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 UPS97822202Angle · crackedINSPECTION TYPE:D, LT FWD UPPER WING FILLET PANEL ATTACH ANGLE IS CRACKED IN TWO, BS 640. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21.Jan 12, 1997 · N748UP · Doug DC871F · Aerodynamic FairingsSDR UPS97822199Rib · crackedINSPECTION TYPE:D LT WING I/B L/E RIB CRACKED AT STA XFS 201.25 UPPER AFT END. STOP DRILLED CRACK AND REPAIRED IAW 57-2-0 FIG 2 .Jan 12, 1997 · N748UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97821926Doubler · corrodedINSPECTION TYPE-C, NR 1 PIT STA 350 TO 370 BTWN STR 35L TO 35R ANTENNA DOUBLER HAS HEAVY CORROSION. REMOVED AND REPLACED DOUBLER IAW DOUGLAS DWG 5754129 AND SRM 51-1-20 D AND 51-1-20.Jan 12, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821897Clip · crackedINSPECTION TYPE: C. FRAME CLIP CRACKED AT STA 1338.23, LT UPPER CUSP, AFT SIDE OF FRAME. STOP DRILLED CRACK PER SRM 53-2-0. FABRICATED FRAME CLIP ANGLE REPAIR AND INSTALLED FASTENERS PER SRM 53-2-0 AND SRM 53-20-10.Jan 12, 1997 · N706UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA9700015Fitting · crackedDURING ROUTINE CHECK INSPECTION, THE LEFT WING RIB ATTACH FITTING AT STATION XW 485 BETWEEN STRINGERS 63 AND 64 WAS FOUND TO BE CRACKED. REPAIR WAS ACCOMPLISHED BY REMOVAL OF EXISTING RIB FITTING, FABRICATION AND INSTALLATION OF NEW RIB FITTING IN ACCORDANCEJan 12, 1997 · N825BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA9700011Doubler · corrodedDURING ROUTINE C-CHECK AND CPCP INSPECTION, A FUSELAGE LOWER SKIN REPAIR DOUBLER WAS FOUND CORRODED AT FUSELAGE STATION 336.5 TO 379.0, BETWEEN LONGERON 32R AND 32L. REPAIR ACCOMPLISHED BY REMOVAL OF CORRODED DOUBLER, FABRICATION AND INSTALLATION OF A REPAJan 12, 1997 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA97011Doubler · crackedDURING MAINTENANCE VISIT, FOUND LT WING LEADING EDGE INTERNAL DOUBLER (P/N 5641252-1) WITH 2 EACH CRACKS, AT XW= 297. REPAIRED BY FABRICATING AND INSTALLING EXTERNAL REPAIR DOUBLER IAW APPROVED FAA-DER REO-02560.Jan 11, 1997 · N8091U · Doug DC871F · Wing Miscellaneous StructureSDR IXXA9700020Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, A FUSELAGE SKIN BULGE WAS FOUND ACCOMPANIED BY MISSING RIVET HEADS AT FUSELAGE STATION 445.0, BETWEEN LONGERONS 30LT AND 32LT. REPAIR WAS ACCOMPLISHED BY REMOVING CORRODED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FIJan 11, 1997 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS97822239Doubler · crackedINSPECTION TYPE:D, LT WING CENTER L/E UPPER DOUBLER AT STA XFS423.0 IS CRACKED. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 57-3-1, 51-1-21.Jan 10, 1997 · N748UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS97822230Rib · crackedINSPECTION TYPE:D, LT WING LE RIB AT STA XOLDI 6.225 IS CRACKED. FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-0.Jan 10, 1997 · N748UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97821863Rib · crackedINSPECTION TYPE: C. UPPER LE RIB CRACKED 2.0 INCHES ON RT WING AT STA. XFS 442.2. STOP DRILLED CRACK PER SRM 57-2-0. FABRICATED AND INSTALLED REPAIR ANGLE PER SRM 57-2-0 AND 51-1-21.Jan 10, 1997 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR RRXA97010Jamb Frame · corrodedDURING MAINTENANCE VISIT, FOUND DOOR JAMB (P/N 9779454) CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=333 AND BETWEEN LONGERONS L35L TO L35R. FABRICATED AND INSTALLED FILLER FROM 7075, 2 EACH REINFORCEMENT ANGLES FROM .080 7075T-0 HEAT-TREATED TO T-6. ALL WORJan 10, 1997 · N8091U · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA97007Skin · crackedPERFORMED INSPECTION IAW SB 57-88 REV 3, FOUND NO DISCREPANCEY TO WING SPARS OR SPAR CAPS. DID FIND LEFT WING LOWER SKIN CRACKED AT Y= 341 AND XCW = 69.5. REPAIRED LOWER WING SKIN BY TEMPORARY MAYOR REPAIR IAW DOUGLAS DRAWING SR0857000 AND 93-01-01-001/DRR01Jan 10, 1997 · N8079U · Doug DC871F · Wing, Plate/SkinSDR IXXA9700026Fitting · corrodedDURING ROUTINE C-CHECK AND CPCP INSPECTION, CORROSION WAS FOUND ON AN ATTACH FITTING AT LONGERON 23 LEFT BETWEEN FUSELAGE STATION 1690 AND 1700. REPAIR ACCOMPLISHED BY REMOVAL OF EXISTING FITTING, FABRICATION AND INSTALLATION OF A NEW LONGERON FITTING IN ACJan 10, 1997 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA9700025Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK ON THE RIGHT WING LEADING EDGE LOWER SURFACE PLATING AT WING STATION XFS 422.750 WAS FOUND. REPAIR WAS ACCOMPLISHED BY STOP DRILLING THE CRACK, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCEJan 10, 1997 · N825BX · Doug DC871F · Wing, Plate/SkinSDR IXXA9700022Door · corrodedDURING ROUTINE C-CHECK AND CPCP INSPECTION, CORROSION ON CENTER WING FUEL TANK ACCESS DOOR AT FUSELAGE STATION 742 WAS FOUND. REPAIR WAS ACCOMPLISHED BY REMOVAL OF EXISTING DOOR, FABRICATION AND INSTALLATION OF NEW DOOR IN ACCORDANCE WITH ENGINEERING ORDER 5Jan 10, 1997 · N825BX · Doug DC871F · Wing, Plate/SkinSDR IXXA9700019Bracket · crackedDURING ROUTINE C-CHECK INSPECTION, THE SPOILER CONTROL CABLE SUPPORT BRACKET WAS CRACKED AT FUSELAGE STATION 857.125 IN THE RIGHT MAIN GEAR WHEELWELL. REPAIR ACCOMPLISHED REMOVAL OF EXISTING BRACKET, FABRICATION AND INSTALLATION OF THE SUPPORT BRACKET IN ACCOJan 10, 1997 · N825BX · Doug DC871F · Drag Control SystemSDR IXXA9700018Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK ON THE RIGHT WING LEADING EDGE LOWER SURFACE AT STATION XS366.500 WAS FOUND. REPAIR ACCOMPLISHED BY STOP DRILLING THE CRACK AND FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH ENGINEERIJan 10, 1997 · N825BX · Doug DC871F · Wing, Plate/SkinSDR UPS97821895Rib · crackedINSPECTION TYPE: C. LT WING L/E RIB AT STA XOLDI 6.225 IS CRACKED IN TWO PLACES ABOVE THE PNEUMATIC DUCT. REPAIRED IAW SRM 57-2-0.Jan 9, 1997 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97821866Skin · crackedINSPECTION TYPE: C. LT WING O/B L/E SKIN AT XFS 711 IS CRACKED AT A SCREW HOLE. CRACK IS APPROX .36 INCH LONG JUST BELOW L/E HFEC INSP. VERIFIED CRACK TERMINATES AT SCREW HOLE. FABRICATED AND INSTALLED REPAIR IAW UPS E.O. DC8-5720-7767-A.Jan 9, 1997 · N706UP · Doug DC871F · Wing, Plate/SkinSDR UPS97821861Rib · crackedINSPECTION TYPE: C. LT WING L/E RIB AT STA XFS 448.581 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER, PER SRM 57-3-11 AND 51-1-21.Jan 9, 1997 · N706UP · Doug DC871F · Wing, Rib/BulkheadSDR RRXA97016Skin · dentedDURING A-MAINTENANCE VISIT, FOUND DENT ON LT WING O/B NOSE SKIN AILERON (P/N 5763133-75), LWR SURFACE, AT XA=725. DAMAGE ROUTED OUT, FABRICATED FILLER AND REINFORCING DOUBLER, INSTALLED ON AILERON NOSE SKIN IAW APPROVED FAA-DER REO-02590.Jan 9, 1997 · N8091U · Doug DC871F · Wing, Plate/SkinSDR RRXA97014Skin · wornDURING A-MAINTENANCE VISIT, FOUND RT WING O/B FLAP LEADING EDGE ASSEMBLY (P/N 5655752-345) WAS CHAFED AND WORN UNDER RIB STRIP, AT XF=244.263. DAMAGE ROUTED OUT IN 2 EACH PLACES, FABRICATED AND INSTALLED FILLERS AND REINFORCING INTERNAL DOUBLER ADDED ON LEADIJan 9, 1997 · N8091U · Doug DC871F · Leading Edge DevicesSDR RRXA97013Skin · dentedDURING MAINTENANCE VISIT, FOUND DENT PAST LIMITATIONS IAW DC-8 SRM ON RT WING I/B FLAP, AT UPPER SURFACE XW=107. FABRICATED AND INSTALLED DOUBLER REPAIR IAW APPRROVED FAA-DER REO-02591.Jan 9, 1997 · N8091U · Doug DC871F · Trailing Edge FlapsSDR RRXA97015Skin · dentedDURING A-MAINTENANCE VISIT, FOUND LT WING LWR SKIN CREASED AND DENTED PAST LIMITATIONS IAW DC-8 SRM, AT XRS=750 BETWEEN STRINGER 53 AND REAR SPAR. FABRICATED AND INSTALLED DOUBLER REPAIR FROM 7075T-6 IAW APPROVED FAA-DER REO-02582.Jan 8, 1997 · N8091U · Doug DC871F · Wing, Plate/SkinSDR IXXA9700021Leading Edge · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON THE LEFT WING LEADING EDGE LOWER SURFACE AT STATION XRS 422.750. REPAIR WAS ACCOMPLISHED BY STOP DRILLING THE CRACK, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH ENGINEJan 8, 1997 · N825BX · Doug DC871F · Wing, Plate/SkinSDR IXXA9700017Frame · corrodedDURING ROUTINE C-CHECK AND CPCP INSPECTION. CORROSION WAS FOUND ON FUSELAGE FRAME UPPER CAP AT FUSELAGE STATION 1080 BETWEEN LONGERONS 30 LEFT AND 36. REPAIR ACCOMPLISHED BY REMOVING THE CORRODED AREA, FABRICATION AND INSTALLION OF A REPAIR FILLER AND REPAIRJan 8, 1997 · N825BX · Doug DC871F · Fuselage Main, FrameSDR IXXA9700016Frame · gougedDURING ROUTINE C-CHECK AND CPCP INSPECTION, FUSELAGE FRAME AT STATION 334 BETWEEN LONGERONS 35 LEFT AND 36 LEFT WAS FOUND TO BE DAMAGED. REPAIR WAS ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND TWO REPAIR ANGLES Jan 8, 1997 · N825BX · Doug DC871F · Fuselage Main, FrameSDR IXXA9700012Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE FUSELAGE SKIN AT STATION 10.000, BETWEEN LONGERONS 28R AND 29R. REPAIR WAS ACCOMPLISHED BY REMOVAL OF THE DAMAGED AREA, FABRICATION, AND INSTALLATION OF REPAIR FILLERS, AND A REPAIR DOUBLER IN ACCOJan 8, 1997 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS97821946Stringer · crackedINSPECTION TYPE-C, RT WING NR 4 ALT TANK AT STA XRS 508.00, WING STRINGER 54 IS CRACKED IN HALF. REMOVED DAMAGED SECTION OF STR 54 AND REPAIRED IAW DHC SK-706-686 REF ENGINEERING FILE NR DC8-57-0748.Jan 7, 1997 · N706UP · Doug DC871F · Wing, Longeron/StringerSDR UPS97821806Air Distr · odorINSPECTION TYPE-N/A, NOTICED STRONG FUEL SMELL IN COCKPIT DURING DESCENT. INSPECTED WINGS AND PYLONS FOR FUEL LEAKS, NONE NOTED. RAN ALL ENGINES AND BOTH PACKS, NO FUEL ODOR NOTED IN COCKPIT OR CARGO BAY AREA.Jan 7, 1997 · N797UP · Doug DC871F · Air Distribution SystemSDR UPS97821846Frame · crackedINSPECTION TYPE-C/CK, FRAME CRACKED RW CTR LE AT APPROX STA 433 TOP SIDE. FABRICATED REPAIR IAW DC8 SRM 57-2-0, ALODINED AND PRIMED IAW DC8 SRM D 51-1-8. INSTALLED REPAIR IAW DC8 SRM D 51-1-20D AND DC8 SRM 51-1-21.Jan 6, 1997 · N715UP · Doug DC871F · Fuselage Main, FrameSDR UPS97821844Brace · crackedINSPECTION TYPE-C/CK, FRAME BRACE CRACKED AT STA 660 LT FWD OF WING SUPPORT. REMOVED CRACKED FRAME BRACE ANGLE, FABRICATED NEW ANGLE IAW DC8 SRM 53-8-1 FIG 1 SHEET 2, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED ANGLE IAW DC8 SRM 51-30SD AND 51-1-20D.Jan 5, 1997 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821845Slot Brace · crackedINSPECTION TYPE-C/CK, LT CENTER LE SLOT BRACE CRACKED AT FWD END O/B OF PANEL 522A TOP SIDE OF LE. REMOVED CRACKED BRACE IAW DC8 SRM 51-1-24 AND DC8 SRM 51-1-20D MATERIAL ID IAW DC8 SRM 57-30D, FABRICATED DOUBLER IAW DC8 SRM 57-2-0 AND DC8 SRM 51-1-24, ALODIJan 4, 1997 · N715UP · Doug DC871F · Leading Edge DevicesSDR IXXA9700024Fitting · crackedDURING ROUTINE C-CHECK AND CPCP INSPECTION, A FLOOR BEAM ATTACH FITTING WAS FOUND CRACKED IN THE MAIN CARGO COMPARTMENT AT FUSELAGE STATION 980. REPAIR WAS ACCOMPLISHED BY REMOVING THE CRACKED FITTING, FABRICATION AND INSTALLATION OF A NEW FITTING IN ACCORDAJan 2, 1997 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS97821843Hinge · crackedINSPECTION TYPE-C/CK, LOWER REAR SPAR O/B AILERON O/B HINGE CRACKED. REMOVED LT O/B AILERON, REMOVED AND REPLACED SUPPORT ASSY IAW DC8 SRM 51-3-1 AND REINSTALLED LT O/B AILERON IAW DC8 MM 27-11-02.Dec 31, 1996 · N715UP · Doug DC871F · AileronsSDR UPS97821832Doubler · crackedINSPECTION TYPE-C, LT O/B AILERON AT CENTER HINGE CUTOUT, SKIN DOUBLER IS CRACKED 2 PLACES. REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED DOUBLER PER SRM 57-8-01 FIG 4 AND 51-1-20.Dec 30, 1996 · N772UP · Doug DC871F · AileronsSDR UPS97821827Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 360.25 IS CRACKED AT THE AFT UPPER EDGE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.Dec 30, 1996 · N772UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97821826Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 366.5 IS CRACKED AT THE AFT UPPER EDGE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.Dec 30, 1996 · N772UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97821825Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 329 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACKED AND REPAIRED PER SRM 57-2-0 FIG 2.Dec 30, 1996 · N772UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97821824Rib · crackedINSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 316.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2.Dec 30, 1996 · N772UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS97821823Casting · crackedINSPECTION TYPE: C. RT WING T/E, OUTBOARD OF MLG TRUNNION AND FWD OF AUXILIARY SPAR, THE STA 98 FLAP HINGE LWR ATTACH CASTING CRACKED. REMOVED CRACKED CASTING, FABRICATED REPLACMENT CASTING INSTALLED CASTING PER SRM 51-1-20D, AND SRM 51-3-1.Dec 30, 1996 · N772UP · Doug DC871F · Wing, Control Surface Attach FittingsSDR UPS97821822Rib · crackedINSPECTION TYPE: C. RT WING L/E RIB AT STA. XOLDI 6.225 CRACKED APPROX. 2.8 INCHES. REMOVED DAMAGED AREA PER SRM 57-2-0. FABRICATED FILLER, DOUBLER, AND INTERCOSTAL PER SRM 57-2-0 AND INSTALLED PER SRM 51-1-20D.Dec 30, 1996 · N772UP · Doug DC871F · Wing, Rib/BulkheadSDR IXXA9700023Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON A LONGERON SPLICE FITTING BETWEEN FUSELAGE STATION 220 AND 240 AT LONGERON 29 RT. REPAIR ACCOMPLISHED BY REMOVAL OF SPLICE FITTING, FABRICATION AND INSTALLATION OF A NEW FITTING IN ACCORDANCE WITH ENGINEDec 30, 1996 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96821794Actuator · failedINSPECTION TYPE-N/A, AFTER LANDING ROLLOUT WHEN RETRACTING FLAPS, RES LOW LIGHT CAME ON FLAPS WOULD NOT RETRACT, HYD QTY FALLING RAPIDLY, SYS PRS WENT TO 0 PSI. FOUND RT W/FLAP ACT CYL BROKE AT COMPENSATING LINK, AND UP-HYD PRS LINE CRACKED AT FITTING. REPLADec 29, 1996 · N703UP · Doug DC871F · Trailing Edge Flap Control SystemSDR RRXA96178Skin · crackedDURING INSPECTION, FOUND 5 INCH CRACK IN LOWER FUSELAGE SKIN AT STA 1240. REPAIRED DAMAGED SKIN TO STA 1240 BY TEMPORARY REPAIR IAW ENGINEER DRAWING B87-R01.Dec 27, 1996 · N500MH · Doug DC871F · Fuselage Main, Plate/SkinSDR SRAA961214Fire Loop · out of positionDURING DESCENT, FIRE BELL RANG ONCE AND NR 1 SHORT CIRCUIT TEST LIGHT FLICKERED ON BRIEFLY THEN STOPPED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED NR 1 ENGINE, FOUND FIRE LOOP OUT OF POSITION, REPOSITIONED FIRE LOOP, PERFORMED FUNCTIONAL CHECK AND ENGINE RDec 25, 1996 · N872SJ · Doug DC871F · Fire DetectionSDR UPS96821784Coalescer Bag · contaminatedINSPECTION TYPE-N/A, STRONG DIESEL FUEL SMELL COMING FROM RIGHT PACK. CREW FELT NAUSEA AND HEADACHES, ONE HAD TO USE OXYGEN. REPLACED RT A/C WATER COALESCER BAG. BOTH PACKS OP/C FOR SMELL, NO SMELL NOTED OP/CK GOOD.Dec 17, 1996 · N706UP · Doug DC871F · Humidity Control SystemSDR UPS96821783Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CK OK (P/N 60-1223-5) (S/N 322) ON, (S/N 10) OFF.Dec 14, 1996 · N750UP · Doug DC871F · Emergency LightingSDR RRXA96172Engine · flamed outNR 1 ENGINE FLAMED OUT DURING DESCENT THROUGH 15,000. CHECKED OIL FILTER CHIP DETECTORS, FUEL FILTER, IGNITION SYSTEM, FUEL TANK SELECTOR RIG, AND LEAK CHECK, NO DEFECTS NOTED. PERFORM CHECKS PER MM 71-00-46. FOUND VBV RIGGING TOO CLOSE, RE-RIGGED VBV PER MDec 13, 1996 · N8079U · Doug DC871F · Engine (Turbine/Turboprop)
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