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 RRXA003259Doubler · crackedDURING A MAINTENANCE VISIT FOUND GROUND RIVET HEADS TO THE CUSP PANEL LT SIDE AT STA 1660 TO 1700, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 16, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003258Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACKED ATTACH FITTINGS 2 AT STA 902 AND L18R LONGERON TO FRAME ATTACH FITTINGS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 16, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00834416Support Bracket · crackedINSPECTION TYPE:C2, LT LWR FUSELAGE STA 702 FILLET FAIRING ATTCH ANGLE IS CRACKED IN RADIUS. REPAIRED FILLET FAIRING ATTACH ANGLE IAW DC8 SRM 53-2-0 AND LONGERON 33 LT IAW TIMCO REO G07690 REV A.Oct 15, 2000 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00834303Angle · crackedINSPECTION TYPE:C2, AFT PIT ''D'' DOOR JAMB ''L'' ANGLE CRACKED. FABED NEW DOOR JAMB ''L'' ANGLE IAW DAC DWG 3712791. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.Oct 14, 2000 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003263Spar · 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. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DOct 13, 2000 · N500MH · Doug DC871F · Wing SparSDR UPS00834304Angle · crackedINSPECTION TYPE:C2, AFT PIT ''D'' DOOR THRESHOLD SUPPORT CRACKED. REMOVED CRACKED SUPPORT ANGLE, FABED NEW SUPPORT ANGLE IAW DAC DWG 5703872. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-21.Oct 13, 2000 · N744UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00834301Bulkhead · crackedINSPECTION TYPE:C2, RIGHT APB CRACKED STA 1766 APPROX L11R. FABED, LOCATED AND DRILLED -25 & -27 DOUBLERS -9 -19 & -11 FILLERS AND -29 ATTACH ANGLE IAW DC8 SRM 51-1-24 & REO G07688. ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 51-1-20D, 51-1-21.Oct 13, 2000 · N744UP · Doug DC871F · Fuselage Main, BulkheadSDR RRXA003286Skin · damagedDURING A MAINTENANCE VISIT FOUND L/E SCREWS PULLING INTO SKIN AND STICKING UP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-4.Oct 12, 2000 · N500MH · Doug DC871F · Leading Edge DevicesSDR RRXA003285Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT SLOT DOOR AT THE BOTTOM I/B L/E PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-4.Oct 12, 2000 · N500MH · Doug DC871F · Leading Edge DevicesSDR RRXA003284Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE INSIDE L/E BULKHEAD BETWEEN STA XFS 285.250 AND XFS 291.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51Oct 12, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003283Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 285.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21.Oct 12, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003282Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 291.500, 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 SRM 51-1-21, 51-1-4.Oct 12, 2000 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003281Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 258.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-4.Oct 12, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003280Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN ANGLE ON FR BULKHEAD AT XS 250, 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 SRM 51-1-21.Oct 12, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003279Skin · crackedDURING A MAINTENANCE VISIT FOUND A CRACK IN INNER SKIN JUST O/B OF STA XS 246, 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 SRM 51-1-21, 51-1-4.Oct 12, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00834299Seat Track · brokenINSPECTION TYPE:C2 LOG ITEM TRANSFERRED FROM LOG PAGE 5275611 ITEM 2 SEAT TRACK BROKEN MAIN CARGO DECK POSS 2-3 LEFT O/B CUT OUT DAMAGED IAW DC8 SRM 53-2-3 FIG 6D. ALODINED,PRIMED AND INSTALLED IAW DC8 SRM 51-3-0, 53-2-3 FIG 6D.Oct 12, 2000 · N744UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA001067Fitting · shearedAFTER T/O TOWER INFORMED US THAT LEFT MAIN GEAR DIDN''T RETRACT ON GEAR RETRACTION. AFTER PERFORMING LOW PASS TO CONFIRM GEAR WAS DOWN, RETURNED TO KDAY. DURING INSPECTION FOUND LT MLG ACT EYEBOLT ATTACH LUG SHEARED. PREPARED ACFT FOR FERRY FLIGHT TO KMQY Oct 12, 2000 · N997GE · Doug DC871F · Main Landing Gear Attach SectionSDR RRXA003749Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME AT STA 360 AND L35, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-4, 53-2-0 AND 51-1-21.Oct 11, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003270Seat Track · damagedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND ELONGATED HOLES TO THE FE'S LT SEAT TRACK, 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 SRM 51-3-0, 51-1-24.Oct 11, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003269Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE 1ST PANEL INSIDE L-1 DOOR FLOOR PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-2Oct 11, 2000 · N500MH · Doug DC871F · Fuselage Floor PanelSDR RRXA003268Skin · corrodedDURING A MAINTENANCE VISIT FOUND LIGHT CORROSION TO THE SKIN AND FINGER DOUBLER BETWEEN STA 879 - 902 AND +45 TO +69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DCOct 11, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003267Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A CRACK TO THE PRESS PANEL BETWEEN STA 834 & 857 AND 0 TO +69, 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 Oct 11, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003266Shear Tie · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AT SHEAR FOOT AT PROD BREAK AT STA 1690 AND L19R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51Oct 11, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003265Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE RT CUSP AT STA 40 AND L21R, 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 SRM 51-1-21.Oct 11, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003264Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON FRAME AFT OF ''B'' PIT DOOR AT STA 560 AND Z=0, 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 SRM 51-1-21.Oct 11, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003278Fitting · crackedDURING A MAINTENANCE VISIT FOUND A GOUGE AND POSSIBLE CRACK TO THE O/B AILERON O/B HINGE POINT FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED DAMAGE AREA AND RETURNED TO SERVICE IAW EOOct 10, 2000 · N500MH · Doug DC871F · AileronsSDR RRXA003277Hinge · damagedDURING A MAINTENANCE VISIT FOUND A DAMAGED HINGE TO THE WING HINGE PANEL T/E UNDER AILERON O/B DAMPNERS, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED AREA AND RETURNED TO SERVICE IAW EO#00-257 Oct 10, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003276Fitting · gougedDURING A MAINTENANCE VISIT FOUND A GOUGED PULLEY CLUSTER FITTING ON O/B SIDE I/B AILERON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. DLENDED DAMAGED AREA AND RETURNED TO SERVICE IAW EO#00-257 WITH AOct 10, 2000 · N500MH · Doug DC871F · AileronsSDR RRXA003275Spar · gougedDURING A MAINTENANCE VISIT FOUND 3 GOUGES ON BOTTOM SIDE OF ATTACH ANGLES AT REAR SPAR AT STA 690, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED DAMAGE AREA AND RETURNED TO SERVICE IAW EO 00-257Oct 10, 2000 · N500MH · Doug DC871F · Wing SparSDR RRXA003274Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE PILOTS LT AFT SEAT TRACK, 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 SRM 53-2-3 FIG.11, 51-3-0.Oct 10, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003273Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES AND WORN TRACK TO THE PILOTS RT AFT SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 53-2-3 FIG.11.Oct 10, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003272Seat Track · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED AND WORN HOLES TO THE F/O''S LEFT AFT SEAT TRACK, DAMAGE EXCEEED 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 SRM 51-3-0, 53-2-3 FIG.11Oct 10, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003271Seat Track · damagedDURING A MAINTENANCE VISIT FOUND WORN AND ELONGATED HOLES TO THE F/O'S RIGHT AFT SEAT TRACK, 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 SRM 51-3-0, 53-2-3 FIG.1Oct 10, 2000 · N500MH · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR RRXA003191Longeron · gougedDURING A MAINTENANCE VISIT FOUND A GOUGED MAIN LUG ATTACH HOLE ON FITTING AT STA 857 AND LONGERON 24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 8, 2000 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003217Tab · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RUDDER FLIGHT TAB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 6, 2000 · N500MH · Doug DC871F · Rudder, Tab StructureSDR RRXA003216Stringer · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE TO THE TOP OF STRINGER NR 64 AT PLATE 505B NR 4 ALT INSIDE TANK BETWEEN STA XW 454 AND XFS 456, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 6, 2000 · N500MH · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA003215Bushing · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE TO THE LUG BUSHING AT STA 857 AND L24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 6, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003214Gusset · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE GUSSET ON NR 4 MAIN INSIDE TANK THRU ACCESS HOLE 505C AND THRU MID-SPAR ACCESS HOLE 560C BETWEEN LWR STR 66 AND 67 AT STA XRS 255, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 6, 2000 · N500MH · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA003213Skin · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLES TO THE NR 2 STUB WING L/E BOTTOM AT STA XFS 251, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 6, 2000 · N500MH · Doug DC871F · Wing, Plate/SkinSDR RRXA003192Doubler · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E INNER SKIN DOUBLER AT STA XFS 360 - 250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8S RM.Oct 6, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00833850Longeron · crackedINSPECTION TYPE:C1, STA 1350 LONG 34L IS CRACKED. REMOVED AND REPLACED LONGERON IAW DWG 3758593, AND SRM 51-1-20D, 51-1-21.Oct 6, 2000 · N779UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA001063Drive Shaft · damagedTHE GROUND HANDLERS DAMAGED THE CREW DOOR LOCKING DRIVE WHILE LOWERING THE ACFT STAIRS. *S/D* REMOVED AND REPLACED BAYONET BRACKET PER DC-8 M/M 52-10-0 CODE 1 AND 52-11-1 CODE 1, OPS CHECK GOOD.Oct 4, 2000 · N801GP · Doug DC871F · Entrance StairsSDR RRXA003211Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ON FORMER AT UPPER ANGLE AT STA XS 250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 4, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003196Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ON FORMER AT STA XS 256, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 4, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003195Frame · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER FORMER ANGLE AT STA XS 250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 4, 2000 · N500MH · Doug DC871F · Fuselage Main, FrameSDR RRXA003194Panel · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 4, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA003193Panel · damagedDURING A MAINTENANCE VISIT FOUND ELONGATED HOLES ON THE LWR ACCESS PANEL FORMER AT STA XS 250 - 240, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.Oct 4, 2000 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS00833852Fitting · damagedINSPECTION TYPE:C1, STA 1690 LONG 32L END HAS HOLES WITH NO EDGE DISTANCE. REMOVED AND REPLACED FITTING IAW DWG 4641324, AND SRM 51-1-20D.Oct 4, 2000 · N779UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS00833851Longeron · damagedINSPECTION TYPE:C1, STA 1690 - 1776 LONG 32L HAS HOLES IN RADIUS. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 5649329, AND SRM 51-1-20D.Oct 4, 2000 · N779UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS00833848Intercostal · crackedINSPECTION TYPE:C1, STA 240 - 260 LONG 33L INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5750726, AND SRM 51-1-21.Oct 4, 2000 · N779UP · Doug DC871F · Fuselage Miscellaneous Structure
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