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 IXXA07SMN003SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION FS 76, LONGERON 35 RIGHT, DOES NOT MEET THE DTA REQUIREMENTS OF MDC 91K0262 REPORT. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION Jan 13, 2007 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN005SSkin · damagedDURING ROUTINE C CHECK, FOUND EXISTING REPAIR AT STATION FS174, LONGERON 34 RIGHT, DOES NOT MEET DTA REQUIREMENTS OF MDC 91K0262 REPORT. REMOVED EXISTING REPAIR REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. AFTER DAMAGE REMOJan 13, 2007 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN004SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION FS104, LONGERON 35 LEFT DOES NOT MEET DTA REQUIREMENTS OF MDC91K0262 REPORT. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREJan 13, 2007 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN015SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND EXISTING REPAIR AT STATION FS 1143, LONGERON 35 RIGHT, DOES NOT MEET THE DTA REQUIREMENTS OF MDC 91K0262 REPORT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED ARJan 13, 2007 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN014SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND INTERIM REPAIR AT STATION FS 518, LONGERON 31 RIGHT. REMOVED EXISTING REPAIR PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED REPAIR PARTS CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLJan 13, 2007 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN022SSkin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND INTERIM REPAIR AT FS 1542, LONGERON 35 LEFT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVAL. FABRICATED EXTERNAL REPAIR DOUBLER AND INTERNJan 13, 2007 · N820BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA07SMN027SSupport Fitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING TRAPEZOIDAL FITTING CRACKED AT STATION 902.000. REMOVED DAMAGED TRAPEZOIDAL SUPPORT FITTING. INSTALLED NEW TRAPEZOIDAL SUPPORT FITTING IAW DOUGLAS DRAWINGS, NUMBER 5750127 AND NUMBER 5750092, DC8 SRM 53-1-0Jan 13, 2007 · N820BX · Doug DC871F · Wing, Attach FittingsSDR IXXA07SMN030SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING OUTBOARD FLAP HAS A NON STANDARD REPAIR ON UPPER SURFACE FROM STATION XF216.000 TO STATION XF220.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORRJan 13, 2007 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA07SMN029SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING-EXTERNAL UPPER SKIN CRACKED AT STATION XRS74.000 STRINGER 11. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND AFTER DAMAGE REMOVEJan 13, 2007 · N820BX · Doug DC871F · Wing, Plate/SkinSDR UPS07848981Fitting · crackedINSPECTION TYPE:C3 NR 2 MAIN FUEL TANK HAS STRINGER END FITTING CRACKED AT STRINGER 55 JUST INBOARD XRS74. REMOVED AND REPLACED STRINGER END FITTING IAW SRM 51-1-20D, 51-3-0 AND 51-01-15.Jan 11, 2007 · N798UP · Doug DC871F · Wing, Longeron/StringerSDR UPS07848994Floorbeam · corrodedINSPECTION TYPE:C3 STA 1700 LBL 26 UNDERSIDE OF FLOORBEAM HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED STRAP AND 2 EA REPAIR ANGLES IAW SRM 51-1-21 AND 53-2-0.Jan 9, 2007 · N798UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS07849055Bulkhead · crackedINSPECTION TYPE:C3 - FOUND AFT PRESSURE BULKHEAD STA 1766 HAS CRACK BTWN L2R & L3R. STOP DRILLED 2 ENDS OF CRACK, FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 53-2-0 FIG 24, 51-1-20D.Jan 8, 2007 · N798UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS07849108Longeron · crackedINSPECTION TYPE:C3 LONGERON 35R CRACKED ALONG RADIUS AT FS 1400-1440. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 51-1-20D, 51-1-21 & DWG 3646937.Jan 7, 2007 · N798UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07849105Longeron · corrodedINSPECTION TYPE:C3 L34L BETWEEN 1420-1440 HAS CORROSION UNDER REPAIR & ON LONGERON. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 53-02-02 FIG 4A, 51-1-20D, 51-1-21 AND DWG 4613495.Jan 7, 2007 · N798UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07849101Longeron · crackedINSPECTION TYPE:C3 LONGERON 35L CRACKED ALONG RADIUS AT FS 1400-1410. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 53-2-2 FIG 4A, 51-1-21, 51-1-20D.Jan 7, 2007 · N798UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07849107Fitting · gougedINSPECTION TYPE:C3 AFT FUSELAGE INSIDE 60 ACCESS AT STA 1766 L11R, LONGERON END FITTING HAS SEVERAL DEEP GOUGES. REMOVED, FABRICATED AND INSTALLED END FITTING IAW SRM 53-02-00 FIG 001F, 51-1-20D AND DWG 7531590.Jan 6, 2007 · N798UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS07849049Stiffener · crackedINSPECTION TYPE:C3 - FOUND EMPENNAGE TAIL SECTION AT STA 1944 RT SIDE, HAT CHANNEL CROSS MEMBER STIFFENER HAS CRACK AT END. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 51-1-21, 53-02-00.Jan 6, 2007 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07849044Stiffener · crackedINSPECTION TYPE:C3 - FOUND EMPENNAGE TAIL SECTION AT STA 1916 INSIDE 62 ACCESS HAT CHANNEL CROSS MEMBER STIFFENER HAS CRACK AT END RT SIDE. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 53-02-00 FIG 001B, 51-1-21 AND 51-1-20D.Jan 6, 2007 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07848998Spar Cap · crackedINSPECTION TYPE:C3 POSSIBLE CRACK AT NR 4 ALT BETWEEN LWR FRT SPAR CAP FLANGE AND STRINGER 64 JUST OUTBOARD XRS428. REMOVED, FABRICATED AND INSTALLED SPAR CAP FLANGE IAW SRM 51-1-20D & DWG 3644046.Jan 6, 2007 · N744UP · Doug DC871F · Wing SparSDR UPS07848941Support Fitting · crackedINSPECTION TYPE:C2 SUPPORT FITTING CRACKED AT STA 980 RBL 24 4 INCHES BELOW CABIN SEAT TRACK. REMOVED AND REPLACED SUPPORT FITTING IAW SRM 51-1-20D AND 51-3-0.Jan 6, 2007 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07848936Rib · crackedINSPECTION TYPE:C3 TWO CRACKS IN END OF RIB AT INBOARD END F/O RIGHT OUTBOARD LEADING EDGE. STOP DRILLED CRACKS, FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 57-02-00-0 FIG 002, 51-1-21 AND 51-1-20D.Jan 6, 2007 · N798UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS07848881Rib · crackedINSPECTION TYPE:C3 CRACKED RIB BEHIND INTERCOSTAL IN RT OB L/E AT XFS 650 PANEL 519B. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-02-00 FIG 002 , 57-03-01 FIG 1, AND 51-1-21.Jan 6, 2007 · N798UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS07849193Fitting · corrodedINSPECTION TYPE:C3 FITTING HEAVY CORROSION AT STA 940 L21R. REMOVED, FABRICATED AND INSTALLED FITTING IAW SAA EA 008-5320-01- A0594, UPS RAA DC8-53-20607, SRM 51-11-8 AND 51-1-20D.Jan 5, 2007 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07849119Cusp Web · corrodedINSPECTION TYPE:C3 MAIN CABIN CUSP HAS HEAVY CORROSION AT STA 1120 LT AROUND FITTING. REPAIRED LT CUSP/SKIN AT STA 1100-1140 IAW RAA DC8-53-20608.Jan 5, 2007 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07849046Fitting · corrodedINSPECTION TYPE:C3 - FOUND LONGERON TO FLOORBEAM FITTING HEAVY CORRODED AND CRACKED AT STA 960 L21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.Jan 5, 2007 · N798UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS07848942Skin · crackedINSPECTION TYPE:C3 LARGE DENT ON NOSE OF RT CTR L/E. CRACKED SKIN, BROKEN RIVETS XFS 392. CUT OUT DAMAGE, FABRICATED FILLER AND DOUBLER. INSTALLED CONICAL WASHERS, FILLER AND DOUBLER IAW SRM 57-02-01-0 FIG 0024, 51-1-21 AND 51-1-20D.Jan 5, 2007 · N798UP · Doug DC871F · Wing, Plate/SkinSDR UPS07848937Skin · wornINSPECTION TYPE:C3 INNER SKIN WORN/CHAFED AT OUTBOARD END OF RIGHT OUTBOARD SLOT VANE. FABRICATED AND INSTALLED INNER DOUBLER IAW SRM 57-3-1 FIG 9.Jan 5, 2007 · N798UP · Doug DC871F · Leading Edge DevicesSDR UPS07848880Rib · crackedINSPECTION TYPE:C3 CRACKED RIB IN RT CTR LE AT XFS 410. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.Jan 5, 2007 · N798UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS07848879Rib · crackedINSPECTION TYPE:C3 CRACKED RIB IN RT CTR LE AT XFS 443. FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 57-02-00 FIG 002 51-1-20D AND 51-1-21.Jan 5, 2007 · N798UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS07848862Rib · crackedINSPECTION TYPE:C3 RIB CRACKED UNDER GUSSET IN RT CTR LE NEXT TO PANEL 523. STOP DRILLED CRACK. FABRICATED 2. REPAIR ANGLES AND INSTALLED IAW SRM 57-03-01, 57-02-00 FIG 002, 51-1-20 AND 51-1-21D.Jan 5, 2007 · N798UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS07848840Stiffener · crackedINSPECTION TYPE:C2 RADIOGRAPHIC INSP DETECTED A CRACK ON THE LT WING AT STA XRS437.00 VERTICAL STIFFENER IN THE LEADING EDGE. REMOVED REPAIR FROM VERTICAL STIFFENER IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER, AND REPAIR ANGLE AT LT WING STA XRSJan 5, 2007 · N744UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS07849227Skin · crackedINSPECTION TYPE:C3 HFEC & VISUAL INSP DETECTED A .225 INCH CRACK ON THE C-4 (D-PIT) LOWER FORWARD JAMB CORNER AS MARKED ON PART. REMOVED AND REPLACED FUSELAGE SKIN IAW SRM 51-1-20D, 51-1-21, 51-1-22, FS 1350 - 1490 L31R - L31L.Jan 4, 2007 · N798UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS07849109Skin · crackedINSPECTION TYPE:C3 LEFT UPPER WING SKIN POSSIBLE CRACKED AT XCW69 AFT SPAR VERY I/B SIDE. CUT OUT DAMAGE, FABRICATED 2 EA DOUBLERS, 1 EA FILLER AND 1 EA ANGLE AND INSTALLED IAW SRM 57-02-01-0 FIG 020 AND 51-1-21.Jan 4, 2007 · N798UP · Doug DC871F · Wing, Plate/SkinSDR UPS07849094Skin · crackedINSPECTION TYPE:C3 HFEC & VISUAL INSP DETECTED A .335 INCH CRACK ON THE C-2 (B-PIT) LOWER AFT JAMB CORNER. CRACK EXTENDS FROM EDGE OF SKIN TO FASTENER HOLE AS MARKED. REMOVED AND REPLACED BELLY SKIN FROM FS 450 TO FS 610 L31R TO L31L IAW SRM 51-1-21, 51-1-20Jan 4, 2007 · N798UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS07849053Skin · crackedINSPECTION TYPE:C3 - FOUND EXT FUSE SKIN HAS 1/4" CRACKED AT L1 DOOR HOLD OPEN RECPT. REMOVED EDGE DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-00 FIG 001R, 51-3-0 AND EO DC8-5330-19684.Jan 4, 2007 · N798UP · Doug DC871F · Passenger/Crew DoorsSDR UPS07849052Intercostal · crackedINSPECTION TYPE:C3 - FOUND IB UPPER RIB OF OB SLOT DOOR STRUCTURE HAS 4" CRACK,CENTER LEADING EDGE LW ABOVE PNEUMATIC DUCT. REMOVED, STOP DRILLED CRACK, FABRICATED AND INSTALLED 1 INTERCOSTAL, AND 1 REPAIR ANGLE IAW SRM 51-1-20D, 57-03-01-0, 51-03-02.Jan 4, 2007 · N798UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS07848996Longeron · crackedINSPECTION TYPE:C3 LONGERON CRACKED AT STA 1766 L14R. REMOVED CRACKED LONGERON, FABRICATED & INSTALLED REPLACEMENT LONGERON AND 2 EA REPAIR SPLICES IAW SRM 53-05-0, 51-02-00, 53-02-02, 51-3-0, 51-1-20D.Jan 4, 2007 · N798UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07848993Longeron · crackedINSPECTION TYPE:C3 LONGERON CRACKED AT STA 1766 L14L. REMOVED DAMAGED LONGERON, FABRICATED AND INSTALLED REPLACEMENT LONGERON AND 2 EA SPLICES IAW SRM 51-1-21, 53-02-02-0 FIG 011, AND 51-1-20D.Jan 4, 2007 · N798UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07848980Attach Angle · crackedINSPECTION TYPE:C3 AFT PRESSURE BULKHEAD TO LONGERON INTERCOSTAL ATTACH ANGLE CRACKED AT STA 1766 L6R. REMOVED, FABRICATED AND INSTALLED ATTACH ANGLE IAW SRM 51-1-21, 51-3-2, 51-20D AND DWG 5773844.Jan 4, 2007 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07848978Attach Angle · crackedINSPECTION TYPE:C3 AFT PRESSURE BULKHEAD TO LONGERON INTERCOSTAL ATTACH ANGLE CRACKED AT STA 1766 L6L. REMOVED, FABRICATED AND INSTALLED ATTACH ANGLE IAW SRM 51-1-21, 51-3-2, 51-1-20D AND DWG 5773844.Jan 4, 2007 · N798UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS07848954Seat Track · wornINSPECTION TYPE:C3 CAPTAIN`S AFT SEAT TRACK I/B WORN AND O/B HAS ELONGATED HOLES. REMOVE AND REPLACE CAPTAIN`S AFT I/B AND O/B SEAT TRACKS IAW SRM 51-1-20D, 51-03-02 AND 51-3-0.Jan 4, 2007 · N798UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07848873Bulkhead · crackedINSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CRACKED AT STA 1766 LBL25. CUT OUT DAMAGE, FABRICATED AND INSTALLED 1 FILLER AND 2 DOUBLERS IAW SRM 53-2-5 FIG 14A.Jan 4, 2007 · N798UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS07848845Skin · crackedINSPECTION TYPE:C2 LT HORIZ STAB L/E UPPER SKIN CRACKED AT STA XFS 60. CUT OUT DAMAGED AREA ON HORIZ STAB LT L/E UPPER SKIN AT STA XFS 60 IAW SRM 55-02-01-0 FIG 4. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER ON LT HORIZ STAB L/E UPPER SKIN STA XFS 60 Jan 4, 2007 · N744UP · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR UPS07849091Pressure Panel · corrodedINSPECTION TYPE:C2 COCKPIT SUBFLOOR HORIZ PRESS PANEL STA -80 LBL 24 HAS EXFOLIATION CORROSION. REPAIRED COCKPIT SUBFLOOR HORIZ PRESS PANEL AT STA -80 LBL 24 IAW SAA EA 008-5330-01-A0608, UPS EO DC8-5330-26007-A, BAC SERVICE MSG 1-275991347, AND FAA FORM 8100Jan 3, 2007 · N744UP · Doug DC871F · Fuselage Floor PanelSDR UPS07849075Window Frame · corrodedINSPECTION TYPE:C2 RIGHT & LEFT WINDOW FRAME Z-ANGLES (CENTER WINDSHIELD) ARE CORRODED AND PITTED. REPAIRED CENTER WINDSHIELD Z-ANGLE IAW SAA EA 008-5310-01-A0570 UPS EO DC8-5310-25945-A, BAC MSG 1-269510850, AND FAA FORM 8100-9.Jan 3, 2007 · N744UP · Doug DC871F · Fuselage Main, StructureSDR UPS07848976Longeron · corrodedINSPECTION TYPE:C2 CORROSION OUT OF LIMITS ON LONGERON L35R STA 50-70. REMOVED LONGERON L35R AT STA 50-70 IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON L35R AT STA 50-70 IAW DWG 3702969, AND SRM 51-1-21, AND 51-1-20D.Jan 3, 2007 · N744UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07848975Fitting · corrodedINSPECTION TYPE:C2 CORROSION OUT OF LIMITS ON END FITTING AT STA 70 L35R. REMOVED AND REPLACED LONGERON END FITTING AT STA 70 L35R IAW SRM 51-1-21, AND SRM 51-1-20D.Jan 3, 2007 · N744UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07848926Angle · crackedINSPECTION TYPE:C2 LEFT HORIZ STAB LEADING EDGE VERY INBOARD UPPER T-ANGLE CRACKED. CUT OUT DAMAGED AREA ON INBOARD UPPER T-ANGLE ON LT HORIZ STAB LEADING EDGE IAW SRM 51-1-21, RECEIVED, LOCATED, DRILLED UP AND INSTALLED T-ANGLE FITTING ON THE LEFT HORIZ STABJan 3, 2007 · N744UP · Doug DC871F · Horizontal Stabilizer Miscellaneous StructureSDR UPS07848838Longeron Splice · crackedINSPECTION TYPE:C2 C-PIT STA 1040 L31L, LONGERON SPLICE FITTING CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING AT STA 1040 L31L IAW SRM 51-01-20D, 51-03-02.Jan 3, 2007 · N744UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS07849074Floorbeam · crackedINSPECTION TYPE:C2 FLOORBEAM VIEWED FROM A-PIT STA 240 LBL 36 HAS A 9 INCH CRACK. REPAIRED FLOORBEAM AT STA 240 LBL 36 IAW SAA EA008-5310-01-A00586 UPS RAA DC8-53-20605-A, BAC MSG 1-271080190, AND FAA FORM 8100-9.Jan 2, 2007 · N744UP · Doug DC871F · Fuselage Main, Floor Beam
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