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 UPS00832109Fitting · crackedINSPECTION TYPE: C 1 STA. 380 - 400 LONGERON 31 LT SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3754473,AND SRM. 51-1-20DMar 4, 2000 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832015Fitting · crackedINSPECTION TYPE:C1 STA 1260-1280, STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 51-1-20D.Mar 4, 2000 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00831907Intercostal · crackedINSPECTION TYPE:C1, INTERCOSTAL ON FWD ENTRY DOOR AT FWD UPPER FWD CORNER IS CRACKED STA 25 LONGERON 6L. REPAIRED IAW SRM 52-2-0 FIG 2.Mar 4, 2000 · N748UP · Doug DC871F · Passenger/Crew DoorsSDR RRXA002188Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUSELAGE INT AT STA 857 TO 879 AND L12R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE ASSY IAW DC-8 SRM 51-1-21D FIG 34 SMar 3, 2000 · N8085U · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832072Fitting · corrodedINSPECTION TYPE: C1, STA. 980 AT LONGERON 24 LT STIFFNER FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING I.A.W. DWG.2647420 AND SRM 51-1-20D.Mar 3, 2000 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832070Fitting · crackedINSPECTION TYPE: C1, FLOORBEAM ATTACH FITTING IS CRACKED AT STA. 160, LBL 60, STR. 21 LT. REMOVED, FABRICATED AND RTEPLACED FITTING I.A.W. DWG.3772916 AND SRM 51-1-20D.Mar 3, 2000 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832069Rib · crackedINSPECTION TYPE: C1, RT WING LE AT STA. XS250.089, THE UPPER LE RIB HAS A 10 INCH CRACK. REPAIRED AREA I.A.W. SRM 57-2-0 FIG.2.Mar 3, 2000 · N748UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832048Rib · crackedINSPECTION TYPE: C1, RT WING LE AT STA. XFS397.750, LOWER LE RIB IS CRACKED AT MID SPAN. REPAIRED AREA I.A.W. SRM 57-2-0 FIG.2.Mar 3, 2000 · N748UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832047Fitting · crackedINSPECTION TYPE: C1, STA. 1220 AT STR. 33 RT, SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3755847 AND SRM 51-1-20D.Mar 3, 2000 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832045Fitting · crackedINSPECTION TYPE: C1, STATION 840 AT LONGERON 18 RT, INTERCOSTAL FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING I.A.W. DWG.3779874 AND SRM 51-1-20D.Mar 3, 2000 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832032Fitting · crackedINSPECTION TYPE:C1 STA 857 LONGERON 19R INTERCOSTAL FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779498, AND SRM 51-1-20D.Mar 3, 2000 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832024Fitting · crackedINSPECTION TYPE:C1 INTERCOSTAL FITTING IS CRACKED AT STA 717, STR 18R. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751640 AND SRM 51-1-20D.Mar 3, 2000 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832022Fitting · crackedINSPECTION TYPE:C1 INTERCOSTAL FITTING AT STA 781, STR 13R IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.Mar 3, 2000 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832019Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB AT STA XFS366.5 IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-02-0 FIG 2.Mar 3, 2000 · N748UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00831994Fitting · crackedINSPECTION TYPE:C1, INTERCOSTAL FITTING IS CRACKED AT STA 760 LONGERON 18L. REMOVED AND REPLACED FITTING IAW DWG 4751643 AND SRM 51-1-20D.Mar 3, 2000 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00831993Fitting · crackedINSPECTION TYPE:C1, INTERCOSTAL FITTING IS CRACKED AT STA 740, LONG 13L. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751643 AND SRM 51-1-20D.Mar 3, 2000 · N748UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00831925Skin · crackedINSPECTION TYPE:C1, LEFT CENTER L/E UPPER SKIN IS CRACKED AT XFS 304. REPAIRED IAW SRM 57-2-1 FIG 38.Mar 3, 2000 · N748UP · Doug DC871F · Leading Edge DevicesSDR UPS00831917Rib · crackedINSPECTION TYPE:C1, RIGHT WING L/E RIB IS CRACKED AT XFS 341.500. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 3, 2000 · N748UP · Doug DC871F · Leading Edge DevicesSDR UPS00831916Frame · crackedINSPECTION TYPE:C1, STA 1766 LBL 23 VERTICLE FRAME IS CRACKED LOWER OUTBOARD END. REPAIRED IAW SRM 53-2-0 FIG 1B.Mar 3, 2000 · N748UP · Doug DC871F · Fuselage Main, FrameSDR RRXA002186Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TOP LT WING AFT OF NR 2 ENGINE CENTER SPAR AT STA 252.351, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW PDO8-57-018.Mar 2, 2000 · N8085U · Doug DC871F · Wing, Plate/SkinSDR UPS00832064Access Door · crackedINSPECTION TYPE: C1, RT INBOARD SLOT, UPPER DOOR IS CRACKED. REMOVED AND REPLACED DOOR I.A.W. MM 27-80-00,OP''S CHECH WAS GOOD.Mar 2, 2000 · N748UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS00832057Skin · crackedINSPECTION TYPE: C1, FUSELAGE SKIN AT STA. 1440 AT STR 28 RT IS CRACKED. REPAIRED AREA I.A.W SRM 53-2-0.Mar 2, 2000 · N748UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00832046Frame · crackedINSPECTION TYPE: C1, STA. 55 AT STR. 24 LT, FRAME IS CRACKED. REPAIRED AREA I.A.W. SRM 53-2-0 FIG.2.Mar 2, 2000 · N748UP · Doug DC871F · Fuselage Main, FrameSDR UPS00832044Doubler · corrodedINSPECTION TYPE: C1, RT WING LE AT STA. XFS810.0, THE INTERNAL DOUBLER HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER I.A.W. DWG3641257,Mar 2, 2000 · N748UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS00832115Longeron · corrodedINSPECTION TYPE: C1, STA. 400 LONGERON 21 LT, HAS HEAVY INTERGRANULAR CORROSION. REPAIRED I.A.W. SRM.53-2-5 FIG. 15Mar 2, 2000 · N748UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00832114Spar · corrodedINSPECTION TYPE: C 1 RT WING LE. AUX TANK UPPER SPAR HAS HEAVY CORROSION BETWEEN XFS 88.75 AND XFS 167.5 REMOVED AND REPLACED SPAR CAP I.A.W. DWG.5766433 AND SRM. 51-1-20D, 51-1-21Mar 2, 2000 · N748UP · Doug DC871F · Wing SparSDR UPS00832111Skin · corrodedINSPECTION TYPE: C 1 RT WING LE. UPPER SKIN HAS HEAVY CORROSION UNDER THE SURFACE BETWEEN XFS 583 TO XFS 686 ** REPAIRED I.A.W. 8110-3.Mar 2, 2000 · N748UP · Doug DC871F · Wing, Plate/SkinSDR UPS00832110Rib · crackedINSPECTION TYPE: C 1 RT WING LE. UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED I.A.W. SRM. 57-2-0 FIG. 2Mar 2, 2000 · N748UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832012Skin · crackedINSPECTION TYPE:C1, RT WING L/E LWR SKIN IS CRACKED ATB THE DRAIN HOLE STA XFS591.250. REPAIRED AREA IAW SRM 57-2-0 FIG 2A.Mar 2, 2000 · N748UP · Doug DC871F · Wing, Plate/SkinSDR UPS00832011Skin · crackedINSPECTION TYPE:C1, RT WING UPPER SKIN AT STA XRS172.00 AND FRONT SPAR IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 39.Mar 2, 2000 · N748UP · Doug DC871F · Wing, Plate/SkinSDR UPS00832010Rib · crackedINSPECTION TYPE:C1, RT WING L/E LWR RIB FWD OF ACCESS PANEL OPENING IS CRACKED AT STA XFS810.0. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5769471 AND SRM 51-1 -20D.Mar 2, 2000 · N748UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00832009Skin · crackedINSPECTION TYPE:C,1 RT WING LWR SKIN ABOVE NR 4 PYLON CUT-OUT HAS REPAIR DOUBLER CRACKED, STA XW485.0. REPAIRED AREA IAW SRM 57-2-1A FIG 2.Mar 2, 2000 · N748UP · Doug DC871F · Wing, Plate/SkinSDR UPS00831906Rib · crackedINSPECTION TYPE:C1, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS. 653.750. REPAIRED IAW SRM 57-2-0 FIG 2.Mar 2, 2000 · N748UP · Doug DC871F · Leading Edge DevicesSDR UPS00831988Longeron · crackedINSPECTION TYPE:C123, STA 1767-1780, STR 18L IS CRACKED UNDER THE END FITTING. REPAIRED AREA IAW SRM 53-2-2 FIG 10 AND FIG 11.Feb 29, 2000 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00831987Longeron · crackedINSPECTION TYPE:C123, STA 1767-1780, LONGERON 18R IS CRACKED. REPAIRED AREA IAW SRM 53-2-2 FIG 10 AND FIG 11.Feb 29, 2000 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00831986Stringer · crackedINSPECTION TYPE:C123 STA 1767, STR 18R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1-20D.Feb 29, 2000 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00831885Frame · crackedINSPECTION TYPE:C123, STA 55 AT LONGERON 24R FRAME IS CRACKED. REPAIRED IAW SRM 53-2-0 FIG 2.Feb 29, 2000 · N706UP · Doug DC871F · Fuselage Main, FrameSDR UPS00831918Rib · crackedINSPECTION TYPE:C123, LOWER VERTICLE STAB L/E RIB IS CRACKED RIGHT SIDE AT ZFS 111.00. REPAIRED IAW SRM 55-2-0 FIG 2.Feb 28, 2000 · N706UP · Doug DC871F · Vertical Stabilizer, Spar/RibSDR UPS00832063Keelbeam · corrodedINSPECTION TYPE:C123, KEEL BEAM HAS HEAVY CORROSION AT STA 780, 740, 670 - 680. REPAIRED AREA IAW 8110-3 APPROVED DH SK 706-039.Feb 27, 2000 · N706UP · Doug DC871F · Fuselage Main, KeelSDR UPS00831984Finger Doubler · crackedINSPECTION TYPE:C123, STA 610 BTWN STR 31L-31R, THE FINGER DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5750365 AND SRM 51-1-20D.Feb 27, 2000 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00831983Floorbeam · crackedINSPECTION TYPE:C123, FLOORBEAM END FITTING IS CRACKED AT STA 1200 RBL54. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3754923 AND SRM 51-1-20D.Feb 27, 2000 · N706UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS00831921Rib · crackedINSPECTION TYPE:C123, RIGHT HORIZONTAL L/E RIB IS CRACKED AT XFS 135. REPAIRED IAW SRM 55-2-0 FIG 2.Feb 27, 2000 · N706UP · Doug DC871F · Horizontal Stabilizer, Spar/RibSDR UPS00832058Frame · corrodedINSPECTION TYPE:C123, STA 1220 FRAME/SLIDE RAIL ABOVE STR 35L HAS HEAVY CORROSION ON UPPER FLANGE LWR SURFACE. REMOVED, FABRICATED AND REPLACED FRAME/RAIL IAW 8110-3 APPROVED DH SK 706-958 AND SRM 51-1-20D.Feb 26, 2000 · N706UP · Doug DC871F · Fuselage Main, FrameSDR UPS00831989Skin · corrodedINSPECTION TYPE:C123, FUSELAGE SKIN HAS HEAVY CORROSION AT STA 690 BTWN STR 31L-31R. REPAIRED AREA IAW 8110-3 APPROVED DH SK 706-984.Feb 26, 2000 · N706UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00831985Rib · crackedINSPECTION TYPE:C123, RT WING L/E AT STA XS250.089, THE RIB/END CAP IS CRACKED. REMOVED AND REPLACED END CAP IAW DWG 5769859 AND SRM 51-1-20D.Feb 26, 2000 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00831980Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E AT STA XS520.168, THE UPPER RIB/END CAP IS CRACKED. REMOVED AND REPLACED END CAP IAW DWG 5769857 AND SRM 51-1-20D.Feb 26, 2000 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS00831913Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB CRACKED AT XILD .7095. REPAIRED IAW SRM 57-2-0 FIG 2.Feb 26, 2000 · N706UP · Doug DC871F · Leading Edge DevicesSDR UPS00832035Splice · crackedINSPECTION TYPE:C123 STA 1748.5 LONG 15L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG DC8-53B-009-39, AND SRM 51-1-20D.Feb 25, 2000 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00832007Longeron · crackedINSPECTION TYPE:C123 STA 1754, LONGERON 14L IS CRACKED. REPAIRED AREA IAW SRM 53-2-2 FIG 10.Feb 25, 2000 · N706UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00831982Longeron · crackedINSPECTION TYPE:C123 STA 1748.5, LONGERON 15R IS CRACKED. REPAIRED AREA IAW SRM 53-2-2 FIG 10.Feb 25, 2000 · N706UP · Doug DC871F · Fuselage Main, Longeron/Stringer
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