Douglas DC-8-71F

Service difficulty reports · 8,938

Newest first. General aviation reporting is voluntary.

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 RRXA003197Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK FORMER AFT OF INTERCOSTAL BELOW SPLICE STRAP AT STA XFS 410.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 3, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR UPS00833859Longeron · corrodedINSPECTION TYPE:C1, STA 1705 LONG 30L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 5649329, AND SRM 51-1-20D.Oct 3, 2000 · N779UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00833858Shear Tie · corrodedINSPECTION TYPE:C1, STA 1760 LONG 28L - 28R 8 SHEAR TIES ARE CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED SHEAR TIES IAW 5612148, AND SRM 51-1-21.Oct 3, 2000 · N779UP · Doug DC871F · Fuselage Main, StructureSDR UPS00833853Finger Doubler · crackedINSPECTION TYPE:C1, STA 1690 - 1890 FINGER DOUBLERS IS CRACKED AT LONG 28R. REMOVED, FABRICATED, AND REPLACED DOUBLERS IAW DWG 5649328, AND SRM 51-1-21.Oct 3, 2000 · N779UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833820Circuit Breaker · damagedINSPECTION TYPE:A CK EMERGENCY EXIT LIGHTING CIRCUIT BREAKER (5A) DAMAGED. REPLACED C/B B1-115 - REF WDM 33-50-01, PG 1,SH 1, SYS OPS CK NORMAL IAW M/M 33-50-01.Oct 3, 2000 · N702UP · Doug DC871F · Emergency LightingSDR UPS00834221Doubler · crackedINSPECTION TYPE:C1, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335.25. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21.Oct 2, 2000 · N779UP · Doug DC871F · Wing, Plate/SkinSDR UPS00833849Rib · crackedINSPECTION TYPE:C1, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 310.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.Oct 2, 2000 · N779UP · Doug DC871F · Wing, Rib/BulkheadSDR RRXA003202Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER STR SPLICE END BETWEEN STA XRS 408 AND 393, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 29, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003201Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT REAR SPAR ATTACH T FITTING AT STA XRS 446, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 29, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003200Stringer Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LWR STR CLIP BETWEEN STRINGERS 62 & 63 ON THE LT UPPER WING NR 1 ALT THRU ACCESS HOLE 505A AND THRU MID SPAR ACCESS HOLE 560A AT STA XW 485, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 29, 2000 · N500MH · Doug DC871F · Wing, Longeron/StringerSDR RRXA003199Clip · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED CLIP ON THE RT CENTER WING THRU ACCESS 516 AND I/B AT STA XCW -23 BETWEEN STRINGERS 53 & 54, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 29, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003210Skin · dentedDURING A MAINTENANCE VISIT FOUND A DENT AT STA 447 BETWEEN L36L TO L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 28, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003209Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE ATTACH ANGLE REAR SPAR UPPER CENTER WING IN CABIN Z-21 AT STA 857 +25 TO -45 LWR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 28, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003198Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE LT CENTER WING THRU ACCESS HOLE 516 AND THRU MID SPAR ACCESS HOLE 560E O/B BETWEEN STA''S XCW 69.5 TO XCW 46 STR 76, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 28, 2000 · N500MH · Doug DC871F · Wing, Longeron/StringerSDR RRXA003835Former · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO TOP T/E I/B FORMER AT STA. XFS 523, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-Sep 27, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003826Former · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BOTTOM T/E FORMER AT STA. XFS188.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4, 51Sep 27, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003757Clip · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L/H LOWER CLIP ON THE L/H CENTER WING THRU ACCESS HOLE 516 THRU MID SPAR ACCESS HOLE 560E BETWEEN STA XCW 46 BETWEEN STR 73 & 74, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM . /////CORRECTIVE ACTION///// Sep 27, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003756Clip · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LWR CLIP L/H CENTER WING THRU ACCESS HOLE 516 THRU MID SPAR ACCESS HOLE 560E AT STA XCW +46 BETWEEN STR 72-73, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREASep 27, 2000 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003755Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON NR 76 LT CENTER WING THRU ACCESS HOLE 516 & THRU MID SPAR ACCESS HOLE 560E O/B BETWEEN XCW 69.5 TO XCW 46, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8Sep 27, 2000 · N500MH · Doug DC871F · Wing, Longeron/StringerSDR RRXA003750Stringer · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE #76 STRINGER L/H CENTER WING THROUGH ACCESS HOLE 516 AND THROUGH MID SPAR ACCESS HOLE 560E O/B BETWEEN STA XCW 69.5 TO XCW 46, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVSep 27, 2000 · N500MH · Doug DC871F · Wing, Longeron/StringerSDR RRXA001058Floor Panel · crackedMAIN CARGO DECK FLOOR CRACKED AT POSITION NR 7. CUT, FITTED AND INSTALLED NEW FLOOR PANE IAW DC-8 M/M CHAPTER 51-1-21.Sep 27, 2000 · N8091U · Doug DC871F · Fuselage Floor PanelSDR RRXA003204Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM T/E FORMER AT STA XFS 145, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 27, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003203Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM T/E FORMER AT STA XFS 151.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 27, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003843Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO DE-ICER VENT HOLES AT STA. XFS204-310, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4,Sep 26, 2000 · N500MH · Doug DC871F · Wing Miscellaneous StructureSDR RRXA003840Frame · tool damageDURING A MAINTENANCE VISIT FOUND DRILL DAMAGE TO LONGERON 20 AT STA. 1580, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW EO 00-257 WITH APPROVED 8110-3 DATED 10/09/00.Sep 26, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003834Former · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BOTTOM T/E FORMER AT STA. XFS250-310, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4, 51Sep 26, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003833Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO DE-ICER VENT HOLES AT STA. XFS404-410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4,Sep 26, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003832Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK IN DE-ICER VENT HOLES AT STA. XFS297-304, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4, 57-2-1Sep 26, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003831Former · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LOWER FORMER AT STA. XFS466, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, 51-1-4.Sep 26, 2000 · N500MH · Doug DC871F · Wing Main, Frame StructureSDR RRXA003830Frame · damagedDURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO LOWER FRAME AT STA. XFS416, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-4.Sep 26, 2000 · N500MH · Doug DC871F · Wing SparSDR RRXA003829Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LWR. SKIN OF DE-ICER VENT AT STA. XFS379-385, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51Sep 26, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003828Skin · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED DAMAGE TO SCREW HOLE CORNER OF I/B END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-26, 51-1-4.Sep 26, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003827Skin · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED DAMAGE TO SCREW HOLE LOWER I/B L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-26, 51-1-21, 51-1-4.Sep 26, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003208Fitting · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE AT AFT END OF THE I/B SIDE CANOE FITTING AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 26, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003207Access Panel · misdrilledDURING A MAINTENANCE VISIT FOUND A DOUBLE DRILLED HOLE TO THE FUEL TANK PANEL LAND RT WING PANEL 514F, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 26, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003206Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE UPPER SURFACE LONGERON ON THE LEFT W/W LONGERON 24 AT STA 879-890, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 25, 2000 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003205Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AT THE AFT LWR CARGO BILGE AT STA 1340 TO 1360 AND L36L TO L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Sep 25, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003138Splice · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ALONG RADIUS OF THE STRESS PANEL ATTACH POINT END SPLICE AT STA Y=780 AND X=-12, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-Sep 24, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003742Attach Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ATTACH FITTING ABOVE LONGERON 24R AT STA 902, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PARTS AND INSTALLED IAW DC-8 SRM 51-1-20D ASep 22, 2000 · N500MH · Doug DC871F · Fuselage Main, Attach FittingsSDR RRXA003050Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H W/W LONGERON VERTICAL FITTING AT STA 940 AND L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PARTSep 22, 2000 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003049Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H W/W LONGERON VERTICAL FITTING AT STA 920 AND L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALSep 22, 2000 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003048Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H W/W LONGERON VERTICAL FITTING AT STA 879 AND L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLSep 22, 2000 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003047Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H W/W LONGERON LWR FITTING AT STA 960 AND L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLEDSep 22, 2000 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003046Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE "C-PIT" FRAME TO LONGERON FITTING UPPER SIDE AT STA 1168 AND L30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 Sep 22, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833787Light · inoperativeINSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER MM 33-50-00, CKS NORMAL.Sep 22, 2000 · N748UP · Doug DC871F · Emergency LightingSDR RRXA003758Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE VERTICAL FITTING R/H W/W LONGERON 24R AT STA 940, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND Sep 21, 2000 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003739Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE ATTACH FITTING AT STA 902 AND L24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-20D AND DWG 26Sep 21, 2000 · N500MH · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS00833782Actuator · out of adjINSPECTION TYPE:N/A, PILOT REPORT-A/C REQUIRES EXCESSIVE RUDDER TRIM ON TAKEOFF AND LANDING DURING CALM WIND CONDITIONS. IN CRUISE FLIGHT AIRCRAFT REQUIRES 5 DEGREES RUDDER TRIM. ADJUSTED RUDDER POWER PACK IAW MM 27-21-02, SYS OPS CHECKS GOOD.Sep 21, 2000 · N755UP · Doug DC871F · Rudder ActuatorSDR UPS00833785Light · inoperativeINSPECTION TYPE:N/A, FLIGHT DECK EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC8 MM 33-5-00 1, OPS CHECKS GOOD.Sep 20, 2000 · N752UP · Doug DC871F · Emergency LightingSDR RRXA003312Angle · corrodedDURING A MAINTENANCE VISIT FOUND A DENT TO THE DOOR JAMB FRAME IN C-CARGO COMPT AT STA 1169 AND LBL 14 WATERLINE -58, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-Sep 19, 2000 · N8076U · Doug DC871F · Fuselage Miscellaneous Structure
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