Douglas DC-8-73
Service difficulty reports · 821
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 = 'DC873' 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 = 'DC873' 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 RRXA991080Fitting · damagedDURING A MAINTENANCE VISIT FOUND AN OVERSIZED HOLE, RUDDER SPAR FITTING AT STA ZR=61.156. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR BUSHING IAW FAA APPROVED TIMCO DER ENGINEERING SSDR RRXA991079Bore · oversizedDURING A MAINTENANCE VISIT FOUND BORE OVERSIZED, MAIN LANDING GEAR LINK BORE, AND HAS ONE LOCATION OF LOCAL BLENDING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR BUSHINGS IAW FAA APSDR RRXA991066Mount · misdrilledDURING A MAINTENANCE VISIT FOUND NUMEROUS OVERSIZED HOLES, NR 4 PYLON MOUNT AREA. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH SDR RRXA991078Jamb · misdrilledDURING A MAINTENANCE VISIT FOUND DOUBLE DRILLED IN VARIOUS LOCATIONS, L-2 ENTRY DOOR AFT JAMB AT STA 1666 AND STA 1660. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA SDR RRXA991077Floorbeam · gougedDURING A MAINTENANCE VISIT FOUND GOUGE, FLOORBEAM, FUSELAGE, AT STA 52, UPPER AFT FLANGE HAS DEEP TOOL GOUGE AT BL 36 LEFT ON UNDERSIDE OF FLANGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED IAW FAA APPROSDR RRXA991076Floorbeam · misdrilledDURING A MAINTENANCE VISIT FOUND MISDRILLED, FLOORBEAM, AT STA 660, UPPER FLANGES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-06273 AND DC08-53-0351, SDR RRXA991075Door Pan · misdrilledDURING A MAINTENANCE VISIT FOUND MISDRILLED, AFT SERVICE DOOR, AFT LWR DOOR PAN, IN TWO PLACES. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE, FILLER, AND DOUBLERS IAW FAA APPROSDR RRXA991074Frame · misdrilledDURING A MAINTENANCE VISIT FOUND MISDRILLED HOLE, FUSELAGE, FRAME AT STA 1140, LONGERON 35 LEFT AT AN INTERCOSTAL LOCATION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SDR RRXA991073Floorbeam · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE, FUSELAGE, FLOORBEAM AT STA 1140, BL 0.0, NO SRM. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SHIM, ANGLE, AND DOUBLER IAW FAA APPROVED TIMCOSDR RRXA991072Floorbeam · misrepairedDURING A MAINTENANCE VISIT FOUND TWO CUTOUTS, FUSELAGE, FLOORBEAM, UPPER FORWARD FLANGE, AT STA 680. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW FAA APPROVED TIMCO DER ENGINESDR RRXA991061Fitting · misdrilledDURING A MAINTENANCE VISIT FOUND OVERSIZED HOLE, RUDDER SPAR FITTING AT STA ZR 61.156 HAS OVERSIZED ATTACH HOLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW OVERSIZED BUSHING IAW FAA ASDR RRXA991063Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND CRACKS, FUSELAGE, FLOORBEAM AT STA 160 AND STA 180, BL 40 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED STRAPS, ANGLES, AND DOUBLERS IAW FAA APPROVED TSDR RRXA991062Floorbeam · crackedDURING A MAINTENANCE VISIT FOUND CRACKS, FUSELAGE, FLOORBEAM, AT STA 160 AND STA 180, CRACKED AT APPROX BL 40 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED STRAPS, ANGLES, AND DOUBLERSSDR RRXA991070Floorbeam · damagedDURING A MAINTENANCE VISIT FOUND A TRIM OUT, FUSELAGE, LONGITUDINAL FLOORBEAM AT BL 11.5 RIGHT FROM STA 21 TO STA 25 IN THE UPPER HORIZONTAL FLANGE AND A BLEND OUT IN THE VERTICAL FLANGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAWSDR RRXA991069Fitting · mismanufacturedDURING A MAINTENANCE VISIT FOUND MATERIAL SUBSTITUTION, P/N: 3616112-3 FITTING IS MADE FROM P/N: 3616111 7075-T6 FORGING. REQUEST TO FAB FROM ALUMINUM BAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED ASDR RRXA991160Longeron · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AND CORROSION, FUSELAGE, LONGERON 36 BETWEEN STA 260 AND STA 300. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SECTION OF LONGERON IAW DAC DWSDR RRXA991068Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACKED SPLICE FITTING AT STA 510, LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT SPLICE IAW FAA APPROVED TIMCO DER ENGINEERING SKETCHSDR RRXA991067Fitting · mismanufacturedDURING A MAINTENANCE VISIT FOUND MATERIAL SUBSTITUTION, P/N: 5711283-514-1379 FITTING IS MADE FROM P/N: 4710626-7075-T6 FORGING. REQUEST TO FAB FROM ALUMINUM BAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRSDR RRXA991065Skin · damagedDURING A MAINTENANCE VISIT FOUND DAMAGE, RIGHT WING, O/B L/E LWR SIDE SKIN AT APPROX STA XFS 716.250. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER SDR RRXA991064Skin · damagedDURING A MAINTENANCE VISIT FOUND DRILL DAMAGE, FUSELAGE, SKIN PANEL, JUST FWD OF STA 70 BETWEEN LONGERONS 21 LEFT AND LONGERON 23 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DSDR RRXA991060Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION, LT HORIZ STAB LOWER T/E PANEL APPROX STA XE 272.280. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HORIZ STAB LOWER T/E PANEL IAW FAA APPROSDR RRXA991059Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION, LT HORIZ STAB LOWER T/E PANEL APPROX STA XE 221.227. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HORIZ STAB LOWER T/E PANEL IAW FAA APPROSDR RRXA991058Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION, LT HORIZ STAB LOWER T/E PANEL APPROX STA XE 149.155. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HORIZ STAB LOWER T/E PANEL IAW FAA APPROSDR RRXA991057Door Frame · crackedDURING A MAINTENANCE VISIT FOUND CRACK, MAIN CARGO DOOR FRAMES AT FS 465 AND FS 495 LOWER LATCH MOUNTS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR CHANNEL IAW FAA APPROVED TIMCO DESDR RRXA991056Frame · gougedDURING A MAINTENANCE VISIT FOUND GOUGE, FUSELAGE, FRAME AT STA 1460 BETWEEN LONGERONS 35 LEFT AND LONGERON 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPRSDR RRXA991055Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND DOUBLE DRILLED, FUSELAGE, FLOORBEAM SUPPORT AT STA 380. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE AND DOUBLERS IAW FAA APPROVED TIMCO DER ESDR RRXA991054Fitting · mismanufacturedDURING A MAINTENANCE VISIT, FOUND P/N: 3755894-2 FITTING, FUSELAGE, MADE FROM P/N: 3755894-4 7075-T6 FORGING (MATERIAL SUBSTITUTION). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. SHOT PEEN FABRICATED AND INSTALLED SDR RRXA991052Nutplate · misinstalledDURING A MAINTENANCE VISIT, FOUND NUTPLATES INSTALLED WHICH ARE NOT BEING USED, FUSELAGE, BETWEEN STA 500 AND STA 520, BETWEEN LONGERONS 35 LEFT AND 35 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATEDSDR RRXA991053Spar · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, WING, LT I/B FLAP REAR SPAR UPPER CAP AT STA XW 97. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT SECTION OF SPAR, REPAIR ANGLES, ANDSDR RRXA991051Floorbeam · damagedDURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE, FUSELAGE, FLOORBEAM AT FS 960 IN THE CAP AND VERTICAL FLANGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE AND DOUBLERS IAW FAA SDR RRXA991159Spar · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, OUTBOARD FLAP, REAR SPAR CAP AT XF=225, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED TIMCO DER SDR RRXA991050Fitting · wornDURING A MAINTENANCE VISIT, FOUND WORN AREA, WING, LT I/B FLAP ATTACH FITTING AT STA 3 WORN GREATER THAN 20 PERCENT OF THE MATERIAL THICKNESS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AND REPAIRED IAW FSDR RRXA991049Floorbeam · damagedDURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE, DOUBLE DRILLED HOLES AND HOLES, FUSELAGE, MAIN CABIN FLOOR BEAMS AT VARIOUS LOCATIONS BETWEEN STA 70 AND STA 200. DAMAGE WAS CAUSED FROM A PREVIOUS MOD.. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TSDR RRXA991048Fitting · gougedDURING A MAINTENANCE VISIT, FOUND GOUGE, LT WING, CANOE FITTING, AT STA 97.906, ON OUTBD AFT EDGE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDED AND REPAIRED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR SDR RRXA991047Skin · damagedDURING A MAINTENANCE VISIT, FOUND DAMAGE, UPPER SKIN, RT O/B AILERON AT STA XW 698. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCSDR RRXA991046Angle · crackedDURING A MAINTENANCE VISIT, FOUND CRACK, AT A FASTENER HOLE, FUSELAGE, AFT 'L' ANGLE, AT FS70 AT LONGERON 36 IS CRACKED OUT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IASDR RRXA991045Skin · damagedDURING A MAINTENANCE VISIT, FOUND DAMAGE, SKIN, RT O/B UPPER SKIN RT O/B AILERON AT FWD AREA BETWEEN STA XA 630.250 AND 608.634. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER SDR RRXA991043Floorbeam · damagedDURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE, FUSELAGE, FLOORBEAM, AT FS 857, AT BL 0 AND RL 20 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE AND DOUBLER IAW FAA APPROVSDR RRXA991157Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA 70 BETWEEN LONGERONS 21 LEFT TO 34 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED TIMCO DSDR RRXA991042Fitting · wornDURING A MAINTENANCE VISIT, FOUND ATTACH FITTING WORN, RT I/B FLAP I/B ATTACH FITTING WORN AREA IS GREATER THAN 20 PERCENT OF THE MATERIAL THICKNESS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTSDR RRXA991040Fitting · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, FORWARD HORIZONTAL FLANGE OF THE FITTING AT FS 1151, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE AND SDR RRXA991158Spar · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, OUTBOARD FLAP, REAR SPAR CAP AT XW=220, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED TIMCO DER ESDR RRXA991041Floorbeam · damagedDURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE, DOUBLE DRILLED HOLES AND HOLES IN BEAM RADIOUS, FUSELAGE, MAIN CABIN FLOORBEAMS, UPPER FLANGES BETWEEN STA 8 AND STA 70 AT BL 46.5 RIGHT AND BL 46.5 LEFT. DAMAGE WAS CAUSED FROM A PREVIOUS MOD. DAMAGE EXCEEDEDSDR RRXA991156Spar · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, OUT-BOARD FLAP, SPAR CAP AT XF=410, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED TIMCO DER ENGINSDR RRXA991155Spar · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING OUT-BOARD FLAP REAR SPAR CAP BETWEEN XF=404 TO XF=405, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVE DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVSDR RRXA991017Angle · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, SPAR CAP, AT STA 857, BETWEEN BL 13 RIGHT AND BL 18 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW DC8 SRM 53-2-5 FIG 1SDR RRXA980246Seal · failedLOST LT PACK AT 35,000, CABIN DEPRESSURIZED, DEPLOYED MASKS. SUSPECT TURBINE IN TRIP. REF 6671-03 AND 6671-08, SAME CONDITION. PACK TEMP WAS ABOVE 85 DEG C. ALSO, NOTABLE FLOOR VIBRATION INDICATED. DESCENDED TO 31,000 RE-INSTATED L-PACK AND OPENED COOLINGSDR DHL98801003Wheel · missingWHILE RETURNING TO RAMP, AIRCRAFT GROUND HANDLING BECAME ABNORMAL. INSPECTION REVEALED NUMBER 2 TIRE MISSING AND NUMBER 1 TIRE FAILED. REMOVED AND REPLACED NUMBER 1 AND NUMBER 2 MAIN WHEEL ASSY AND NR 2 WHEEL TRANSDUCER.SDR RRXA98004Ballast · failedTHERE WAS A FLASH AND THEN ELECTRICAL SMOKE FROM F/O'S SIDE PANEL UNDER WINDOW, BY MAP LIGHT. SMOKE STOPPED QUICKLY AND CLEARED OUT. NO PROBLEM AFTER THAT. FOUND GLARESHIELD FLUORESCENT LIGHTS INOP. REPLACED BALLAST PER MM 33-12. GLARESHIELD FLUORESCENT LSDR DHL97801003Rt Unit · failedRADAR TESTED NORMAL ON GROUND AND IN FLIGHT BUT, WILL NOT NOT PAINT ANYTHING IN ANY OTHER MODE. RETURNED TO MIA , DUMPED FUEL. REMOVED AND REPLACED RADAR R/T UNIT PER MM 34-41-0. SYSTEM OPS CHECK OK.
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