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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UPS99830842Skin · crackedINSPECTION TYPE:C123 RT WING LWR SKIN ABOVE THE NR 4 PYLON HAS A 5 INCH CRACK, JUST OUTBOARD OF THE OUTBOARD SLOT, OUTBOARD END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-1A FIG 1.SDR UPS99830837Skin · crackedINSPECTION TYPE:C123 LT WING L/E UPPER SKIN AT STA XFS307.0 AT THE SPAR IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 38.SDR UPS99830836Skin · crackedINSPECTION TYPE:C123 LT WING L/E UPPER SKIN AT STA XFS591.25, 2 FWD OF THE SPAR IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 38.SDR UPS99830833Skin · crackedINSPECTION TYPE:C123 LT WING L/E UPPER SKIN AT STA XFS628.75 2 FWD OD THE SPAR IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 38.SDR UPS99830803Skin · crackedINSPECTION TYPE:C123, RT WING L/E UPPER SKIN WAS CRACKED AT 3 LOCATIONS: FS 572.0, FS 577.0, & FS 610. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-1 FIG 38.SDR UPS99830800Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIBS AT FS 735.0 & 738.75 WERE CRACKED AT THE AFT UPPER ENDS. STOP DRILLED CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0 FIG 2.SDR UPS99830790Rib · crackedINSPECTION TYPE:C123, RT WING L/E RIBS AT FS 616.25 AND FS 622.5 ARE CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0 FIG 2.SDR UPS99830774Doubler · crackedINSPECTION TYPE:C123, RT WING L/E AT FS 341.5, THE INTERNAL DOUBLER HAD A 7 INCH CRACK. REPAIRED THE DOUBLER IAW DH SK718-263.SDR UPS99830770Skin · crackedINSPECTION TYPE:C123, LT WING L/E UPPER SKIN AT STA XWS 257.5 IS CRACKED AT 6 HOLES AT L/E. REPAIRED AREA IAW SRM 57-2-1 FIG 2H.SDR UPS99830841Skin · crackedINSPECTION TYPE:C123 NR 4 PYLON INBD SKIN AT STA YN 278 IS CRACKED THROUGH A SCREW HOLE. CUT OUT DAMAGED AREA AND REPAIRED IAW DH SK718-147.SDR UPS99830840Angle · crackedINSPECTION TYPE:C123 FWD ACCY COMPT, FS 680, BETWEEN LONG 22R AND 23R, THE ANGLE INSIDE THE A FRAME IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 3642983 AND SRM 5-1-20D.SDR UPS99830793Skin · crackedINSPECTION TYPE:C123, THE FUSELAGE SKIN WAS CRACKED AT FS 1750 AND LONG 14L. CUT OUT THE DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 53-2-1 FIG 7.SDR UPS99830588Skin · crackedINSPECTION TYPE:N/A, FUSELAGE SKIN DAMAGE JUST AFT OF THE NLG W/W HAS AN 11 INCH CRACK. DUE TO LEFT NOSE TIRE TREAD SEPARATION. *S/D* DAMAGE REMOVED AS REQ'D RHODES 75705 RSB 0596 1 QC 2, FABRICATED AND DRILLED DOUBLER PER UPS DRAWING UPS-SDF-9900296 F BPT SDR UPS99830977Frame · crackedINSPECTION TYPE:S/V, STA-117 FRAME CRACKED AT BOTTOM FWD OF NOSE GEAR. FABBED AND INSTALLED REPAIR IAW REA-O6756 DYE PENNED REPAIR PARTS IAW ASTM-E-7417-95A. NO CRACKS NOTED IAW DC8 SRM 51-1-20D.SDR UPS99830976Frame · crackedINSPECTION TYPE:S/V STA-105 FRAME CRACKED BOTTOM FWD OF NOSE. FAB REPAIR ANGLES AND FILLERS IAW REO 06767 DYE PENNED REPAIR PARTS IAW MIL STD 15378, NO CRACKS NOTED ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC 8 51-1-20D.SDR UPS99830870Doubler · corrodedINSPECTION TYPE:SV STA 8 TO 70 FINGER DOUBLER RT SIDE HAS CORROSION. REMOVED AND REPLACED FINGER DOUBLER IAW DC8 SRM 51-1-21, 53-3-1.SDR UPS99830944Frame · damagedINSPECTION TYPE:SV, FUSELAGE FRAME AT STA 80 LT O/B NOSE WHEEL WELL IS DAMAGED. REC'D SERVICEABLE FRAME SECTION FROM AIRCRAFT (S/N 46038), HEAT TREATED REPAIRS DOUBLERS 7075-0--063 TO 7075-T6 IAW TPS 1003 REV A. FABBED DOUBLERS IAW REO 06791. DYE PENT REPAISDR RRXA991636Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE FRAME AT FLOORBEAM AT STA 1727, LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0. (CORROSION SDR RRXA991635Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOORBEAM AT STA 1727 AT FRAME R/S. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOORBEAM IAW FAA DER ENGINEERING SKETCH NR SK-087-316SDR RRXA991471Frame · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE FRAME, AT STA 1727, AT THE FLOORBEAM (LON L/R). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 53-2-0. (CORROSION DAMSDR RRXA991435Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR BEAM AT STA Y1727 AT FRAME. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOORBEAM SECTION IAW FAA APPROVED ENGINEERING SKETCH NRSDR RRXA991629Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, RIGHT, RT OB FLAP AT STA X=410 FLAP SUPPORT FITTING LWR SURFACE UNDER FLAP TRACKS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW SDR RRXA991518Fitting · corrodedDURING A MAINTENANCE VISIT FOUND SPOTS OF CORROSION ON RT O/B FLAP AT STA X-410, FLAP SUPPORT FITTING LWR SURFACE UNDER FLAP TRACKS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW SDR UPS99831047Structure · damagedINSPECTION TYPE:N/A, FUSELAGE NOSE SECTION, INTERM, REPAIR EO DC8 5300-11498A TO INCLUDE REMOVAL OF NOSE LANDING GEAR DOORS, BOTH PAC'S INOP (REF DEFERRAL M- 177745) RT PNEUMATIC PRESSURE INDICATION INOP (REF DEFERRAL M-177744 ) REF INCIDENT NUMBER RS99-288. SDR RRXA991646Retract Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RT MLG, RETACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED RT MLG CYL RETRACT PIN BOSS BORE IAW AAR FAA-99-417 AND EWA MA AI-3210-01:03. (CORROSION DSDR RRXA991645Retract Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT MLG, RETRACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED LT LMG RETRACT PIN BOSS BORE IAW AAR FAA 99-417 AND EWA MA AI-3210-01:03.SDR RRXA991473Retract Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT MLG RETRACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED LT MLG RETRACT PIN BOSS BORE IAW AAR FAA APPROVED DER ENGINEERING SKETCH NR 99-417 AND EMERSDR RRXA991472Retract Pin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, MAIN LANDING GEAR, RIGHT MLG, RETRACT PIN BOSS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REBUSHED RIGHT MLG CYL RETRACT PIN BOSS BORE IAW ARR FAA APPROVED DER ENGINESDR UPS99830527Cylinder · failedINSPECTION TYPE:N/A, LOSS OF MAIN RESERVOIR HYDRAULIC FLUID. AILERON AND RUDDER MAN LIGHT ON, PRESSURE FLUCTUATED. RAN LOSS OF HYDRAULICS CHECKLIST, RECOVERED NORMAL GEAR, FLAPS, BRAKES, NW STEERING. FLT CONT NOTIFIED, DECLARED INFLIGHT EMERGENCY W/ATC. NORSDR UPS99830489Cowl · damagedINSPECTION TYPE:N/A, NR 3 ENG FAN COWL (O/B) DAMAGED WHEN NOSE GEAR COLLAPSED, SEE LOG PAGE 208929 ITEMS 1 AND 2. OPENED COWL TRANSFERRED TO UPS NON-ROUTINE 544690.SDR RRXA991625Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, LE, UPPER SKIN BETWEEN XFS 341.50 AND XOLDI 6.225. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SKIN IAW FAA SKETCH NR 087-252. (COSDR RRXA991465Skin · corrosionDURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, L/E UPPER SKIN BETWEEN STA XFS 341.50 VOID AND STA XFS 6.225. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SKIN IAW FAA APPROVED DER SDR RRXA991626Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, OB, SLOT VANE, INNER DOUBLER AT XOLDI 6.225. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DAC DWG 5769933-21 AND DC8 SRM SDR RRXA991520Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT O/B SLOT VANE INNER DOUBLER HAS HEAVY CORROSION AT STA XOLDI 6.225. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DAC DWG NR 576993SDR RRXA991437Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 31 LEFT BETWEEN STA Y660 AND STA Y680, UPPER FLANGE.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED LONGERON SECTION IAW FAA APPROVED DER ENGINSDR RRXA991634Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 1120, BETWEEN LONGERONS 36 AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED FRAME IAW DC8 SRMSDR RRXA991440Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, RT INBD FLAP UPPER SKIN BETWEEN STA XW0 TO STA XW5, AT 5 TO 6 INCHES FWD OF THE T/E. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SKIN IAW SDR RRXA991432Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME AT FSY 1120, BETWEEN LONGERONS 36 AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED FRAME IAW DC8 SRM 53-2-0 FIG 2. (CORROSIONSDR UPS99830414Strap · brokenINSPECTION TYPE:N/A, RT ESCAPE TAPE RESTRAINING STRAP BROKEN. REMOVED AND REPLACED STRAP.SDR RRXA991627Skin · corrosionDURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, AND BULGED SKIN AT FRONT SPAR, STA XS 250.089. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-0 FIG 2A. (CORROSDR RRXA991516Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT WING, L/E HAS BULGED SKIN AT FRONT SPAR AT STA XS 250.089. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-0, FIG 2A. (SDR RRXA991467Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, LT WING L/E HAS BULGED SKIN AT FRONT SPAR AT STA XS 250.089. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC8 SRM 57-2-0, FIG 2A. (COSDR RRXA991662Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, WING, LT CENTER L/E UPPER RIB CRACKED AT FASTENER END AT STA XFS 347.75, 354, AND 372.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DCSDR RRXA991463Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK, LT CENTER L/E UPPER RIB AT FASTENER END, AT STA XFS 347.75, XFS 354, AND XFS 372.750. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR LT, L/E RIBSDR UPS99830946Frame · damagedINSPECTION TYPE:SV 2 FRAME DAMAGED AT -87 RT O/B OF NWW. REC'D SERVICEABLE FRAME SECTION FROM A/C (S/N 46038). HEAT TREATED REPAIR PARTS 7075-0 TO 7075 T6.063 IAW TPS-1003 REV A. INSTALLED SERVICEABLE FRAME SECTION IAW DC8 SRM 51-1-20D & 51-1-21. FABBED ANSDR UPS99830945Frame · damagedINSPECTION TYPE:SV 2 FRAME DAMAGED AT -87 LEFT O/B NWW. FABBED AND INSTALLED FRAME AND REPAIR PARTS (SPLICES) IAW REO 06776 & DC8 SRM 51-1-20D.SDR UPS99830466Intercostal · corrodedINSPECTION TYPE:SVC, AFT ACCY COMPARTMENT, CORROSION AT INTERCOSTAL ATTACH ANGLE AROUND FASTENERS AND ANGLE, FS 1560 LONGERON 26L. REMOVED INTERCOSTAL(P/N 5615377-93) FAB AND INSTALLED NEW INTERCOSTAL IAW TIMCO REO 06698.SDR UPS99830465Seat Track · corrodedINSPECTION TYPE:SVC, AFT ACCY COMPARTMENT, SEAT TRACK CORRODED BEYOND LIMITS AT FS L3L10. REMOVED SEAT TRACK FROM FS 1500-1700 L3L10 AND SPLICED IN NEW SEAT TRACK SECTION, INSTALLED SPLICES AND REINSTALLED FLOORBOARDS AND CARGO SYSTEM IAW DC8 SRM 53-2-3, 51-SDR RRXA991661Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK, RIGHT WING, L/E UPPER SKIN AT STA XFS 423.25, CRACKED AT 2 RIVET HOLES, ALSO HAS 12 RIVET HEAT CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RSDR RRXA991628Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT, LE, AUX TANK UPPER AFT MOUNTING CHORD BETWEEN STA XFS 7.50 AND XFS 20.0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED THE CHORD IAW D
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