Douglas DC-8-62
Service difficulty reports · 2,778
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 = 'DC862' 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 = 'DC862' 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 96ZZZX2663Longeron · corrodedDURING C-CHECK, FOUND LONGERON 32L BETWEEN STATIONS 1530-1670 HAS LEVEL 2 CORROSION. REMOVED AND REPLACED LONGERON IAW SRM 51-1-21, ARM 51-1-8, AND SRM 51-1-20D.SDR 96ZZZX2662Stiffener · corrodedDURING C-CHECK FOUND AFT BULKHEAD WALL, FORWARD SIDE VERTICAL STIFFENER AT LBL 22 HAS CORROSION, BOTTOM END. REMOVED AND REPLACED CORRODED STIFFENER IAW SRM 51-1-21.SDR 96ZZZX2661Frame · corrodedDURING C-CHECK, FOUND CABIN WINDOW NR 25 LEFT, INNER FRAME SURFACE HAS CORROSION. REMOVED CORROSION AND REPAIRED IAW DRW SR 08530014. TREATED AND PRIMED AREA IAW SRM 51-1-8 AND REPLACED FASTENERS IAW 51-1-20D.SDR 96ZZZX2637Bulkhead · corrodedDURING C-CHECK, FOUND SKIN HAS CORROSION LEVEL 2 AT AFT BULKHEAD WALL FORWARD SIDE FLOOR LEVEL, RBL 7 INCHES AND RBL 15 INCHES. REPAIRED IAW DACO ACTION NR 291159.SDR 96ZZZX2636Skin · corrodedDURING C-CHECK, FOUND FORWARD LAVATORY WASTE DISPOSAL SERVICE AREA SKIN AROUND SERVICE NIPPLE WITH EXFOLIATION CORROSION. REMOVED INTERNAL PANEL. FABRICATED NEW INTERNAL PANEL PLATE IAW SRM 53-2-0. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED IAW SRM 51-1-SDR 96ZZZX2635Doubler · corrodedDURING C-CHECK, FOUND AIR CONDITIONING COMPARTMENT INTERNAL DOUBLER LOCATED BETWEEN FS 208 AND FS 270 AT L31R WITH A WIDE SPREAD. REMOVED INTERNAL DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW DAC DRAWING NR 5613862 AND SRM 51-1-21 AND SRM 51-1-20D.SDR 96ZZZX2634Bulkhead · crackedWEB IS CRACKED, AFT SIDE OF FLAT AFT PRESSURE BULKHEAD AT LONGERON 10R, INSTALLED DOUBLERS AND FILLER IAW SRM 53-2-5 AND SRM 51-1-20.SDR 96ZZZX2633Frame · corrodedDURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT AREA RT SIDE AT FRAME/STA 270 AND BETWEEN L28R AND L29R. FRAME HAS LOCAL CORROSION. FOUND CORROSION BEYOND LIMITS. CUT OUT CORRODED AREA, FABRICATED NEW FRAME SECTION AND EXTERNAL DOUBLER STRAP IAW SRM 52-2-5,SDR 96ZZZX2632Longeron · corrodedDURING C-CHECK, FOUND CORROSION LEVEL 2 AT LONGERON 27 RT BETWEEN FS 208.00 TO FS 270.00. REMOVED AND REPLACED LONGERON IAW 53-2-0, SRM 51-1-21, AND SRM 51-1-20D.SDR 96ZZZX2630Skin · corrodedDURING C-CHECK, FOUND VERTICAL FIN, RT FORWARD EDGE WITH CORROSION ON SKIN AND SCREWS. REMOVED DAMAGED AREA AND FABRICATED DOUBLER PER SRM 53-2-1. INSTALLED DOUBLER PER SRM 53-2-1. REF: OPERATOR CONTROL NR 0683.SDR 96ZZZX2629Skin · corrodedDURING C-CHECK, FOUND VERTICAL STABILIZER, L/E CORRODED AT APPROXIMATELY STA 179.750. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 55-2-1, TREATED AND PRIMED IAW 51-1-8. SEALED AREA IAW SRM 51-1-16. REF: OPERATOR CONTROL NR 1707.SDR 96ZZZX2628Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN BELOW FREON EXHAUST DOOR HAS WORKING FASTENERS, LT SIDE. REMOVED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, CLEANED CORROSION IN AREA, FOUND WITHIN LIMITS. TREATED AND PRIMED AREA AND INTERCOSTAL IAW SRM 51-1-8. INSTALLED RSDR 96ZZZX2627Doubler · corrodedDURING C-CHECK, FOUND DOUBLER AROUND DOOR NR 60 IS EXFOLIATED. REMOVED DOUBLER, FABRICATED NEW ONE IAW SRM 53-1-0 AND SRM 53-5-2, FIGURE 1. TREATED AND PRIMED IAW SRM 51-1-8 AND INSTALLED IAW SRM 51-1-21.SDR 96ZZZX2626Doubler · corrodedDURING C-CHECK FUSELAGE RT SIDE, STRUCTURAL DOUBLER HAS CORROSION AROUND IT, BETWEEN FS 188 TO FS 208 AND BETWEEN L24R AND L28R. REMOVED DOUBLER WITH CORROSION, FABRICATED NEW DOUBLER FROM 7075-T6 .065 INCH. TREATED AND PRIMED IAW SRM 51-1-8. INSTALLED DOUBSDR 96ZZZX2625Frame · corrodedDURING C-CHECK, FOUND FUSELAGE RT SIDE STRUCTURAL FRAME STA 270 HAS CORROSION FROM L21R TO L36R. INSTALLED NEW SECTION OF FRAME AT FS 270 FROM L21R TO L36R IAW SRM 53-2-5, FIGURE 8C-2, AND SRM 51-1-21, SRM 51-1-20D.SDR 96ZZZX2624Circumferential · corrodedDURING C-CHECK, FOUND CIRCUMFERENTIAL LEVEL 2 CORROSION. CUT OUT DAMAGED AREA FABRICATED FROM 7075T6. INSTALLED NEW SECTION IAW 53-2-5 AND 51-1-21, 51-3-0.SDR 96ZZZX2623Panel · corrodedITEM NR 1080. LEFT WING TOP TRAPEZOID PANEL CORRODED. FABRICATED AND INSTALLED NEW PANEL PER DER DRAWING A/R/W/ 950051-0203 AND SRM 51-1-20.SDR 96ZZZX2622Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN WITH CORROSION FUSELAGE STA 208.00 BETWEEN L29 AND L31. REMOVED CORROSION, REPAIRED IAW E.O. NR 961ALE.005D-7.SDR 96ZZZX2621Finger Doubler · corrodedDURING C-CHECK, FOUND CORROSION ON COCKPIT SUB-FLOOR BEAM FS 188.00 TO FS 208.00. REPAIRED IAW DER DRAWING 950087-0083, JOSSIAR, CO.SDR 96ZZZX2620Skin · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION AT AFT CARGO COMPARTMENT DOOR. REPAIRED IAW SRM 51-1-8, SRM 53-2-0, AND SRM 52-2-0.SDR 96ZZZX2619Longeron · corrodedDURING C-CHECK, FOUND CORROSION LEVEL 2 AT LONGERON 25 RT BETWEEN FS 208.00 AND FS 270.00. REMOVED AND REPLACED LONGERON IAW SRM 53-2-0, SRM 51-1-21, AND SRM 51-1-20D.SDR 96ZZZX2618Longeron · corrodedDURING C-CHECK, FOUND CORROSION LEVEL 2 AT LONGERON 26 RT BETWEEN FS 208.00 TO FS 270.00. REMOVED AND REPLACED LONGERON.SDR 96ZZZX2504Crank Assy · brokenFLAP CRANK ASSY IS BROKEN ON LUG AREA WHERE BOLT P/N NAS1105-23 GOES THROUGH. SUSPECT CAUSE, METAL FATIGUE AND CORROSION.SDR IXXA9665Angle · crackedDURING ROUTINE C-CHECK INSPECTION, THE VERTICAL STABILIZER FUSELAGE ATTACH ANGLE AT STATIONS 1626, 1640, AND 1667, WAS FOUND CRACKED. REPAIR OF THE CRACKED ANGLE WAS ACCOMPLISHED IAW DOUGLAS ROD SKETCH 96-04-02-005, WHICH IS FAA DER APPROVED. (X)SDR IXXA9664Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, LOCALIZED CORROSION WAS FOUND TO THE LEFT LEADING EDGE, STA XFS 195, UPPER ATTACH BOLT HOLES. REPAIR TO THE LEADING EDGE WAS ACCOMPLISHED IAW FAA DER APPROVED SKETCH A40-R04. (X)SDR IXXA9663Door Track · wornDURING ROUTINE C-CHECK INSPECTION, THE AFT LOWER FORWARD CARGO DOOR FORWARD GUIDE TRACK WAS FOUND WORN BEYOND LIMITS. REPAIR OF THE DOOR TRACK WAS ACCOMPLISHED IAW REPAIR SKETCH A40-R05 WHICH IS FAA DER APPROVED. (X)SDR IXXA9662Cover Plate · crackedDURING ROUTINE C-CHECK INSPECTION, FUEL PROBE ATTACH PLATES 9, 15, AND 17, OF THE LEFT WING WERE FOUND CRACKED. REPAIR OF THE ATTACH PLATES WAS ACCOMPLISHED IAW FAA DER APPROVED SKETCHES 96108-1, 96108-2, AND 96108-3.SDR IXXA9661Aux Spar Web · crackedDURING ROUTINE C-CHECK AND MLG ATTACH FITTING REPLACEMENT, THE LEFT AUXILIARY SPAR WEB WAS FOUND WITH LOCAL CORROSION AND CRACKS. THE WEB WAS REPLACED WITH A NEW WEB IAW DOUGLAS DRAWING 3641823-1. (X)SDR IXXA9654Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, KEEL BEAM SUPPORT FITTINGS AT FS 895 AND FS 902 WERE FOUND CRACKED. THE FITTINGS WERE REMOVED, FABRICATED, AND INSTALLED IAW AIRCRAFT SRM 53-1-0. (X)SDR IXXA9653T-Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE KEEL BEAM SUPPORT FITTING AT FS 950 WAS FOUND CRACKED. THE FITTING WAS REMOVED, FABRICATED AND INSTALLED IAW AIRCRAFT SRM 53-1-0. (X)SDR IXXA9652Plank · crackedDURING ROUTINE C-CHECK INSPECTION, THE NR 1 OUTBOARD PYLON REMOVABLE PLANK WAS FOUND CRACKED. THE PLANK WAS REMOVED, REPAIRED, AND REINSTALLED IAW AIRCRAFT SRM 54-2-2 AND SRM 5-1-21. (X)SDR ARWA9604002Trunnion · crackedDURING RIGHT MLG REMOVAL, FOUND CRACKS IN TRUNNION FITTING LUGS. REPLACED TRUNNION (P/N 5893930-508N) PER DC-8 S/B 57-94.SDR IXXA9660Longeron · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT LONGERON 24 WAS FOUND CRACKED BETWEEN FASTENER HOLES AT FS 920. REPAIR OF THE LONGERON WAS ACCOMPLISHED BY STOP DRILLING THE CRACK, FABRICATING AND INSTALLING REPAIR DOUBLER IAW AIRCRAFT SRM 53-2-2 AND SRM 51-1-21.SDR IXXA9658Rib · crackedDURING ROUTINE C-CHECK INSPECTION, THE NR 2 PYLON STUB WING UPPER CENTER RIB WAS FOUND CRACKED. REPAIR TO THE RIB WAS ACCOMPLISHED BY FABRICATING AND INSTALLING REPAIR DOUBLER AND ANGLE IAW THE AIRCRAFT SRM 57-2-0 AND SRM 51-1-20D. (X)SDR IXXA9657Rib · crackedDURING ROUTINE C-CHECK INSPECTION, THE NR 2 PYLON STUB WING, INBOARD RIB, FORWARD SECTION, WAS FOUND WITH 2 CRACKS. THE RIB ASSEMBLY WAS REMOVED AND REPLACED IAW THE AIRCRAFT SRM 51-2-0. (X)SDR IXXA9656Longeron · crackedDURING ROUTINE C-CHECK INSPECTION, LONGERON 24 LEFT WAS FOUND CRACKED BETWEEN FASTENER HOLES AT FS 920. THE CRACK WAS STOP DRILLED. REPAIR WAS ACCOMPLISHED BY FABRICATING AND INSTALLING REPAIR DOUBLER IAW THE AIRCRAFT SRM 53-2-2 AND SRM 51-1-21. (X)SDR IXXA9655Aux Spar Web · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT AUXILIARY SPAR WEB AT APPROXIMATE WS XW 97 WAS FOUND WITH LOCAL CORROSION. THE CORROSION WAS REMOVED, TREATED, AND PROTECTED IAW AIRCRAFT SRM 51-1-8. (X)SDR IXXA9649O-Ring · failedKLCK/TJSJ - EN ROUTE, ALL MAIN HYDRAULIC SYSTEM QUANTITIES DROPPED TO THE STANDPIPE LEVEL. AN UNEVENTFUL LANDING WAS ACCOMPLISHED AT TJSJ, AND THE AIRCRAFT WAS TOWED BACK TO THE RAMP. INSPECTION OF THE AIRCRAFT REVEALED AN O-RING HAD BLOWN ON THE SLOT CONTROSDR IXXA9667Hinge Flange · bentDURING ROUTINE C-CHECK INSPECTION, THE LEFT ELEVATOR, NR 4 HINGE FLANGE WAS FOUND BENT. THE DAMAGED AREA WAS REMOVED IAW THE AIRCRAFT SERVICE REPAIR MANUAL. (X)SDR IXXA9648Turbocompressor · malfunctionedRJTY/RJOI - EN ROUTE BETWEEN RJTY AND RJOI, NR 1 CABIN TURBOCOMPRESSOR BECAME NOISY AND PRODUCED AN OILY SMELL. THE NR 12 TC WAS SHUT OFF, AND WAS DEFERRED AT RJOI. THE NR 12 TC WAS SCHEDULED FOR REPLACEMENT DUE TO POSSIBLE BEARING/OIL SEAL FAILURE. (X)SDR IXAA9666Longeron · corrodedDURING ROUTINE C-CHECK, LONGERON 35 RIGHT WAS FOUND WITH CORROSION, CORROSION REMOVAL WAS BEYOND SRM LIMITS. THE AFFECTED SECTION OF LONGERON WAS REMOVED, FABRICATED, AND INSTALLED IAW AIRCRAFT SRM 51-1-8 AND SRM 53-2-3. (X)SDR IXXA9669Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, LOCALIZED CORROSION OF THE FUSELAGE PLATING, AT FS 1620, LONGERON 5 LEFT, WAS FOUND. THE CORROSION WAS REMOVED, REPAIR DOUBLERS FABRICATED AND INSTALLED IAW THE AIRCRAFT SRM 51-1-8 AND SRM 53-2-1. (X)SDR IXXA9668Le Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, LOCALIZED CORROSION WAS FOUND ON THE VERTICAL STABILIZER LEADING EDGE. DAMAGE WAS AT STA ZFS 173, RIGHT, ATTACHMENT SCREW HOLE. THE CORROSION WAS REMOVED, REPAIR DOUBLERS FABRICATED AND INSTALLED IAW WITH THE AIRCRAFT SRM 5SDR ABXA9600448Fire Warning · malfunctionedDURING CRUISE, NR 2 ENGINE FIRE WARNING LIGHT AND BELL CAME ON INTERMITTENTLY AND THEN WOULD NOT TEST. NR 2 ENGINE SCAN REVEALED NO VISUAL CONFIRMATION OF FIRE. SHUTDOWN THE NR 2 ENGINE AND THEN FIRE WARNING TESTED OK. NR 2 ENGINE MAINTAINED 25 PSI OF OIL PSDR IXXA9659Plating · corrodedDURING ROUTINE C-CHECK INSPECTION, EXTERNAL CORROSION OF THE FUSEAGE SKIN WAS FOUND. DAMAGE LOCATED BETWEEN FS 1500 AND FS 1530 AT LONGERON 1. REPAIR WAS ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF REPAIR DOUBLER. REPAIR WAS ACCOMPLISHSDR IXXA9640Bolt · brokenON TAKEOFF OUT OF PHIK, AFTER LANDING GEAR RETRACTION, BOTH THE MLG DOOR NOT LATCHED LIGHT AND THE GEAR NOT LATCHED LIGHT STAYED ON. AFTER SEVERAL GEAR CYCLES, THE GEAR UPLATCHED. THE AIRCRAFT RETURNED TO PHIK, WHERE MAINTENANCE INSPECTED THE LANDING GEAR ANSDR ARWA9603009Oil Press Light · flickeredON DESCENT, NR 4 ENGINE OIL PRESSURE LIGHT FLICKERED, OIL PRESSURE FLUCTUATED, OIL QUANTITY WENT DOWN TO ZERO. SHUTDOWN AND SECURED ENGINE. WINDMILLING PRESSURE 14 PSI FOR 17 MINUTES. UPON ARRIVAL CHECKED OIL QUANTITY, INDICATOR READS 5 GALLONS, CHECKED OILSDR ABXA9600372Hinge · chafedDURING C-CHECK INSPECTION, DISCOVERED RIGHT HAND INBOARD FLAP HINGE, INBOARD ARM CHAFED. REPAIRED RIGHT HAND INBOARD FLAP HINGE FITTING IAW ABX REA D857-13609MR.SDR ABXA9600371Jamb · crackedDURING C-CHECK INSPECTION, DISCOVERED AFT CARGO COMPARTMENT, AFT DOOR CUTOUT SKIN HAS A VISIBLE .25 INCH CRACK FROM EDGE TO FASTENER HOLE JUST ABOVE SKIN RADIUS AT LOWER FORWARD CORNER. FABRICATED C-4 DOOR JAMB PAN SPLICE AT AFT DOOR CUTOUT SKIN IAW ABX REA DSDR ABXA9600370Jamb · crackedDURING C-CHECK INSPECTION, DISCOVERED THE FUSELAGE SKIN CRACKED APPROXIMATELY 1.5 INCHES AT FUSELAGE STATION 560, LONGERON 33R, C-2 DOOR JAMB. FABRICATED C-2 DOOR JAMB WEB AT FUSELAGE STATION 560 AND LONGERON 33R IAW ABX REA D853-13607MR.
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