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.
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 UPS98825804Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 628.750 THE L/E UPPER RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.SDR UPS98825803Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 635.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.SDR UPS98825799Rib · crackedINSPECTION TYPE-C, RT WING L/E AT STA XFS 678.750 - THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.SDR UPS98825762Rib · crackedINSPECTION TYPE:C, RT WING L/E AT STR XFS 653.750, THE L/E RIB IS CRACKED. REPAIRED IAW SRM 57-2-0.SDR UPS98825887Intercostal · crackedINSPECTION TYPE-C, MAIN ENTRY DOOR INTERCOSTAL HAS CRACK IN THE RADIUS AS VIEWED THRU UPPER FWD LIGHTENING HOLE. REPAIRED IAW SRM 52-3-2.SDR UPS98825883Fitting · crackedINSPECTION TYPE-C, LONGERON 34R FITTING AT FS 8 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR UPS98825882Fitting · crackedINSPECTION TYPE-C, LONGERON 33L FITTING AT FS 8 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR UPS98825862Doubler · corrodedINSPECTION TYPE-C, INTERNAL DOUBLER HAS HEAVY CORROSION O/B OF LONGERON 30R BETWEEN FS 35 TO 55. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5649028 AND SRM 51-1-20.SDR UPS98825844Frame · crackedINSPECTION TYPE-C, MAIN ENTRY DOOR LWR FRAME HAS A CRACK AND DEEP GOUGE. REPAIRED CRACKED FRAME IAW SRM 52-2-0 FIG 2.SDR UPS98825843Web · crackedINSPECTION TYPE-C, MAIN ENTRY DOOR LWR AFT WEB IS BENT AND CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT WEB IAW SRM 53-3-2.SDR UPS98825806Longeron · corrodedINSPECTION TYPE-C, LONGERON 30R FS 35 TO 55 HAS HEAVY CORROSION AND OUT OF LIMITS. REMOVED AND REPLACED LONGERON IAW SRM 51-1-20D.SDR UPS98825798Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR STA XFS 822.500. REPAIRED IAW SRM 57-2-0.SDR UPS98825797Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT STA XFS 635.000. REPAIRED IAW SRM 57-2-0.SDR UPS98825795Doubler · corrodedINSPECTION TYPE-C, HEAVY CORROSION BETWEEN INTERNAL DOUBLER AND SKIN AT LONGERON 31R AND BETWEEN FS 35 AND 55. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW SRM 53-3-1 AND 51-1-21.SDR UPS98825792Splice · crackedINSPECTION TYPE-C, NR 1 PIT AT STA 600 TO 620 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR UPS98825791Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT STA XFS 572.500. REPAIRED IAW SRM 57-2-0.SDR UPS98825763Rib · crackedINSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA XFS 810.000. REPAIRED IAW SRM 57-2-0.SDR UPS98825761Rib · crackedINSPECTION TYPE:C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER STA 772.500. REPAIRED IAW SRM 57-2-0.SDR UPS98825845Shear Tie · crackedINSPECTION TYPE-C, STA 641 BETWEEN STR 26R TO 27R, SHEAR TIE HAS A 2 INCH CRACK. REMOVED FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW SRM 53-4-1 FIG 40 AND DWG 5750837.SDR UPS98825716Bottle · low pressureINSPECTION TYPE-A, FOUND ESCAPE SLIDE BOTTLE PRESSURE BELOW MINIMUMS, GUAGE READ 2300 PSI. REMOVED AND REPLACED ESCAPE SLIDE PER MM 25-60-01.SDR RRXA98043Panel · tornDURING A MAINTENANCE VISIT, FOUND NR 2 ENGINE FAN CASE, RT SIDE, AFT THE CLOSE-OUT PANEL ATTACHED TO THE AFT END OF THE STRUT AT 3:00 POSITION WAS SNAGGED DURING ENGINE HOIST, PART WAS TORN ON UPPER FLANGE. REMOVED DAMAGED PANEL, FABRICATED AND INSTALLED NEW SDR RRXA98041Angle · corrosionDURING A MAINTENANCE VISIT, FOUND LONGERON 34 RIGHT, STA 290 TO STA 310, OUTBD ANGLE IS CORRODED BEYOND LIMITATIONS IAW DC-8 SRM. CUT OUT DAMAGE SECTION BETWEEN STA 290 AND STA 310. FABRICATED AND INSTALLED REPAIR DOUBER IAW FAA APPROVED DER TIMCO ENGINEERINSDR IXXA9800042Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON LONGERON 35 LEFT SPLICE FITTING AT FUSELAGE STATION 450. REPAIR WAS ACCOMPLISHED BY REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW SPLICE FITTING IN ACCORDANCE WITH FAA DER APPROVED DRSDR IXXA9800039Fitting · damagedDURING ROUTINE C-CHECK INSPECTION, FOUND LEFT WING NUMBER FIVE SPOILER HINGE FITTING CRACKED. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION NEW HINGE FITTING IN ACCORDANCE WITH DAC DRAWING 3654073 AND ENGINEERING ORDER 27-DC8SDR IXXA9800038Plating · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON LEFT WING LOWER LEADING EDGE BETWEEN STATIONS XS415 AND 422. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION AN INTERNAL FILLER AND AN EXTERNAL REPLAIR DOUBLER IN ACCORDANSDR UPS98826060Web · crackedINSPECTION TYPE-C, RT I/B AILERON, O/B END WEB CRACKED (CLOSURE RIB). REMOVED CLOSURE RIB, FABBED REPAIR DOUBLER FOR IT AND INSTALLED IAW REO 0429A REVA, DC8-SRM 51-1-8 AND DC8 SRM 51-1-21.SDR UPS98825707Battery · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHTS BATTERY DEAD. CHARGED AND REINSTALLED EMERGENCY BATTERY, OP CHKS GOOD.SDR RRXA98040Jamb · corrosionDURING A MAINTENANCE VISIT, FOUND DOOR JAMB WEB AT STA 560 HAS EXFOLIATION CORROSION. CORROSION IS 100 PERCENT THROUGH WEB IN THE CORNER RADIUS. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED NEW WEB AND REPAIR STRAP IAW FAA APPROVED DER TIMCO ENGINEERING SKESDR RRXA98039Angle · misdrilledDURING A MAINTENANCE VISIT, FOUND ADDITIONAL DRILLING HOLES IN THE FUSELAGE TO VERTICAL ATTACHMENT ANGLE AT STA 1766. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04249 AND DC-8 SDR UPS98826059Fitting · crackedINSPECTION TYPE-C, FWD OF ACCESS 560-B, 30 FT INBD OF XW408 CRACKED IN STRINGER END FITTING. REMOVED CRACKED FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-3-2 AND INSTALLED IAW DC8 SRM 51-1-20D.SDR UPS98825991Longeron · damgedINSPECTION TYPE:D/CK STA 340 L28L LONGERON IS DAMAGED AT Z FITTING. BLENDED OUT DAMAGED IAW UPS DC8 SRM 53 2 0. FABBED REPAIR STRAP IAW REO 04279 AND DC8 SRM 51 1 24. ALODINED AND PRIMED REPAIR AREA AND STRAP IAW DC8 SRM 51 1 8. INSTALLED REPAIR IAW REO 04SDR UPS98825733Longeron · corrodedINSPECTION TYPE:D/CK, L33 LEFT STA 190 TO 390 REQUIRED REPLACEMENT. REMOVED LONGERON STA 190-390, DRILLED NEW LONGERON HALVES IAW DC8 SR M 51 1 24. INSTALLED LONGERON WITH HI-LOKS AND RIVET6S IAW DC8 SRM 5 1 1 20D AND 51 1 21.SDR UPS98825998Extrusion · corrodedINSPECTION TYPE:D/CK SURFACE CORROSION ON FLOOR STRUCTURE AT STA 1740. REMOVED CORROSION AND DAMAGED EXTRUSION FABBED NEW EXTRUSION IAW DC8 SRM 53 7 1 AND DWGT 5755032. INSTALLED EXTRUSION IAW DC8 SRM 51 1 20D. ALODINED AND PRIMED IAW DC8 SRM 51 1 8.SDR UPS98825990Rib · crackedINSPECTION TYPE:D/CK LEFT WING MIDDLE LEADING EDGE RIB CRACKED AT FUEL DOOR. RECEIVED REO FABRICATED PARTS HEAT TREATED IAW REO 04277. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW REO 04277 AND DC8 SRM 51 1 20D.SDR UPS98825692Rib · crackedINSPECTION TYPE-C, LT WING L/E RIB CRACKED LWR ARM STA 385.250. REPAIRED IAW SRM 57-3-1.SDR IXXA9800040Splice · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK LOCATED ON LONERGON SPLICE FITTING 32 RIGHT AT FUSELAGE STATION 1350. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION AN NEW SPLICE FITTING IN ACCORDANCE WITH FAA PER APPROVED DRAWING SDR UPS98826080Splice · corrodedINSPECTION TYPE-D/CK, UPPER CARGO SEAT TRACK REPAIR SPLICE CORRODED, MISSING STRAP OPEN HOLES AND 1 STRAP STA 1320 TO 1340 LBL 52. FABBED NEW STRAP, ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-3 AND 51-1-8.SDR UPS98826077Seat Track · corrodedINSPECTION TYPE-D/CK, MAIN CARGO SEAT TRACK ALONG LEFT SIDE, STA 1010 TO 1030 CRACKED AND CORRODED. REMOVED TRACK STA 1010 TO 1090, FABBED AND INSTALLED NEW STICK IAW DC8 SRM 53-2-3.SDR UPS98826076Frame · corrodedINSPECTION TYPE-D/CK, MAIN CABIN STA 150 AT RIGHT HAND CUSP, INSIDE R-1 DOOR, FRAME BOTTOM FWD CORNER CORRODED. REMOVED ANGLE, DRILLED UP REPAIR ANGLE IAW3 DC8 SRM 53-30 AND INSTALLED IAW DC8 SRM 51-1-20.SDR UPS98826070Seat Track · corrodedINSPECTION TYPE-C, UPPER CARGO SEAT TRACK (LOWER SIDE) CORRODED AT STA 1400, RBL 60. REMOVED SEAT TRACK FS 1370 TO 1430 IAW SRM 53-4-1. DRILLED UP NEW TRACK AND SPLICES IAW DC8 SRM 53-4-1 AND 53-2-3. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8. INSTSDR UPS98826065Fitting · crackedINSPECTION TYPE-C, PIT DOOR CLOSE OUT FITTING CRACKED AT FS 1420 BL 0. REMOVED DOOR BARRIER CLOSE OUT. FABRICATED DOUBLER IAW DC8 SRM 53-2- 0. ALODINED AND PRIMED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8, 51-1-20. FABRICATED FITTING IAW 5616673. ALODINED/SDR UPS98826064Seat Track · gougedINSPECTION TYPE-C, CABIN SEAT TRACK H GOUGED AND CRACKED AT STA 575. REMOVED DAMAGE OUT IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PLUG AT STA 575 SEAT TRACK H IAW DC8- SRM 51-30.SDR UPS98826063Bracket · crackedINSPECTION TYPE-C, LT AFT OVERWING EXIT DOOR HAS 2 CRACK IN WINDOW FRAME TEE AT FWD LWR CORNER. REMOVED CRACKED BRACKET AND INSTALLED NEW ONE IAW DC8 SRM 51-1-2- AND 51-1-20D.SDR UPS98826013Seat Track · gougedINSPECTION TYPE:D/CK, CABIN SEAT TRACK I IS GOUGED WORN AND CORRODED STA 270. REMOVED SEAT TRACK PLUG PRIMED SEAT TRACK PLUG IAW DC8 SRM 51 1 8. INSTALLED NEW SEAT TRACK PLUG IAW DC8 SRM 53 2 3.SDR UPS98826011Seat Track · corordedINSPECTION TYPE:D/CK, CABIN SEAT TRACK CORRODED STA 516-530. REMOVED SEAT TRACK STA 410 590. FABBED NEW SPLICES, DRILLED NEW TRACK IAW DC8 SRM 53 3 2 AND 53 21 0. INSTALLED IAW DC8 SRM 53 2 3 AND 51 1 8 AND 51 3 0.SDR UPS98826010Longeron · corrodedINSPECTION TYPE:D/CK, CORROISON ON LONGERON 31 RIGHT BETWEEN STA 640 AND 660. REMOVED CORROSION FABBED REPAIR STRAP PER REO 04338. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8. INSTALLED STRAP IAW DC8 SRM 5 1 1 20D AND 51 1 16.SDR UPS98826009Seat Track · corrodedINSPECTION TYPE:D/CK SEAT TRACK B-C CORRODED AT STA 1240. REMOVED DAMAGED TRACK STA 1190 TO 1270. FABRICATED AND INSTALLED NEW TRACK IAW DC8 SRM 51 3 0 AND 51 1 8 AND 53 2 3.SDR UPS98826008Floorbeam · corrosionINSPECTION TYPE:D/CK CORROSION BETWEEN LAV SUB FLOOR, FLOORBEAMS AND SEAT TRACK, LAV AREA STA 60-70. REMOVED CORROSION FOUND CRACK FLOORBEAM STA 55 RBL 33. REMOVED DAMAGED AREA FABBED REPAIR FILLER AND ANGLE AND INSTALLED PER REO 4350. ALODINED AND PRIMED ASDR UPS98826007Angle · corrodedINSPECTION TYPE:D/CK CORRODED HARDWARE AT STA 70 IN FLOORBEAM AFT OF LAV AREA. REMOVED CORRODED ANGLE AND REPLACED IAW DC8 SRM 51 1 20D AND 51 1 11.SDR UPS98826006Pulley Bracket · corrodedINSPECTION TYPE:D/CK RIGHT MAIN WHEEL WELL FLAP CONTROL PULLEYS WORN AND HARDWARE EVIDENCE OF CORROSION JUST ABOVE GEAR DOOR UPLOCK OTBD. REMOVED AND REPLACED PULLEY BRACKET ON RIGHT SIDE IAW DC8 SRM 51 3 0. REMOVED AND REPLACED PULLEY HARDWARE IAW DC8 MM 20
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