNDER AN EXISTING REPAIR ON THE CENTER SECTION OF THE LOWER FORWARD CARGO COMPARTMENT FUSELAGE STATION 335. REPAIR ACCOMPLISHED, REMOVAL OF PREVIOUS REPAIR, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATIOAug 27, 2002 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02839465Longeron · crackedINSPECTION TYPE:C1 AFT FUSELAGE ACCESS THROUGH DOOR 60 AT FS 1766-1790 LONGERON 17L IS CRACKED. REMOVED AND REPLACED LONG 17L FS 1766-1790 IAW DC8 SRM 51-1-20D AND 51-1-21.Aug 27, 2002 · N755UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02839460Longeron · crackedINSPECTION TYPE:C1 AFT FUSELAGE ACCESS THROUGH DOOR 60 AT FS 1766-1790 LONGERON 17R IS CRACKED. REMOVED LONG & ASSOCIATED PARTS IAW DC8 SRM 51-1-20D & 51-1-21. INSTALLED NEW LONG AND ASSOCIATED PARTS IAW DC8 SRM 51-1-20D & 51-1-21.Aug 27, 2002 · N755UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02839451Fitting · crackedINSPECTION TYPE:C1 S-51 STRINGER END FITTING CRACKED FWD SIDE AT XRS 74.000 2 MAIN. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-20D AND 51-1-23.Aug 27, 2002 · N755UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS02839447Fitting · crackedINSPECTION TYPE:C1 S-51 STRINGER END FITTING CRACKED AFT SIDE AT XRS74.000 NR 3 ALT. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-1-23.Aug 27, 2002 · N755UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS02839444Pan · crackedINSPECTION TYPE:C1 A-PIT DOOR FWD LOWER STOP ON DOOR AND DOOR PAN UNDER FITTING ARE CRACKED AT STA 320 AT LONG 32R. REMOVED AND REPLACED STOP FITTING, REMOVED, FABRICATED AND REPLACED LOWER PAN SECTION IAW SRM 52-4-2 AND 52-2-0 FIG 2.Aug 27, 2002 · N708UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS02839443Angle · crackedINSPECTION TYPE:C1 A-PIT CARGO DOOR FWD AND AFT ANGLES UNDER SEAL AREA AT STA 280 AND 340 ARE CRACKED ON DOOR. REMOVED, FABRICATED AND REPLACED ANGLES IAW DWG 5754260, AND SRM 51-1-20D, 51-1-21.Aug 27, 2002 · N708UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS02839434Longeron · crackedINSPECTION TYPE:C-1 LONG 17L AND END FITTING CRACKED AT STA 1772. REMOVED LONG AND END FITTING, FABRICATED LONGERON SLICE AND DRILLED UP NEW END FITTING IAW DRAWING 5649327 AND SRM 51-1-24, INSTALLED REPAIR PARTS IAW SRM 51-1-20D.Aug 27, 2002 · N708UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02839433Skin · crackedINSPECTION TYPE:C1 STA 8.000, LONG 33L DOUBLER INSTALLED, CLASSIFIED CATEGORY D. REMOVED DOUBLER, STOP DRILLED CRACK NDT HFEC INSPECTED, CRACK TERMINATES AT STOP DRILL. CUT OUT DAMAGED AREA, FABRICATED FILLER AND REPAIR DOUBLER IAW SK 708-078, INSTALLED FILLAug 27, 2002 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02839427Skin · damagedINSPECTION TYPE:C-1 STA 8.0, LONG 33R DOUBLER, CLASSIFIED CATEGORY D. REMOVED DOUBLER, CUT OUT DAMAGED AREA NDT HFEC INSPECTED NO CRACKS NOTED. FABRICTAED FILLER AND DOUBLER IAW SAA SK 708-080. INSTALLED FILLER AND DOUBLER IAW EO DC8-5330-12800-C, AND SAA SAug 27, 2002 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02839350Skin · damagedINSPECTION TYPE:C1 STA 1400 LONG 30L EXTERNAL DOUBLER, CLASSIFIED CATERGORY D, IAW DC8-5330. REMOVED EXTERNAL DOUBLER AT STA 1400 LONG 30L. FABRICATED INTERNAL AND EXTERNAL DOUBLERS IAW SRM 53-2-1 FIG 7, INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW SRM 51-1-Aug 27, 2002 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02839320Longeron · crackedINSPECTION TYPE:C1 STA 1772 LONG 17R AND END FITTING ARE CRACKED. REMOVED LONGERON 17R AND END FITTING, FABRICATED LONGERON SECTION AND REPLACED END FITTING, AND INSTALLED END FITTING AND LONGERON SECTION IAW DWG 4772397 AND 5649327, AND SRM 51-1-20D.Aug 27, 2002 · N708UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02839306Skin · damagedINSPECTION TYPE:C1 STA 1460 LONG 30L EXTERNAL DOUBLER. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW SRM 53-2-1 FIG 7.Aug 27, 2002 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200139SStructure · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DISCOVERED ON THE FUSELAGE BY THE LEFT HINGE OF THE RADOME. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER, IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAug 26, 2002 · N828BX · Doug DC871F · Fuselage Main, StructureSDR IXXA0200126SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE STATION 1660 LONGERON 11L UPPER AFT CORNER ON THE AFT ENTRY DOOR CUTOUT. REPAIR ACCOMPLISHED, REMOVED DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER, DOUBLER AND TRIPLER IN ACCORDAAug 26, 2002 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200125SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, TWO CRACKS WERE DECTECTED ON THE FUSELAGE SKIN AT STATION 490 ON THE LOWER AFT CORNER OF THE FORWARD ENTRY DOOR CUT OUT. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOULBER AND TRIPLER IN ACAug 26, 2002 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200124SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE AT FS 490 LONGERON 11R UPPER AFT CORNER OF THE FORWARD SERVICE DOOR CUT OUT. REPAIR ACCOMPLISHED, REMOVED DAMAGE, FABRICATION AND INSTALLATION OF REPAIR DOULBER AND TRIPLER IN ACCORDANCE WAug 26, 2002 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200123SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE UPPER FORWARD CORNER OF THE FORWARD SERVICE DOOR CUT OUT. REPAIR ACCOMPLISHED, REMOVED DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER, DOUBLER AND TRIPLER IN ACCORDANCE WITH THE DOAug 26, 2002 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200122SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE, AT FS 1620 LONGERON 11R ON THE UPPER AFT CORNER OF THE AFT SERVICE DOOR CUT OUT. REPAIR ACCOMPLISHED, CUT OUT DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR FILLER, DOUBLER AND TRAug 26, 2002 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200121SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE SKIN. FUSELAGE STATION 8 LONGERON 28R. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIRAug 26, 2002 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0200120SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FUSELAGE, FS 1620 LONGERON 21L BY THE AFT ENTRY DOOR CUT OUT ON THE LOWER FORWARD CORNER. REPAIR ACCOMPLISHED, REMOVED DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER, DOUBLER AND TRIPLER INAug 26, 2002 · N828BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02839484Fitting · crackedINSPECTION TYPE:C1 L17L AT STA 1770, FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.Aug 26, 2002 · N755UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839459Fitting · crackedINSPECTION TYPE:C1 LONGERON 17R AT STA 1770 HAS CRACKED FITTING. REMOVED OLD FITTING, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.Aug 26, 2002 · N755UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839438Fitting · crackedINSPECTION TYPE:C2 STA 1228 BATHTUB FITTING IS CRACKED BETWEEN LONG 32R-33R INSIDE TORQUE BOX. REMOVED AND REPLACED FITTING IAW DWG 3755840, AND SRM 53-2-0 FIG 2D.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839426Fitting · crackedINSPECTION TYPE:C-1 C-BAG BIN, BATHTUB FITTING CRACKED AT STA 1200, LONG-28L. REMOVED BATH TUB FITTING, FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG 2D. INSTALLED REPAIR DOUBLER INSTALLED NEW FITTING IAW SRM 53-2-0 FIG2D, AND SRM 51-1-20D.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839419Shear Tie · corrodedINSPECTION TYPE:C-1 LIGHT CORROSION BETWEEN LONG 35L AND 35R STA 260 EXTENDING UNDER SHEAR TIES. CORROSION OUT OF LIMITS ON SHEAR TIE AT STA 260, LONG 35L. REMOVED SHEAR TIE IAW SRM 51-1-20. FABRICATED SHEAR TIE IAW SRM 53-4-1, INSTALLED SHEAR TIE IAW SRM 5Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Main, StructureSDR UPS02839416Fitting · crackedINSPECTION TYPE:C-1 C BAG BIN, BATH TUB FITTING CRACKED AT STA 1160 LONG 34R, INSIDE TORQUE BOX. REMOVED CRACKED BATH TUB FITTING IAW 53-2-0. FABRICATED REPAIR ANGLES AND FABRICATED REPAIR PARTS IAW SRM 53-2-0 FIG 2D, INSTALLED REPAIR ANGLES AND BATH TUB FITAug 26, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839414Fitting · crackedINSPECTION TYPE:C1 AFT SIDE STA 1240 FRAME INTERCOSTAL TO FRAME FITTING IS CRACKED AT LONG 33R. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839413Fitting · crackedINSPECTION TYPE:C1 STA 1140 LONG 35R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758496, AND SRM 51-1-20D.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839390Fitting · crackedINSPECTION TYPE:C1 STA 1240 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839326Fitting · crackedINSPECTION TYPE:C1 STA 1240 AFT INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT LONG 33R. REMOVED AND REPLACED FITTING IAW DWG 4758514, AND SRM 51-1-20D.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839323Attach Fitting · crackedINSPECTION TYPE:C1 STA 1230 LONG 35R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758570, AND SRM 51-1-20D.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839309Longeron · crackedINSPECTION TYPE:C1 LONG 34L IS CRACKED AND CORRODED BEYOND LIMITS STA 1746 LONG 34L. REMOVED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG 10.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02839308Longeron · corrodedINSPECTION TYPE:C1 STA 1746 LONG 34R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 5649329, AND SRM 53-2-2 FIG 10.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS02839305Doubler · crackedINSPECTION TYPE:C1 INTERNAL SPLICE DOUBLER IS CRACKED AND CORRODED STA 1690 TO 1766 AT LONG 28L. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW DWG 5644130, AND SRM 51-1-21.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02839302Fitting · crackedINSPECTION TYPE:C1 STA 1745 BETWEEN LONG 35R AND 35L FWD BACKUP FITTING FOR TAILSKID SHOCK ABSORBER IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750865, AND SRM 51-3-0.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839299Doubler · crackedINSPECTION TYPE:C1 INTERNAL SPLICE DOUBLER IS CORRODED AND CRACKED STA 1690 TO 1766 AT LONG 28R. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5644130, AND SRM 51-1-21, 51-1-20D.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS02839297Fitting · crackedINSPECTION TYPE:C1 STA 1230 LONG 33R INTERCOSTAL TO FRAME ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839296Fitting · crackedINSPECTION TYPE:C1 STA 1180 BATHTUB FITTING CRACKED LONG 28L. REMOVED AND REPLACED FITTING IAW DWG 3755842 AND SRM 53-2-0 FIG 2D.Aug 26, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS02839514Frame · crackedINSPECTION TYPE:C1 STA 683 FWD SIDE LOWER BULKHEAD FRAME IS CRACKED BETWEEN LONG 28R TO 29R. REMOVED, FABRICATED AND REPLACED FRAME SECTION IAW DWG 9753751, AND SRM 51-1-20D, 53-2-5, 51-3-0.Aug 25, 2002 · N708UP · Doug DC871F · Fuselage Main, FrameSDR UPS02839488Frame · crackedINSPECTION TYPE:C1 FRAME AT STA -12 IN LT NOSE TUNNEL IS GOUGED AND CRACKED AT LBL 24 AFT SIDE. REMOVED FRAME, FABRICATED AND INSTALLED FRAME IAW DWG 5613861, AND SRM 51-1-20D.Aug 25, 2002 · N708UP · Doug DC871F · Fuselage Main, FrameSDR UPS02839364Skin · crackedINSPECTION TYPE:C1 C-PIT DOOR SKIN IS CRACKED AND GOUGED NEAR LOWER FWD CORNER APPROX STA 1180 AT LONG 32R. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 52-2-0 FIG 4, 52-4-1.Aug 25, 2002 · N708UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS02839295Shear Tie · crackedINSPECTION TYPE:C1 STA 640 SHEAR TIE IS CRACKED BETWEEN LONG 26L TO 27L. REMOVED SHEAR TIE, FABRICATED AND INSTALLED REPAIR IAW SRM 52-2-0 FIG 2A.Aug 25, 2002 · N708UP · Doug DC871F · Fuselage Main, StructureSDR UPS02839294Shear Tie · crackedINSPECTION TYPE:C1 STA 640 SHEAR TIE IS CRACKED BETWEEN LONG 26R TO 27R. TRIMMED SHEAR TIE IAW SRM 53-2-0 FIG 2A, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-2-0 FIG 2A, AND 53-4-1 FIG 10.Aug 25, 2002 · N708UP · Doug DC871F · Fuselage Main, StructureSDR UPS02839446Beam · crackedINSPECTION TYPE:C1 LEFT CENTER SERVICE DOOR BEAM SEGMENT ON DOOR IS CRACKED AT APPROX STA 1295 AT LONG 16L, 3RD LIGHTENING HOLE FROM TOP. CUT INTERCOSTAL/BEAM, FABRICATED AND INSTALLED BEAM SECTION IAW SRM 52-2-0 FIG 2, 52-40-01.Aug 24, 2002 · N708UP · Doug DC871F · Service DoorsSDR UPS02839304Fitting · crackedINSPECTION TYPE:C1 KEEL BEAM FITTING 2ND FROM FRONT IS CRACKED BETWEEN WHEEL WELLS STA 902 APPROX LBL4 TO RBL 4. REMOVED AND REPLACED FITTING IAW DWG 4775262-1, AND SRM 51-1-20D, 51-3-0.Aug 24, 2002 · N708UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA0200118SWing · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LEFT WING LOWER LEADING EDGE SCREW HOLE. REPAIR ACCOMPLISHED, REMOVAL OF PREVIOUS REPAIR, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF FILLER AND DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCAug 23, 2002 · N828BX · Doug DC871F · Wing StructureSDR UPS02839483Skin · crackedINSPECTION TYPE:C1 L1 UPPER FWD DOOR CORNER HAS 4 EACH CRACKS ON EXTERNAL SKIN. FABRICATED DOUBLERS AND FILLER. INSTALLED REPAIR DOUBLERS, FILLERS, DOOR PAN, PAN SPLICES, DOOR SOPS, TORQUE BOX WEBS, SEAL DEPRESSOR AND CALIFORNIA PNL IAW DC8 SRM 51-1-21, 51-1Aug 23, 2002 · N755UP · Doug DC871F · Fuselage Main, Plate/Skin
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