Douglas DC-8-63F
Service difficulty reports · 1,883
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 = 'DC863F' 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 = 'DC863F' 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 ABXA9800497Skin · crackedLEFT WING UPPER TRAILING EDGE SKIN STATION XRS 160 AT THE REAR SPAR IS CRACKED IN 2 PLACES. REPAIRED SKIN IAW DC8 SRM 57-2-0.SDR ABXA9800496Skin · crackedRIGHT WING LEADING EDGE SKIN UPPER SURFACE AT STATION XFS 197 IS CRACKED AT A FASTENER HOLE. REPAIRED LEADING EDGE SKIN IAW DWG 5769859 AND DC8 SRM 57-2-0.SDR ABXA9800489Skin · crackedLEFT WING LEADING EDGE UPPER SKIN INTERNAL DOUBLER AT STATION XS 251 CRACKED. REPAIRED IAW DACO DWG 5769759 AND DC8 SRM 51-3-0.SDR IXXA9800088Fitting · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON A FUSELAGE FITTING BETWEEN FUSELAGE STATION 70 AND 80, LONGERON 33 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING. FABRICATION AND INSTALLATION A NEW FITTING IN ACCORDANCE WITH DOUGLAS DRAWISDR IXXA9800091Plating · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RUDDER RIGHT SIDE EXTERNAL PLATING AND STATION ZR208.625. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWISDR IXXA9800087Plank · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON NUMBER FOUR PYLON INTERMEDIATE OUTBOARD PLANK AT STATION YIP 241. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION OF AN INTERNAL AND EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH DSDR ABXA9800657Bulkhead Web · cracked1 .5 INCH CRACK AT AFT BULKHEAD STATION 1890, UPPER RIGHT CORNER ABOVE BRACKET WITH MOUNT BOLT FOR RUDDER POWER MECHANISM. REPAIRED IAW DC8 SRM 52-2-0.SDR IXXA9800075Plating · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING LOWER LEADING EDGE AT STATION XFS 304. REPAIR ACCOMPLISHED STOP DRILL CRACK, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-8-57SDR RRXA98221Wire · brokenSTRONG ELEC ODOR DEVELOPING IN COCKPIT. TURNED OFF MAX WHITE LIGHTS. ODOR DISSIPATED. DEFERRED PER MEL 33-1 CAT 'C' DUE 6-9-98 CONT NR 805491. PLACARD INSTALLED, CONNECTOR DISCONNECTED. FOUND 2 WIRES BROKEN AT CONNECTOR.SDR IXXA9800085Longeron · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED BETWEEN FUSELAGE STATION 180 AND 220, LONGERON 31 LEFT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION A NEW LONGERON SPLICE FITTING IN ACCORDANCE WITH FAA DER APPROVED DRAWINGS COSDR ABXA9800658Bulkhead · crackedLEFT WING CANTED BULKHEAD LOWER FLANGE CRACKED AT XRS 508.977 BETWEEN STRINGERS 63-64. REPAIRED IAW ABX REA D853-22858MR AND DC8 SRM 51-1-20D.SDR IXXA9800084Plank · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON NUMBER TWO PYLON OUTBOARD INTERMEDIATE PLANK PANEL AT STATION YN 190. REPAIR ACCOMPLISHED STOP DRILL CRACK, FABRICATION AND INSTALLATION AN INTERNAL AND EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH FAASDR ABXA9800656Fitting · crackedATTACH FITTING AT CANTED STATION XRS 495 TO STRINGER 63 (UPPER SKIN) HAS CRACK AT LAST FASTENER HOLE. FABRICATED REPLACEMENT ATTACH FITTING IAW DWG 3648143 AND ABX REA 857-22859.SDR ABXA9800655Angle · crackedCRACK IN LEFT WING REAR SPAR LOWER CAP STATION 857 LBL 70 INBOARD APPROXIMATELY 9 LEFT MLG WHEEL WELL, FORWARD, LOWER, OUTBOARD. REPAIRED IAW DWG SR08570009 AND DC8 SRM 51-1-8 AND 51-1-20D.SDR IXXA9800083Plank · wornDURING ROUTINE C CHECK INSPECTION, WEAR WAS DETECTED ON THE NUMBER FOUR PYLON UPPER INBOARD PLANK SIX INCHES FORWARD OF STATION YUS 297. REPAIR ACCOMPLISHED BLENDING, POLISH THE AFFECTED AREA IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-SJO-98-0351, FAX ACSDR IXXA9800093Jamb · crackedDURING ROUTINE C CHECK INSPECTION, A CRACKED FITTING WAS DETECTED AT UPPER TORQUE BOX FORWARD DOOR JAMB, AFT CARGO COMPARTMENT AT FUSELAGE STATION 1177 - X 68. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW FITTING IN ACCORSDR IXXA9800089Plating · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED AT AFT ACCESSORY COMPARTMENT INTERNAL DOUBLER AT FUSELAGE STATION 1620, BETWEEN LONGERONS 24 AND 27 LEFT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION REPAIR FILLERS, REPAIR DOUBSDR IXXA9800086Doubler · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LOWER FUSELAGE, EIGHT EACH EXTERNAL FINGER DOUBLERS BETWEEN FUSELAGE STATIONS 1352 AND 1586.5. REPAIR ACCOMPLISHED TRIMMING OFF THE CORRODED FINGERS OF THE AFFECTED DOUBLERS IN ACCORDANCE WITH DOUGLSDR IXXA9800072Plating · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATIONS 1610 AND 1700, LONGERONS 31 LEFT AND 31 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION A NEW SECTION OF PLATINSDR ABXA9800651Frame · crackedSTATION 1040 FRAME UPPER CHORD, LOWER SURFACE AFT SIDE, AT LONGERON 31R AND 32R HAS HEAVY EXFOLIATION CORROSION AND IS CRACKED. REPAIRED IAW ABX REA D853-22857, SRM 51-1-21, 51-1-20D AND 51-1-11.SDR IXXA9800074Floor · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON MAIN CABIN FLOOR PRESSURE PANEL BETWEEN FUSELAGE STATION 863 AND 878, BL +X4 TO -X5.50. REPAIR ACCOMPLISHED CORROSION BLEND OUT, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH FSDR IXXA9800073Plating · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATION 301.5 AND 324, LONGERONS 33 AND 34 LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION TWO INTERNAL FILLERS AND AN EXTSDR ABXA9800591Skin · crackedTWO .25 INCH CRACK ON FWD PASSENGER ENTRY DOOR LOWER AFT CORNER SKIN PANEL. REPAIRED IAW DC8 SRM 53-2-0.SDR ABXA9800592Rib · crackedRIGHT WING LEADING EDGE AT STATION XFS 641.25 IS CRACKED AT UPPER END. REPAIRED IAW DRAWING ABX K05056.SDR ABXA9800556Fitting · crackedSTATION 440 TO 460 LONGERON 31R SPLICE FITTING IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21D AND 51-1-20D.SDR ABXA9800555Fitting · crackedSTATION 600 TO 620 LONGERON 31L SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.SDR ABXA9800593Fitting · crackedSTATION 1120 FRAME TO CUSP FITTING, RIGHT SIDE IS CRACKED. REPAIRED IAW DC8 SRM 51-1-18 AND DWG 9755584.SDR ABXA9800594Rib · crackedLEFT WING LEADING EDGE STUB UPPER RIB CRACKED AT APPROXIMATELY XFS.550. REPAIRED IAW DC8 SRM 51-1-8, 51-1-20D AND ABX DWG K05056.SDR ABXA9800595Doubler · corrosionRIGHT WING LEADING EDGE LOWER SKIN DOUBLER FORWARD EDGE BETWEEN STATION XFS 372.75 AND XF 379.0 HAS HEAVY EXFOLIATION CORROSION. REPAIRED IAW DC8 SRM 51-3-0 AND DWG 5641253.SDR IXXA9800109Doubler · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LEFT MAIN LANDING GEAR LOWER SUPPORT DOUBLER. REPAIR ACCOMPLISHED CORROSION REMOVAL IN ACCORDANCE WITH DOUGLAS FAX ACTION NUMBER 368547 AND 368589 AND ENGINEERING ORDER 57-DC8-904.SDR CKSA98341Seat Track · damagedFOUND TWO SECTIONS OF SEAT TRACK DAMAGED AT STA 380 ON NR 1 AND NR 2 TRACKS AFTER REMOVAL OF CARGO. REPAIRED DAMAGED AREAS OF SEAT TRACK IAW DOUGLAS DC-8 SRM CH 53-2-3. NON-ROUTINE M-7 ITEM 1 LOG PAGE 815-0860.SDR ABXA9800596Fitting · crackedAFT END FITTING ON LONGERON INTERCOSTAL AT STATION 717, LONGERON 14L IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-20D.SDR ARWA980504Wire Rope · brokenSJU - FLT 510 - ON PRE-DEPARTURE CHECK, FOUND MANUAL REVERSION LIGHT ON WITH GUST LOCK LOCKED. FABRICATED GUST LOCK CABLE RUN IAW MM 91-10-22. INSTALLED IAW MM 27-70-0, OPS CHECKED NORMAL. (M)SDR ABXA9800924Rib · crackedNR 4 PYLON UPPER RIB HAD CRACK AT END. REPAIRED IAW DC8 SRM.SDR ABXA9800564Angle · crackedTORQUE BOX WEB LOWER SUPPORT ANGLE CRACKED FROM FS 190 TO FS 200, LONGERON 21R. REPAIRED IAW DWG 575700 AND DC8 SRM 51-1-21, 51-1-21D AND 51-1-8.SDR ABXA9800563Web · crackedLOWER TORQUE BOX WEB CRACKED AND CORRODED BEYOND LIMITS, FWD GALLEY DOOR FS 150 TO FS 160, LONGERON 17R TO LONGERON 21R. REPAIRED IAW DC8 SRM 51-1-21, 51-1-20, 51-1-8 AND 51-1-11.SDR ABXA9800577Fitting · crackedSTRINGER NR 59 END FITTING CRACKED AT NR 4 ALTERNATE FUEL TANK. INSTALLED REPLACEMENT FITTING PER DWG 5644973, DC8 SRM 51-1-20D AND 51-1-23.SDR ABXA9800576Fitting · crackedLONGERON END FITTING AT STATION 742 LONGERON 19L CRACKED. REPLACED FITTING PER DC8 SRM 51-1-20D.SDR ABXA9800575Skin · corrosionRIGHT WING LEADING EDGE UPPER SKIN AT STATION XFS 610 HAS HEAVY CORROSION AND IS CRACKED. REPAIRED IAW DC8 SRM 52-2-1 AND 51-1-21.SDR ABXA980578Rib · crackedRIGHT WING LEADING EDGE RIB AT STATION XS 442.185 IS CRACKED AT AFT UPPER END. INSTALLED ANGLE REPAIR DOUBLERS IAW DC8 SRM 51-1-21 AND 51-1-20D.SDR ABXA9800586Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 354.0 IS CRACKED AT THE AFT UPPER END. INSTALLED REPAIR ANGLES IAW DC8 SRM 51-1-20D AND 51-1-8.SDR ABXA9800579Intercostal · crackedLEFT WING LEADING EDGE JUST OUTBOARD OF THE LEADING EDGE AUX TANK, THE INTERCOSTAL IS CRACKED AT THE INBOARD END. REPAIRED IAW DC8 SRM 51-01-20 AND DOUG DWG NR 5769859.SDR ABXA9800557Rib · crackedLEFT WING LEADING EDGE RIB STATION XS 227.335 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056 AND SRM 51-1-20D.SDR ABXA9800559Angle · crackedLEFT INBOARD STUB WING HAS 2 CRACKS AT STATION XS 250.089. REPAIRED IAW DC8 SRM 57-2-0, 51-1-8, AND 51-1-20D.SDR ABXA9800558Rib · crackedLEFT INBOARD STUB WING STATION XS 250.089 UPPER LEADING EDGE RIB CRACKED. REPAIRED IAW DC8 SRM 51-1-8, 51-1-20D AND DWG K05056.SDR ABXA9800562Rib · crackedRIGHT WING OUTBOARD SLOT, OUTBOARD UPPER CLOSURE RIB IS CRACKED. REPAIRED IAW DC8 SRM 51-3-0 AND 51-1-21.SDR ABXA9800561Rib · crackedTHE LEFT OUTBOARD SLOT OUTBOARD UPPER CLOSURE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DC8 SRM 51-1-21 AND 51-1-20D.SDR ABXA9800560Stiffener · crackedLEFT INBOARD STUB WING AT STATION XS 250.089, THE VERTICAL STIFFENER ANGLE (RIB ATTACH ANGLE) IS CRACKED AT THE BOTTOM END. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-8.SDR ABXA9800532Fitting · crackedSTATION 1040-1060 STRINGER 31L SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D.SDR ABXA9800531Bracket · crackedLEFT WING OUTBOARD LEADING EDGE FWD TAI SUPPORT BRACKET BETWEEN STATION XFS 603.75 AND 610 IS CRACKED IN TWO PLACES. REPAIRED IAW DC8 SRM 51-1-8 AND 51-1-20D.
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