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 CKSA97492Stringer · corrodedDURING ROUTINE B CHECK INSPECTION, FOUND STR 30 RT SIDE HAS CORROSION INSIDE AC JUST FWD OF STA 55. REMOVED STR 30 AND REPLACED IAW DC8 SRM 53-1-0. NON-ROUTINE TASK CARD NUMBER 001331.SDR CKSA97491Fitting · corrodedDURING ROUTINE B CHECK INSPECTION, FOUND EXFOLIATION CORROSION ON NR 27RT STRINGER END FITTING AT FS70. REMOVED AND REPLACED STRINGER END FITTING IAW DC8 SRM 53-1-0. NON-ROUTINE TASK CARD NUMBER 001321.SDR CKSA97490Skin · corrodedDURING ROUTINE B CHECK INSPECTION, FOUND STA 25 LONGERON 31R CORRODED. REMOVED DAMAGED AREA AND REPAIRED IAW AIA/E/2631. NON-ROUTINE TASK CARD NUMBER 001310.SDR CKSA97489Intercostal · corrodedDURING ROUTINE B-CHECK INSPECTION, FOUND AFT OF STA 8 INTERCOSTAL BELOW L30R SKIN BULGING AND RIVET HEADS POPPED. REMOVED DAMAGED AREA AND REPAIRED IAW AIA/E/2632 AND 2624 PER EDR D8-05493 AND EDR D8-05485. NON-ROUTINE TASK CARD NUMBER 001037.SDR RRXA97256Support · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE PAST LIMITATIONS ON FLOOR SUPPORT AT, STA 1660 AND BL 33 RIGHT. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED (2 EACH) FILLERS AND DOUBLERS IAW FAA DER APPROVED ENGINEERING SKETCH D02-R15 AND DC-8SDR RRXA97264Longeron · crackedDURING A MAINTENANCE VISIT, FOUND CRACK ON LONGERON 34 RIGHT AT, STA 1270. *S/D* REMOVED LONGERON 34R, FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH D02-R09.SDR ABXA9701866Fitting · corrodedFITTING AT STA 920 CORRODED. FABRICATED AND INSTALLED FITTING IAW DACO DWG NR3649114.SDR ABXA9701864Skin · crackedRT WING LOWER SKIN STA 69.5 HAS CRACKS. REPAIRED IAW DACO DWG J060095 AND ABX EA 57300008-0030.SDR RRXA97242Fire Warning · malfunctionedINTERMITTENT FIRE WARNING ON NR 2 ENG. SHUT BLEED AIR OFF ON NR 2, NO FURTHER WARNINGS, FIRE WARNING TEST GOOD. COULD NOT DUPLICATE PROBLEM. TIGHTENED PNUE CLAPS ON NR 2 PNUE PRESSURE REG, NO OTHER DEFECTS NOTED. ON GROUND RUN NR 2 ENG FIRE WARNING OPS CHESDR RRXA97319Skin · damagedDURING A MAINTENANCE VISIT, FOUND FUSELAGE OUTER SKIN BENT AND DAMAGED BELOW A PIT DOOR BETWEEN STA 296 TO STA 302. REMOVED DAMAGED SKIN SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D02-R01.SDR RRXA97252Skin · corrodedDURING C-CHECK INSPECTION, FOUND BULGE IN FUSELAGE SKIN LONGERON 28 LT FS 1655 TO 1660.SDR RRXA97249Pressure Web · corrodedDURING C-CHECK INSPECTION, FOUND PRESSURE WEB UPPER SURFACE CORRODED FS 923 BL 0.SDR RRXA97251Angle · corrosionDURING C-CHECK INSPECTION, FOUND LT WING INBD L/E UPPER SCREW ATTACH HOLES CORRODED AT ATA XFS 41 TO 55. *S/D* REMOVED CORROSION AND FOUND LEADING EDGE UPPER SPAR ATTACHMENT ANGLE DAMAGED BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED ATTACHMENT ANGLE, FABRICATEDSDR RRXA97250Angle · corrosionDURING C-CHECK INSPECTION, FOUND LT WHEEL WELL UPPER PRESSURE WEB ATTACH ANGLE CORRODED FS 857 BL 41 TO 46 LT. *S/D* REMOVED ATTACHMENT ANGLE, REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-5 FIGURE 16 SHEET 2. TREATED AREA IAWSDR RRXA97248Skin · corrodedDURING C-CHECK, INSPECTION FOUND RT FWD WASTE SERVICE DOOR HINGE ATTACH AREA IS CORRODED FS 83 TO 96, LONGERON 27 RT AND 28. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA DER COTNEY ENGINEERING SKETCH D02-R10. TRESDR RRXA97247Frame · corrodedDURING C-CHECK INSPECTION, FOUND FS 1020 FRAME HAS CORROSION ON UPPER FWD FLANGE ABOVE LONGERON 33 AND 34 LT.SDR RRXA97246Skin · crackedDURING C-CHECK INSPECTION, FOUND LT WING CENTER OF LEADING EDGE CRACKED AT SCREW HOLE (LOWER SURFACE) STA XFS 520. *S/D* REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER, IAW FAA DER APPROVED ENGINEERING SKETCH D02-R12, AND TREATED ARSDR RRXA97245Skin · corrodedDURING C-CHECK, INSPECTION FOUND SKIN UNDER LONGERON 35 RT BETWEEN FRAMES 1060 AND 1080 TO BE CORRODED.SDR RRXA97244Rib · crackedDURING C-CHECK INSPECTION, FOUND OTBD RIB ON INBD LT FLAP CRACKED IN RADIUS.SDR RRXA97243Longeron · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 35 RT CRACKED ON SIDE AT FS 1270. *S/D* REMOVED LONGERON 35R, FABRICATED AND INSTALLED NEW LONGERON IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH D02-R09.SDR RRXA97240Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM AT, STA 920 RT. *S/D* REMOVED CORROSION DAMAGE FROM FLOORBEAM, FABRICATED AND INSTALLED REPAIR ANGLES IAW FAA APPROVED COTNEY ENGINEERING SKETCH D02-R04 AND DC-8 SRM 51-1-8, 51-1-20D AND 51-1-21SDR ABXA9701447Skin · gappedA GAP WAS DISCOVERED BETWEEN NR 2 PYLON APRON AND COWLING AT FWD LEADING EDGE. REPAIRED IAW ABX REA D854-20688.SDR RRXA97239Skin · crackedDURING A MAINTENANCE VISIT, FOUND CRACK ON RIGHT WING UPPER SKIN AT XFS= 520. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA DER COTNEY ENGINEERING SKETCH D02-R06, DC-8 SRM 51-1-21 AND 51-3-0.SDR RRXA97238Rib · crackedDURING A MAINTENANCE VISIT, FOUND CRACK DAMAGE RIGHT FLAP RIB AT, XFS= 38.SDR RRXA97227Pressure Panel · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION/CRACKED ON PRESSURE PANEL WEB AT, STA 920, BL 62 LEFT. *S/D* REMOVED CORROSION DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCHES D02-R04 AND D02-R07 AND DSDR RRXA97228Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE AND CRACK ON INNER SKIN AT, STA 380 TO STA 400 AND BETWEEN LONGERONS 31 RIGHT AND 34 RIGHT. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER AND FINGER DOUBLER IAW FAA DER APPROVED ENGISDR RRXA97226Skin · crackedDURING A MAINTENANCE VISIT, FOUND LEFT WING LEADING EDGE OF STUB WING UPPER SURFACE SKIN CRACKED AT SCREW HOLE XFS=461. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA DER APPROVED ENGINEERING SKETCH D02-R02, AND DC-SDR ABXA9701863Panel · crackedRT 505F PANEL LAND, 7 HOLES HAVE CRACKS. REPAIRED IAW ABX REA D857-20366MR.SDR ABXA9701862Doubler · crackedRIGHT WING CENTER LEADING STATION XFS 518 HAS CRACK ORIGINATING FROM FASTENER HOLE. REPAIRED IAW ABX REA D857-20383MR.SDR ABXA9701865Door · corrodedRIGHT CORNER OF ASSY COMPT DOOR HAS INTERNAL CORROSION. REPAIRED IAW ABX REA D853-20387MR.SDR ABXA9701408Skin · excessive gapDURING PREFLIGHT, FOUND EXCESSIVE GAP AT LEADING EDGE OF NR 3 PYLON. INSTALLED SEAL AND STAINLESS STEEL STRIP IAW ABX REA D854-20655.SDR RRXA97219Oil Press Ind · malfunctionedNR 3 ENGINE OIL PRESSURE INDICATOR READS 100 PSI. PRECAUTIONARY ENGINE SHUT DOWN AND RESTART IN FLIGHT.SDR RRXA97218Oil Temp Ind · malfunctionedNR 2 ENGINE SHUTDOWN DURING FLIGHT AT 0414Z FOR HIGH OIL TEMP. WINDMILL OIL PRESSURE .23 PSI. ADJUST ACCORDING TO SPEED AS EXPECTED. FUEL TO ENGINE WINDMILLED FROM 0457 - 0500Z. INSPECTED ENGINE IAW EWA JRH PAGE 69-70 OIL TEMP WAS WITHIN LIMITS, NO DEFECTSSDR IXXA9700107Ballast · burntAFTER TAKEOFF TOL, SMOKE EMANATED FROM FLIGHT ENGINEER'S PANEL IN THE VICINITY OF THE CABIN PRESSURE CONTROLLER AND THE HYDRAULIC SELECTOR CONSOLE. FLIGHT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE FOUND THAT THE F/E'S INSTRUMENT WHITE LIGHTING BSDR ARWA970702Oil Tube · looseNUMBER 3 ENGINE OIL QUANTITY ZERO, PRESSURE FLUCTUATION, ENGINE SHUTDOWNAT 0047Z3 WINDMILL OIL PRESSURE 15 PSI. FOUND B-NUT LOOSE ON THE NR 6 BEARING OIL TRANSFER TUBE TO ENGINE CASE FITTING.SDR RRXA97212Fire Loop · failedNR 2 ENGINE FIRE WARNING AT CRUISE. SHUT DOWN ENGINE IAW QRH. ALL INDICATIONS OF FIRE WARNING ERASED. REMOVED AND REPLACED LOWER AND UPPER AFT FIRE LOOPS (NR 2 ENG). NR 2 FIRE WARNING SYSTEM OPS CHECK GOOD, NO DEFECT NOTED.SDR ABXA9701277Line · leakingHYDRAULIC FLUID LOSS OCCURRED ON CLIMBOUT. EMERGENCY CHECKLIST WAS ACCOMPLISHED. SYSTEM WAS ISOLATED, HYDRAULIC QUANTITY STABILIZED ABOVE STANDPIPE. WHEN AUX PUMP WAS TURNED ON DURING DESCENT, LOSS OF FLUID RESUMED UNTIL SELECTING LANDING GEAR DOWN AND FLAPSDR ABXA9701260Panel · crackedDURING COMPLIANCE WITH AD 90-16-05 AND SB 55-15R3, FOUND HORIZONTAL STABILIZER HAD .75 INCH CRACK, AT LT FORWARD LOWER CONSTANT BOX PANEL. PLACED ON CONTINUING INSPECTION EVERY 900 FLIGHT HOURS OR EVERY 3 MONTHS (WHICH EVER COMES FIRST) IAW DAC SB 55-15.SDR ABXA9701252Air Distribution · odorDURING CRUISE EXPERIENCED STRONG HYDRAULIC FLUID ODOR IN COCKPIT. FLUID ODOR WAS FOUND TO BE RESIDUAL FLUID FROM PREVIOUS HYDRAULIC LEAK AT CARGO DOOR HYDRAULIC PUMP. CLEANED RESIDUAL FLUID.SDR IXXA9700085Electrical Syst · odorEN ROUTE, CREW NOTICED HOT ELECTRICAL SMELL IN COCKPIT BELOW THE CIRCUIT BREAKER PANEL. SMELL DISSIPATED AFTER ABOUT 1 MINUTE. FOLLOWING AN UNEVENTFUL LANDING IN TOL, MAINTENANCE INVESTIGATED THE ORIGIN OF THE SMELL. NO CAUSE WAS FOUND AFTER A COMPLETE ENGISDR ABXA9701406Doubler · crackedDURING C-CHECK, FOUND CRACK EMANATING FROM FASTENER HOLE AT RIGHT WING STATION XFS 518. REPAIRED INTERNAL DOUBLER IAW ABX REA D857-20383MR.SDR RRXA97184Damper Unit · malfunctionedELEVATOR HAS BUFFETING AS AIRSPEED INCREASES. WHEN THE AIRPLANE IS BANKED AND ELEVATOR BACK PRESSURE IS APPLIED, BUFFET INCREASES, ON FINAL APPROACH FOR LANDING, FULL FLAPS, SPEED 160KTS BUFFETING IS ALSO FELT IF ELEVATOR BACK PRESSURE IS APPLIED. NOTE: PTCSDR RRXA97183Elevator Control · flutterELEVATOR HAS AREO DYNAMIC FLUTTER AS THE AIRSPEED INCREASES, THE FLUTTER RATE INCREASES. AT 300 KTS IAS THE FLUTTER IS FAST ENOUGH THAT IT FEELS LIKE A BUZZ. INSPECTED ELEVATOR SYSTEM IAW MM CHAPTER 27-40-0, NO DEFECTS NOTED, ELEVATOR SYSTEM OPS CHECK GOOD.SDR ABXA9701124Angle · corrodedDURING C-CHECK, FOUND RIGHT FWD SERVICE DOOR FWD LOWER ANGLE AT CUSP CORRODED. FABRICATED AND INSTALLED NEW ANGLE IAW DC8 SRM 51-1-24 AND ABX REA D853-19482.SDR ABXA9701123Skin · corrodedRIGHT FLAP, TOP SIDE, INBOARD EDGE FOUND CORRODED DURING C-CHECK. REMOVED CORROSION, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW DC8 SRM 51-1-8 AND 57-2-1.SDR ABXA9701122Support · crackedFLOOR SUPPORT CRACKED AT STA 759 AND 875.375, BETWEEN SEAT TRACKS C AND D. FABRICATED SUPPORT ANGLES AND INSTALLED IAW DC8 SRM 51-1-8 AND ABX REA 853-19470.SDR ABXA9701121Skin · corrodedDURING C-CHECK, FOUND CORROSION ON LEFT WING LEADING EDGE AT XFS 285 ON UPPER SURFACE. INSTALLED FILLER AND DOUBLER IAW DC8 SRM 51-1-8.SDR ABXA9701120Skin · corrodedDURING C-CHECK, FUSELAGE SKIN WAS FOUND BULGED AT STA 400 LONGERON 34L. REMOVED CORRODED SKIN AND REPAIRED IAW DC8 SRM 53-4-1 AND ABX REA D853-19125MR.SDR ABXA9701103Longeron · corrodedDURING C-CHECK, FOUND CORROSION ON LONGERON 36L AT STA 450 TO 610. *S/D* REPAIRED IAW DC8 SRM 51-1-200 AND ABX REA D853-19137MR.SDR ABXA9701102Frame · corrodedCORROSION ON FRAME 12, LOWER LEG AT L30L. *S/D* REPAIRED IAW DC8 SRM 51-1-20A AND ABX REA D853-19476MR.
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