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 UPS04842136Frame · crackedINSPECTION TYPE: C1, AIR CONDITIONING ACCESSORY COMPT AT FS 56 ABOVE L24R FRAME IS CRACKED AT PNEUMATIC DUCT STANDOFF ATTACH BRACKET. REMOVED CRACKED FRAME SECTION. RECEIVED NEW -5 AND -17, -19 SPLICES. HEAT TREATED, LOCATED, DRILLED FRAME SECTION AND SPLIFeb 24, 2004 · N752UP · Doug DC871F · Fuselage Main, FrameSDR UPS04841957Battery Pack · dischargedINSPECTION TYPE: N/A AS REPORTED FROM THE FLIGHT CREW EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. OK FOR SERVICE.Feb 23, 2004 · N718UP · Doug DC871F · Emergency LightingSDR IXXA0400010OWindow · delaminatedDURING TAKEOFF FROM KMCO F/O'S WINDOW STARTED DELAMINATION. CREW SHUTOFF WINDOW HEAT AND DELAMINATING STOPPED. CREW RETURNED AIRCRAFT TO KMCO AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. AFeb 19, 2004 · N821BX · Doug DC871F · Flight Compartment WindowsSDR UPS04841952Intercostal · crackedINSPECTION TYPE: C3, STATION 25 CUSP WEB/INTERCOSTAL IS CRACKED AT LONG 21L. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-2-0 FIG 1B.Feb 17, 2004 · N703UP · Doug DC871F · Fuselage Miscellaneous StructureSDR GKZR200482309Keelbeam · crackedRIGHT KEEL BEAM AREA, FORMER JUST I/B OF MLG DOOR ACT MOUNT CRACKED. CRACK WAS STOP DRILLED BUT WENT PAST, CRACK 3 INCHES ABOVE END OF 1ST CRACK GOES FWD AND AFT. REMOVED FORMED WEB IAW DC-8 SRM 51-1-21. FABRICATED WEB MATERIAL USED 7075 .071. INSTALLED WEB Feb 17, 2004 · N823BX · Doug DC871F · Fuselage Main, KeelSDR GKZR200482308Doubler · crackedRUDDER BOTTOM SIDE FWD AT FILLET ON RT SIDE DOUBLER CRACKED AT RIVET IN NUT PLATE TO END OF DOUBLER. REMOVED SEALANT AND PAINT FROM AREA NO EVIDENCE OF A CRACK IAW DC-8 SRM 51-1-8. TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND SEALED IAW DC-8 SRM 51-1-16 PG. 1-9.Feb 17, 2004 · N823BX · Doug DC871F · Rudder, Plate/SkinSDR GKZR200482307Splice · crackedRIGHT LONGERON SPICE AT R34 STA 1490 CRACKED. REMOVED LONGERON SPLICE IAW DC-8 SRM 51-1-21. PERFORMED NDT FOUND NO CRACK IAW DC-8 SRM 51-5-2 TREATED AND PRIMED IAW DC-8 SRM. INSTALLED LONGERON SPLICE IAW DC-8 SRM 51-1-21. (CLOSED)Feb 17, 2004 · N823BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR GKZR200482306Clip · crackedLEFT WING UPPER CLIP INSIDE NR 1M ACCESS HOLE 505C AT STA 252-351 BETWEEN REAR SPAR NR 1 STRINGER CLIP CRACKED. REMOVED LT UPPER WING CLIP INSIDE NR 1 MAIN TANK ACCESS HOLE 505C AT STA 252-351 ON STRINGER NR 1. FABRICATED AND INSTALLED REPLACEMENT PART IAW DCFeb 17, 2004 · N823BX · Doug DC871F · Wing Miscellaneous StructureSDR GKZR200482304Structure · crackedLT WING INSIDE NR 1A FUEL TANK FROM ACCESS PANEL 505B BETWEEN STA. 495.665 AND 508.977 LWR STRINGER NR 53 CRACKED. CUT AND REMOVED STRINGER NR 53 BETWEEN STA 495 AND 508 IAW DC-8 SRM 57-2-2. CUT AND INSTALLED REPLACEMENT STRINGER AND SPICES IAW DC-8 SRM 57-2-Feb 17, 2004 · N823BX · Doug DC871F · Wing Main, Frame StructureSDR GKZR200482305Stringer · crackedLEFT UPPER WING THRU ACCESS HOLE 506A AT STA 408.343 NR 7 UPPER STRINGER FROM REAR SPAR CRACKED AT SPLICE. CRACKED BLENDED OUT IAW DC-8 SRM 57-2-0. (CLOSED)Feb 17, 2004 · N823BX · Doug DC871F · Wing, Longeron/StringerSDR UPS04841951Bearing · corrodedINSPECTION TYPE: C3, LEFT HORIZONTAL STAB HINGE BEARING WILL NOT ACCEPT GREASE. DISASSEMBLED HINGE. FOUND STAB BEARING BORE CORRODED. REPAIRED PER SAA SK 703-677 AND UPS EO DC8-5510-19991-A.Feb 12, 2004 · N703UP · Doug DC871F · Horizontal Stabilizer StructureSDR UPS04841915Fitting · crackedINSPECTION TYPE: C3, STATION 1270 LONG 35L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759258 AND SRM 51-1-20D, 51-3-0.Feb 11, 2004 · N703UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04841930Angle · crackedINSPECTION TYPE: C3, STATION 55, LBL 50 TWO INTERCOSTAL ANGLE SUPPORTS ARE CRACKED. REMOVED, FABRICATED AND INSTALLED ANGLE SUPPORTS IAW DWG 4888755, 4888754 AND SRM 51-1-21.Feb 8, 2004 · N703UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04841857Rib · crackedINSPECTION TYPE: C3, RT WING O/B LEADING EDGE LOWER RIB IS CRACKED AT XFS 825. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.Feb 8, 2004 · N703UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04841836Duct · overtempVERY STRONG ODOR OF FUEL IN COCKPIT THROUGH ENTIRE FLIGHT. RAN PACKS ON GROUND FOR 30 MINS, COULD NOT DETECT ANY KIND OF ODOR IN COCKPIT. SUSPECT ODOR DUE TO OVERTEMP OF DUCT, NO DEFECTS NOTED ON GROUND.Feb 6, 2004 · N752UP · Doug DC871F · Cabin Cooling SystemSDR UPS04841851Battery Pack · inoperativeEMERGENCY LIGHTS INOP DUE TO POWER ON AC AND LIGHT SWITCH LEFT IN ARMED POSITION. REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK.Feb 5, 2004 · N750UP · Doug DC871F · Emergency LightingSDR UPS04841868Skin · crackedINSPECTION TYPE: C3, FUSELAGE SKIN IS CRACKED AT FASTENER HOLE AT STATION 1342 LONG 31R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.Feb 4, 2004 · N703UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS04841929Longeron · crackedINSPECTION TYPE: C3, STATION 1270 LONG 36 IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STATION 1270 - 1310, FABRICATED AND INSTALLED STRAP DOUBLERS AND CHANNELS IAW UPS ENGINEERING FILE DC8-53-20393 AND SAA SK 703-514.Feb 3, 2004 · N703UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR GKZR200482303Floor Panel · delaminatedMAIN CARGO FLOOR FORM PALLET POSITION 4 AFT HAS MULTIPULE AREAS OF DISBONDING. REMOVED ALL HARDWARE FROM MAIN CARGO COMPARTMENT FLOOR P4 AFT IAW DC-8 SRM 51-03-00. FABRICATED REPLACEMENT FLOOR BOARDS FROM GIL FAB BOARD 16 EA. FROM 5042B ATI PO 16802. TREATED Feb 3, 2004 · N823BX · Doug DC871F · Fuselage Floor PanelSDR GKZR200482302Support · crackedLEFT MLG SUPPORT MITTING CRACKED (TRAP) TOP FLANGE. REMOVED LT TRAP FITTING IAW DC-8 MM 20-16-0. FITTED AND DRILLED NEW L/H TRAP IAW ATI DRAWING 5750127 SPOT FACED HOLES AS REQUIRRED. TREATED AND PRIMED IAW DC-8 SRM 51-1-8. TORQUED LT TRAP FITTING IAW SB DC-8Feb 3, 2004 · N823BX · Doug DC871F · Fuselage, Landing Gear Attach FittingsSDR GKZR200482301Skin · corrodedRIGHT SIDE STA 35 L30 SKIN HAS CORROSION. REMOVED FASTENERS IAW DC-8 SRM 51-1-20, DRILLED NEW DOUBLER PART NUMBER 5649028U AND INSTALLED IAW DC-8 SRM 51-1-21, DRILL AND INSTALLED NEW LONGERON PART NUMBER 3648667 IAW DC-8 SRM 51-1-21. (CLOSED)Feb 3, 2004 · N823BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS04841856Finger Doubler · corrodedINSPECTION TYPE: C3, INTERNAL FINGER DOUBLER IS CORRODED BEYOND LIMITS STATION 1260-1350 LONGERON 31R. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW SRM 53-4-1 FIG 17A, 51-1-20D, 51-1-21.Feb 3, 2004 · N703UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS04841848Rib · crackedINSPECTION TYPE: C3, RIGHT WING CENTER L/E LOWER RIB HAS A HOLE WORN THRU AT XFS 416. REMOVED DAMAGE, NDT VERIFIED NO CRACKS AT DAMAGE REMOVAL. FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.Feb 3, 2004 · N703UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04841844Bracket · crackedINSPECTION TYPE: C3, RIGHT O/B AILERON HINGE BRACKET IS CRACKED AT STATION 610.882. REMOVED AND REPLACED BRACKET IAW DWG 3653812 AND SRM 51-1-21.Feb 3, 2004 · N703UP · Doug DC871F · AileronsSDR UPS04841797Battery Pack · unserviceableEMERGENCY LIGHTS INOP. BATTERY FAILED REPLACED EMERGENCY LIGHT BATTERY.Feb 2, 2004 · N750UP · Doug DC871F · Emergency LightingSDR UPS04841942Fitting · crackedINSPECTION TYPE: C3, STATION 1200 LONG 27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755849 AND SRM 51-1-20D.Feb 1, 2004 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04841931Angle · crackedINSPECTION TYPE: C3, STATION 1235, LONG 33R SUPPORT ANGLE IS CRACKED AND INTERCOSTAL IS GOUGED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED SUPPORT ANGLE AND INTERCOSTAL IAW DWG 9754949, 4758514 AND SRM 51-1-20D.Feb 1, 2004 · N703UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04841921Skin · corrodedINSPECTION TYPE: C3, FUSELAGE SKIN IS CORRODED BEYOND LIMITS AT STATION 1265 AT LONG 36. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.Feb 1, 2004 · N703UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS04841917Fitting · crackedINSPECTION TYPE: C3, STATION 1240 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D.Feb 1, 2004 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04841890Rib · crackedINSPECTION TYPE: C3, RIGHT WING L/E UPPER RIBS ARE CRACKED AT XFS 410.25, XFS 347.75, XFS 354. STOPDRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.Feb 1, 2004 · N703UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04841889Rib · crackedINSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XS 478.897. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.Feb 1, 2004 · N703UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04841887Rib · crackedINSPECTION TYPE: C3, RT WING L/E UPPER RIB IS CRACKED AT XFS 728.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.Feb 1, 2004 · N703UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04841886Rib · crackedINSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 641.25. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.Feb 1, 2004 · N703UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04841866Fitting · crackedINSPECTION TYPE: C3, STA 1270 LONG 36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3759222 AND SRM 51-1-20D.Feb 1, 2004 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04841854Attach Fitting · crackedINSPECTION TYPE: C3, LONGERON 35R INTERCOSTAL TO FRAME ATTACH FITTING AT STA 1230 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758570 AND SRM 51-1-20D.Feb 1, 2004 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04841843Doubler · crackedINSPECTION TYPE: C3, RT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 5760545 AND SRM 51-1-21, 51-1-20D.Feb 1, 2004 · N703UP · Doug DC871F · Wing, Plate/SkinSDR UPS04841943Intercostal · crackedINSPECTION TYPE: C3, STATION 55 LBL 50 INTERCOSTAL IS CRACKED BELOW CEILING. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5758542 AND SRM 51-1-20D.Jan 31, 2004 · N703UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04841927Support · crackedINSPECTION TYPE:C3 A/C BAY CEILING SUPPORT ANGLE IS CRACKED AT STATION 55 LBL 30. REMOVED, FABRICATED AND REPLACED ANGLE FITTING IAW DWG 4774654 AND SRM 51-1-20D.Jan 31, 2004 · N703UP · Doug DC871F · Fuselage Main, StructureSDR UPS04841919Support Fitting · crackedINSPECTION TYPE: C3, FLOORBEAM SUPPORT FITTINGS ARE CRACKED AT STATION 798 AND 822 AT LBL 23. REMOVED, FABRICATED AND REPLACED FITTINGS IAW DWG 3773906 AND SRM 51-1-20D.Jan 31, 2004 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04841885Floor Support · crackedINSPECTION TYPE: C3, MAIN CABIN FLOOR SUPPORT CHANNEL IS CRACKED AT STA 863 AT LBL 23. REMOVED, FABRICATED AND REPLACED SUPPORT CHANNEL IAW DWG 5758265 AND SRM 51-1-20D.Jan 31, 2004 · N703UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04841867Floor Support · crackedINSPECTION TYPE: C3, FLOOR SUPPORT FITTING IS CRACKED AT STATION 340 LONG 36-33L. REMOVED AND REPLACED FITTING IAW DWG 9754002 AND SRM 51-1-20D.Jan 31, 2004 · N703UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04841855Fitting · crackedINSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STA 798, RBL 23. REMOVED AND REPLACED FITTING IAW DWG 3773906 AND SRM 51-1-20D.Jan 31, 2004 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04841847Support Fitting · crackedINSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STATION 742 RBL 23. REMOVED AND REPLACED FITTING IAW DWG 3773906 SRM 51-1-20D, 51-3-0.Jan 31, 2004 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04841846Support Fitting · crackedINSPECTION TYPE: C3, MAIN CABIN FLOORBEAM SUPPORT FITTING IS CRACKED AT STA 822 RBL 23. REMOVED AND REPLACED FITTING IAW DWG 3773906 AND SRM 51-1-20D.Jan 31, 2004 · N703UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04841920Support Fitting · crackedINSPECTION TYPE: C3, RIGHT O/B FLAP HINGE 219 I/B SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3653781 AND SRM 51-1-20D.Jan 30, 2004 · N703UP · Doug DC871F · Trailing Edge FlapsSDR UPS04841884Rib · crackedINSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 835. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.Jan 30, 2004 · N703UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04841883Rib · crackedINSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 778.75. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.Jan 30, 2004 · N703UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04841882Rib · crackedINSPECTION TYPE: C3, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 791.250. STOPODRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.Jan 30, 2004 · N703UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04841881Rib · crackedINSPECTION TYPE: C3, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 766.250. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.Jan 30, 2004 · N703UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04841880Rib · crackedINSPECTION TYPE:C3 LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 372.75, XFS 379. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.Jan 30, 2004 · N703UP · Doug DC871F · Wing, Rib/Bulkhead
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