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 RRXA991313Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, R-2 DOOR FWD FRAME INSIDE WEB AT STA 1620, LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED 2 EACH FITTINGS IAW DC8 SRMJan 11, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991312Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LT UPPER CUSP DOOR FRAME FITTING AT STA 1620, LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOOR FRAME FITTING IAW DC8Jan 11, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991286Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, SKIN, AT SCREEN HOLE RT WING O/B L/E I/B SEGMENT AT STA XFS 676.756 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER ANDJan 11, 1999 · N8085U · Doug DC871F · Wing, Plate/SkinSDR RRXA991037Fitting · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK, EXTENDING FROM BOLT HOLE RT I/B FLAP I/B HINGE ATTACH FITTING AT XW 3.125. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. MACHINE REPAIRED FITTING AND INSTALLED IAW FAA APPRJan 11, 1999 · N8085U · Doug DC871F · Wing Miscellaneous StructureSDR UPS99828609Floorbeam · corrodedINSPECTION TYPE-C, FS 879 FLOORBEAM AT LBL 60 IS CORRODED BEYOND LIMITS. REPAIRED FLOORBEAM IAW DH SK701-681.Jan 10, 1999 · N701UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS99828584Doubler · corrodedINSPECTION TYPE-C3, INTERNAL DOUBLER AT LONG 31L FS 1620 TO 1670 IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DHC SK713-220 AND SRM 51-1-21.Jan 10, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828583Doubler · crackedINSPECTION TYPE-C3, LONG 31R BETWEEN FS 400 TO 450 IS CRACKED AND CORRODED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5755271 AND SRM 51-1-20D AND 51-1-21.Jan 10, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828568Doubler · corrodedINSPECTION TYPE-C3, FS 354 TO 450 AT LONG 31L, THE FINGER DOUBLER WAS CORRODED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 AND 51-1-20D, 51-1-21.Jan 10, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828567Doubler · corrodedINSPECTION TYPE-C3, FS 210 TO 354 AT LONG 31L, THE FINGER DOUBLER WASS CORRODED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5755271 AND SRM 51-1-20D, 51-1-21.Jan 10, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828510Longeron · corrodedINSPECTION TYPE-C3, LONG 35L AT FS 360 TO 380 HAS MODERATE CORROSION. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D.Jan 10, 1999 · N713UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS99828509Longeron · corrodedINSPECTION TYPE-C3, LONG 32R AT FS 438 HAS CORROSION. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D.Jan 10, 1999 · N713UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS99828508Longeron · corrodedINSPECTION TYPE-C3, LONG 34L FS 390 TO 450 HAS SEVERE CORROSION. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 5755271 AND SRM 51-1-20D.Jan 10, 1999 · N713UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS99828507Longeron · corrodedINSPECTION TYPE-C3, FS 390 TO 450, LONG 33L HAS CORROSION INSIDE HAT CHANNEL. REMOVED, FABRICATED AND REPLACED LONGERON IAW SRM 51-1-20D, AND DWG 5755271.Jan 10, 1999 · N713UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS99828502Longeron · corrodedINSPECTION TYPE-C3 LONG 33R IS CORRODED AT FS 190 THRU 300. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D.Jan 10, 1999 · N713UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS99828501Skin · crackedINSPECTION TYPE-C3, FUSELAGE SKIN AT FS 60, LONG 12L, HAS A .150 CRACK. CUT OUT DAMAGED AREA AND REPAIRED IAW DHC SK713-223.Jan 10, 1999 · N713UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS99828404Longeron · corrodedINSPECTION TYPE:C3, LONGERON 35L AT FS 390-450 HAS SEVERE CORROSION. REMOVED, FABRICATED, AND REPLACED LONGERON IAW SRM 53-4-1 AND 51-1-20D.Jan 10, 1999 · N713UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA991317Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, MARKER BEACON MOUNTING SKIN BETWEEN STA 640 AND STA 660 AND BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERINGJan 10, 1999 · N8085U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA991309Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ATTACH ANGLE AT STA 1100, LONGERON 29 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLES IAW DC8 SRM 51-1-9. (CORROSION DAMAGEJan 10, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA991308Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BILGE FRAME AT NUTPLATES, AT STA 1040, BETWEEN LONGERONS 28 LEFT AND LONGERON 33 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPJan 10, 1999 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA991304Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, ACCESSORY, FWD, FRAME AT STA 680, BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR Jan 10, 1999 · N8085U · Doug DC871F · Fuselage Main, FrameSDR UPS99828487Clip · corrodedINSPECTION TYPE-C, FS 855 REAR SPAR IS CORRODED BEYOND LIMITS AT LBL 28. REMOVED AND REPLACED DAMAGED CLIP IAW SRM 51-1-20D AND 51-3-0.Jan 9, 1999 · N701UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS99828462Fitting · crackedINSPECTION TYPE:C3, STA 1490 AT LONG 34R, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 36194343 AND SRM 51-1-20D.Jan 9, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828423Longeron · crackedINSPECTION TYPE-C, LONG 35R FS 85 TO 95 IS CRACKED UNDER THE SPLICE. REMOVED, FABRICATED AND REPLACED LONGERON IAW SRM 53-2-2 AND 51-1-2OD.Jan 9, 1999 · N701UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA991307Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BILGE, OUTPLATES TOP CAP AND AFT FACE OF WEB FRAME, AT STA 1260 BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FAJan 9, 1999 · N8085U · Doug DC871F · Fuselage Main, FrameSDR RRXA991306Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BILGE UPPER CAP UNDER NUT PLATE AND WEB AT STA 1306, BETWEEN LONGERONS 34 LEFT AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ANJan 9, 1999 · N8085U · Doug DC871F · Fuselage Main, FrameSDR UPS99828582Doubler · corrodedINSPECTION TYPE-C3, INTERNAL DOUBLER AT LONG 31R FS 1600 TO 1670 IS CORRODED. REPAIRED DOUBLER IAW DHC SK713-220.Jan 8, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828571Longeron · crackedINSPECTION TYPE-C3, LONG 33R WAS CRACKED AT FS 1580. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D.Jan 8, 1999 · N713UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS99828570Skin · crackedINSPECTION TYPE-C3, THE FUSELAGE SKIN AT THE UPPER AFT CORNER OF THE RT AFT SERVICE DOOR WAS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 16.Jan 8, 1999 · N713UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS99828506Fitting · corrodedINSPECTION TYPE-C3, LONG 34L END FITTING CORRODED AT FS 1640. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Jan 8, 1999 · N713UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828403Rib · crackedINSPECTION TYPE:C3, RT WING L/E RIB AT XS 454.976 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 8, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828402Rib · crackedINSPECTION TYPE:C3, RT WING L/E RIB AT XS 442.185 IS CRACKED AT THE UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 8, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828401Rib · crackedINSPECTION TYPE:C3, RT WING L/E RIB AT XFS 304.00 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 8, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR RRXA991302Support · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BILGE GILL LINER ATTACHMENT SUPPORT FROM STA 1420R TO STA 1440R AT LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SUPPJan 8, 1999 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS99828722Rib · crackedINSPECTION TYPE:C, LT WING L/E RIB AT XFS 685.0 IS CRACKED AT THE AFT UPPER FASTENER. REPAIRED IAW SRM 57-2-0.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828720Rib · crackedINSPECTION TYPE:C RT WING L/E RIB AT 467.897 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828657Seat Track · corrodedINSPECTION TYPE-C3, SECOND OBS SEAT TRACKS ARE CORRODED UNDER THE NUT PLATES. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-20D AND 51-3-0.Jan 7, 1999 · N713UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS99828569Rib · crackedINSPECTION TYPE-C3, LT WING L/E RIB AT XOLDI 6.225, I/B SIDE IS CRACKED ABOVE THE PNEU DUCT. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828505Rib · crackedINSPECTION TYPE-C3, LT WING L/E RIB AT XFS 304.0 IS CRACKED AT THE FWD PNEU DUCT SUPPORT ROD MOUNT FITTING. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828504Rib · crackedINSPECTION TYPE-C3, LT WING L/E RIB AT XFS 710.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828503Rib · crackedINSPECTION TYPE-C3, RT WING L/E RIB AT XFS 304.0 IS CRACKED AT THE FWD PNEU DUCT SUPPORT ROD MOUNT FITTING. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828472Doubler · crackedINSPECTION TYPE:C3, RT WING L/E LWR SKIN AT STA XFS341.5, THE T/E INTERNAL DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW SRM 57-3-0 FIG 7.Jan 7, 1999 · N713UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS99828471Rib · crackedINSPECTION TYPE:C3, LT WING L/E RIB AT STA XFS435.789 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828470Rib · crackedINSPECTION TYPE:C3, LT WING L/E RIB AT STA XFS622.5 IS CRACKED AT THE AFT LWR FAST. REPAIRED AREA IAW SRM 57-2-0.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828399Rib · crackedINSPECTION TYPE:C3, LT WING L/E RIB AT XFS 360.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828398Rib · crackedINSPECTION TYPE:C3, LT WING L/E RIB AT XFS 722.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACKED AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828397Rib · crackedINSPECTION TYPE:C3, LT WING L/E RIB AT XFS 778.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828396Rib · crackedINSPECTION TYPE:C3, LT WING L/E RIB AT XFS 860.0 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828395Rib · crackedINSPECTION TYPE:C3, RT WING L/E RIB AT XFS 716.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828394Rib · crackedINSPECTION TYPE:C3, RT WING L/E RIB AT XFS 722.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS99828393Rib · crackedINSPECTION TYPE:C3, RT WING L/E RIB AT XFS 741.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Jan 7, 1999 · N713UP · Doug DC871F · Wing, Rib/Bulkhead
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