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 UPS03840823Longeron · crackedINSPECTION TYPE: C1, STATION 1781 LONG. 17R AND END FITTING ARE CRACKED, REMOVED LONGERON AND ENDFITTING, FABRICATED LONGERON AND REPLACED END FITTING IAW DWG. 4772397 AND 5649327,AND SRM. 51-1-21,51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA0300041OStator Vane · out of rigEN ROUTE TO KRFD FROM IAH NR 3 ENGINE COMPRESSER STALLED ON DECELERATION OF DESCENT. ON LEVEL OFF, ENGINE STALLED AGAIN WHEN POWER WAS APPLIED. IT WAS DECIDED TO FLY DIRECT TO TOL. POWER NOT ADJUSTED UNTIL NR 3 ENGINE WAS SHUTDOWN ON FINAL APPROACH TO TOL. May 21, 2003 · N825BX · Doug DC871F · Turbine Engine Compressor SectionSDR UPS03840760Attach Fitting · crackedINSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED STA 1152 LONG 20R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840759Fitting · crackedINSPECTION TYPE: C1, STA 1781 LONG 17L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840758Fitting · crackedINSPECTION TYPE: C1, LT STA 980 FITTING IS CRACKED NEXT TO FUSELAGE ON WING BOX. REMOVED AND REPLACED FITTING IAW DWG 4647365 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Wing, Center BoxSDR UPS03840757Fitting · crackedINSPECTION TYPE: C1, STATION 1690 LONG 28L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840756Fitting · corrodedINSPECTION TYPE:C1 A/C BAY STA 70 LONG FRAME FITTING 34L IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4611159 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840709Attach Fitting · crackedINSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STATION 1220 AT LONG 20R. REMOVED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840706Fitting · crackedINSPECTION TYPE:C1 INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1160 LONG 18R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840705Fitting · crackedINSPECTION TYPE: C1, LT SIDE STA 800 ON SUBFLOOR AFT OF FLOORBEAM AT LBL 60 THERE IS A CRACKED SUPPORT FITTING. REMOVED AND REPLACED FITTING IAW DWG 3643112 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840704Fitting · crackedINSPECTION TYPE:C1 INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1200 LONG 20R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840703Fitting · crackedINSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1152 LONG 19R. REMOVED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840702Fitting · crackedINSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT LONG 1180 LONG 18R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840700Attach Fitting · crackedINSPECTION TYPE: C1, INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT STA 1220 LONG 19R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.May 21, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840822Rib · crackedINSPECTION TYPE: C1, LEFT WING LE. UPPER RIB IS CRACKED AT XFS 697.5 STOPDRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED STACK ANGLE REPAIR IAW SRM. 57-2-0 FIG. 2May 20, 2003 · N705UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS03840780Angle · crackedINSPECTION TYPE: C1, 1 INCH CRACK ON ANGLE DOUBLER INNER FRAME OF R-1 DOOR AT STA 160 LONG 15R-17R ON DOOR. REMOVED, FABRICATED AND INSTALLED ANGLE DOUBLER IAW DWG 5615762, AND SRM 51-1-21, 51-1-21A, 51-3-0.May 20, 2003 · N705UP · Doug DC871F · Service DoorsSDR UPS03840779Web · crackedINSPECTION TYPE: C1, 1.25 INCH CRACK UPPER LEFT INNER WEB R-1 DOOR AT STA 156 LONG 12R TO 13R ON DOOR. STOP DRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 52-2-0 FIG 1B.May 20, 2003 · N705UP · Doug DC871F · Service DoorsSDR UPS03840708Longeron · crackedINSPECTION TYPE: C1, AT STATION 1730 CANTED FRAME LONGERON 14L IS CRACKED. REMOVED LONGERON SECTION STATION 1710-1760, FABRICATED AND INSTALLED LONGERON SECTION IAW SRM 53-2-2 FIG 10.May 20, 2003 · N705UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS03840707Fitting · crackedINSPECTION TYPE:C1 MAIN CABIN LONGERON END FITTING IS CRACKED BETWEEN STA 660-680 LONG 11L. REMOVED AND REPLACED FITTING IAW DWG 5750540 AND SRM 51-1-20D.May 20, 2003 · N705UP · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS03840701Longeron · crackedINSPECTION TYPE: C1, STATION 1730 LONG 14R IS CRACKED. REMOVED LONGERON STA 1720 TO 1760, FABRICATED AND INSTALLED LONGERON SECTION IAW DWG 5649327 SRM 53-2-2 FIG 10.May 20, 2003 · N705UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS03840825Skin · crackedINSPECTION TYPE: C1, R-1 LOWER AFT CORNER DOUBLER AND TRIPLER DOES NOT CONFORM TO SRM. 53-2-0 FIG. 14 STA. 418 AT LONG. 21R. REMOVED EXISTING REPAIR,CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER,TRIPLER AND FILLER IAW SRM. 5May 19, 2003 · N705UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS03840755Skin · damagedINSPECTION TYPE: C1, L-1 UPPER AFT CORNER DOUBLER,TRIPLER DOES NOT CONFORM TO SRM 53-2-0 FIG 15, STA 60 AT LONG 10L. REMOVED EXISTING DOUBLER AND TRIPLER, FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 53-2-0 FIG 15.May 19, 2003 · N705UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS03840699Skin · crackedINSPECTION TYPE: C1, REMOVE DOUBLER FROM L-1 DOOR UPPER FWD CORNER, DOUBLER DOES NOT CONFORM TO SRM. REPAIR PER SRM 53-2-0 FIG 15 ST STA 60 LONG 10L. REMOVED EXISTING REPAIR, CUTOUT CRACK DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOMay 17, 2003 · N705UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0300035OWire · chafedON CLIMB OUT FROM TOL TO ATL CREW REPORTED RUDDER MANUAL REVERSION LIGHT CAME ON. THE CREW REPORTED THAT THE RUDDER WAS POWERED BUT THE LIGHT WAS STAYING ON. CREW RETURNED TO TOL. MAINTENANCE VERIFIED HYDRAULIC PRESSURE AND QUANTITY ARE OKAY. MAINTENANCE FOUMay 16, 2003 · N823BX · Doug DC871F · Flight Control System WiringSDR UPS03840631Window · out of adjustINSPECTION TYPE: PFLT, COPILOTS SIDE WINDOW WILL NOT OPEN DISCOVERED ON POST FLIGHT ADJUSTED WINDOW GUIDE AT TOP FORWARD CORNER OF F/O SLIDING WINDOW.Apr 30, 2003 · N718UP · Doug DC871F · Flight Compartment WindowsSDR UPS03840431Smoke Barrier · tornINSPECTION TYPE: PFLT, MAIN CARGO DECK SMOKE CURTAIN HAS A 8 INCH TEAR & HAS COME UNSCURED BOTH IN THE LOWER LT OUTBOARD SIDE. PERFORMED INTERIM REPAIR EO DC8 -2550-1872B TRASFERD TO D-258389 FINAL SMOKE CURTAIN REPAIR ACCOMPLISHED PER UPS E.O. #DC8-2550Apr 18, 2003 · N729UP · Doug DC871F · Portable Oxygen SystemSDR UPS03840430Frame · crackedINSPECTION TYPE: PFLT, 2 INCH GOUGE IN NR 4 PIT SLOPING WALL 3 FT ALT OF BULKHEAD AFTER PULLING BACK THE LINER, FOUND FRAME CRACKED. REMOVED FLOOR PANEL IN NR 4 PIT RIGHT SIDE FWD TO INSPECT FLOOR SUPPORT FRAME FOR DAMAGE . KMA 56755 / ACCOMPLSIHED PERMANApr 18, 2003 · N729UP · Doug DC871F · Fuselage Main, FrameSDR UPS03840429Slide · deterioratedINSPECTION TYPE: PFLT, CREW ENTRY DOOR ESCAPE SLIDE COMING APART. RE-ATTACHED CREW ENTRY ESCAPE SLIDE COVER & SECURED TO DOOR.Apr 17, 2003 · N700UP · Doug DC871F · Escape SlideSDR UPS03840445Battery Pack · will not testINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DO NOT TEST. REMOVED AND REPLACED SHIPS EMERGENCY LIGHT BATTERY PACK PER 33-50-01, OPS CHECK NORMAL.Apr 16, 2003 · N700UP · Doug DC871F · Emergency LightingSDR UPS03840428Battery Pack · inoperativeINSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED SHIPS EMERGENCY LIGHT BATTERY PACK PER 33-50-01, OPS CKS NORMAL.Apr 15, 2003 · N700UP · Doug DC871F · Emergency LightingSDR UPS03840423Compressor · stalledNR 3 ENGINE COMPRESSOR STALL IFSD AT FL350 WHEN POWER WAS REDUCED FROM 85 TO 77 N & CONTINUED TO STALL IN DESCENT WHEN POWER WAS REDUCED BELOW 72N NR 3 ENG SHUTDOWN IN FLIGHT DUE TO CONTINUED COMPRESSOR STALLS IN LEVEL FLIGHT WITHOUT MOVING THROTTLE. REMOVED Apr 9, 2003 · N705UP · Doug DC871F · Turbine Engine Compressor SectionSDR UPS03840387Skin · crackedLOWER WING SKIN CRACK OUTBOARD NR 1 ENGINE PYLON STA XW 508. FERRIED TO SAA FOR REPAIR. *S/D* CUT OUT CRACKED AREA ON SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED WING SKIN FILLER, REPAIR FILLER AND DOUBLER IAW 8110-3 APPROVED SAA SK 77Mar 28, 2003 · N772UP · Doug DC871F · Wing, Plate/SkinSDR UPS03840377Switch · inoperativeEMERGENCY EXIT LIGHT SWITCH ANNUNCIATOR LIGHT INOP. RELAMPED EMERGENCY EXIT ANNUNCIATOR, OPS CHECK OK.Mar 27, 2003 · N701UP · Doug DC871F · Emergency LightingSDR UPS03840376Smoke Detector · inoperativeNR 3 SMOKE DETECTOR DOES NOT TEST. RELAMPED, OPS CHECK GOOD.Mar 27, 2003 · N706UP · Doug DC871F · Smoke DetectionSDR UPS03840346Battery Pack · inoperativeEMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33-50-01.Mar 24, 2003 · N701UP · Doug DC871F · Emergency LightingSDR UPS03840340Battery · inoperativeEMERGENCY EXIT LIGHTS INOP. REMOVED NAD REPLACED BATTERY AND RELAY UNIT AND OPS CHECKED GOOD PER MM 33-50-01.Mar 22, 2003 · N729UP · Doug DC871F · Emergency LightingSDR IXXA0300027OFitting · damagedON APPROACH TO BFI CREW RECEIVED A FLAP SPLIT INDICATION ALONG WITH A AIRCRAFT ROLL TO THE LT. CREW RAISED FLAPS AND DIVERTED TO PDX. MAINTENANCE INSPECTION AND REPAIR IS IN PROGRESS. ADDITIONAL INFORMATION WILL BE PROVIDED AS IT BECOMES AVAILABLE. MAINTENMar 19, 2003 · N830BX · Doug DC871F · Trailing Edge Flap ActuatorSDR UPS03840275Switch · inoperativeDOORS NOT LATCHED LIGHT ILLUMINATED REMAINED ON AFTER GEAR RETRACTION (LEFT GEAR DOOR). RECYCLED GEAR, BROUGHT FLAPS TO 10 DEG, LIGHT EXTINGUISHED. BROUGHT FLAPS UP, RESUMED NORMAL FLIGHT. CHECKS OK ON GROUND. REMOVED AND REPLACED LEFT ALT GEAR DOOR SWITCHMar 11, 2003 · N748UP · Doug DC871F · Door Warning SystemSDR IXXA0300024OCompressor · stalledAFTER DEPARTURE FROM GSO DURING CLIMB OUT TO TOL. WHEN POWER REDUCED FROM CLIMB TO CRUISE, CREW NOTED NR 1 ENGINE COMPRESSOR STALL. PRECAUTIONARY ACTION WAS TAKEN AND ENGINE SHUTDOWN FOR REMAINDER OF FLIGHT. CREW MADE AN UNEVENTFUL LANDING IN TOL.Mar 9, 2003 · N820BX · Doug DC871F · Turbine Engine Compressor SectionSDR UPS03840260Window · leakingINSPECTION TYPE:N/A, F/O CLEAR VIEW WINDOW STILL SQUEALING AT CRUISE AIR SPEEDS AND THE WINDOW IS VERY DIFFICULT TO OPEN. PRESSURIZED A/C TO 8 PSI DIFF, NO SQUEAL NOTED. SEALED EYEBROW WINDOW WITH AERODYNAMIC SEALENT. LUBED F/O CLEARVIEW WINDOW & WINDOW OPEMar 6, 2003 · N755UP · Doug DC871F · Flight Compartment WindowsSDR IXXA0300022OControl Cable · out of rigAFTER DEPARTURE FROM GSO WHILE PERFORMING POST HEAVY MAINTENANCE CHECK FLIGHT. COMPRESSOR STALL ON NR 1 ENGINE WAS NOTED WHILE REDUCING POWER SETTING FROM CLIMB TO CRUISE. AS PRECAUTIONARY ACTION NR 1 ENGINE WAS SHUTDOWN. AS MORE INFORMATION BECOMES AVAILAMar 5, 2003 · N820BX · Doug DC871F · Power LeverSDR UPS03840194Bell Assy · weakINSPECTION TYPE: PFLT, WHEN TESTING FIRE WARNING SYSTEM ON ALL 4 ENG FIRE WARNING BELL IS WEAK, BARELY AUDIBLE. REMOVED AND REPLACED BELL ASSY ENG FIRE WARNING SYSTEM, OPS CHECK PER MMNL 26-10-03. SYSTEM NORMAL.Feb 18, 2003 · N715UP · Doug DC871F · Fire DetectionSDR UPS03840165Landing Gear · collapsedNOSE LANDING GEAR COLLAPSED AFTER ENGINE SHUT DOWN, APPROX. 4 FT FRO M BLOCK. AIRCRAFT SOLD IN "AS IS" CONDITIONFeb 11, 2003 · N797UP · Doug DC871F · Nose/Tail Landing GearSDR IXXA0300014OComputer · failedAFTER DEPARTURE FROM MCO DURING CLIMBOUT DESTINED FOR TOL AIRCRAFT EXPERIENCED YAW ABNOMALY. CREW ELECTED TO RETURN TO MCO. AFTER UNEVENTFUL LANDING IN MCO MAINTINANCE INSPECTED SYSTEM AND TRANSFERRED THE YAW DAMPNER TO MEL. ALL WORK COMPLETED PER APPLICABLFeb 11, 2003 · N827BX · Doug DC871F · Autopilot SystemSDR UPS03840166Window · stuckINSPECTION TYPE:PFLT CAPT'S SLIDE WINDOW WILL NOT OPEN. CYCLE LOCK AND OPS, CHECK NORMAL.Feb 10, 2003 · N702UP · Doug DC871F · Flight Compartment WindowsSDR IXXA060475SPlate · damagedDURING ROUTINE C CHECK FOUND LEFT WING NUMBER FOUR FLAP VANE HAVE AN ELONGATED HOLE. REMOVED DAMAGED PLATE, FABRICATED NEW PLATE, LOCATED DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW PLATE IAW DOUGLAS DRAWING 5655752, DC8 SRM 51-1-8, 51-1-20D, AND 51-Feb 9, 2003 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060474SPanel · crackedDURING ROUTINE C CHECK, FOUND LEFT FLAP ICE BREAKER PANEL CRACKED AT STATION XF219. REPAIRED PER TIMCO EO REO609034 AND DC8 SRM 51-3-0.Feb 9, 2003 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060476SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE RIB AT STATION 341 CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED DOUBLER IAW DC8 SRM 57-2-0, 51-1-8, AND 51-1-20D.Feb 8, 2003 · N820BX · Doug DC871F · Wing, Rib/BulkheadSDR IXXA060477SFrame · damagedDURING ROUTINE C CHECK, FOUND FRAME DAMAGED AT STATION 1903 LEFT SIDE ABOVE HINGE CUT OUT. REMOVED DAMAGE, FABRICATED REPAIR ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR IAW DC8 SRM 51-1-8, 53-2-0, AND 51-1-21.Feb 4, 2003 · N820BX · Doug DC871F · Fuselage Main, FrameSDR UPS03840138Panel · crackedNR 4 PYLON SIDE HAS 3.5 INCH CRACK IN ACCESS PANEL 499E {FIBERGLASS PANEL} 8 INCHES AFT OF L/E OF PANEL VERTICAL CRACK FROM BOTTOM EDGE OF PANEL. PANEL REPAIRED PER REF SRM 51-1-19.Feb 2, 2003 · N744UP · Doug DC871F · Nacelle/Pylon, Plate/Skin
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