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 ABXA9701101Pressure Web · corrosionDURING C-CHECK, CORROSION FOUND ON PRESSURE PANEL WEB RUNNING UNDER FLOORBEAM, COCKPIT FLOOR FS 12.00. *S/D* REPAIRED IAW ABX REA D853-19472MR.SDR ABXA9701100Longeron · crackedDURING C-CHECK, FOUND LONGERON 35L, STA 500 TO 540 CRACKED. *S/D* REPAIRED IAW DC8 SRM 51-1-8 AND ABX REA 853-19130MR.SDR ABXA9701094Skin · corrodedDURING C-CHECK, FOUND CORROSION IN STUB-WING AT SPAR CAP ATTACH EDGE ON RIGHT HAND LEADING EDGE . *S/D* FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC8 SRM 51-1-8 AND ABX REA D823-19144MR.SDR IXXA9700087Plating · crackedDURING ROUTINE C-CHECK INSPECTION, A TWO INCH CRACK WAS FOUND ON THE RIGHT WING LEADING EDGE PLATING AT STATION XFS376.000. REPAIR ACCOMPLISHED STOP DRILLING ENDS OF THE CRACK, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRASDR IXXA9700096Bracket · crackedDURING ROUTING C-CHECK INSPECTION, FOUND THE RIGHT WING INBOARD CANOE FITTING HANGER BRACKET CRACKED. REPAIR ACCOMPLISHED REMOVAL OF BRACKET, FABRICATION AND INSTALLATION OF NEW BRACKET IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8 SRM 51-1-21, 51-1-0 ANDSDR IXXA9700100Bulkhead Bracket · crackedDURING ROUTINE C-CHECK INSPECTION, THE TOP AFT PRESSURE BULKHEAD SUPPORT BRACKET WAS FOUND CRACKED. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED BRACKET, FABRICATION AND INSTALLATION OF NEW BRACKET IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 51-1-21, 51-1-0 ANDSDR IXXA9700098Bulkhead Bracket · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND THE AFT PRESSURE BULKHEAD RIGHT SUPPORT BRACKET CRACKED ABOVE THE THIRD STIFFENER. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED BRACKET, FABRICATION AND INSTALLATION OF NEW BRACKET IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANYSDR IXXA9700097Bulkhead Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LEFT SUPPORT FITTING CRACKED ABOVE THE THIRD STIFFENER. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION OF NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SDR IXXA9700093Cap Clip · crackedDURING ROUTINE C-CHECK INSPECTION, THE LEFT WING LOWER OUTBOARD FILLET CAP CLIP WAS FOUND CRACKED AT STATION 69.5. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF NEW CAP CLIP IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8 SRM 5SDR ABXA9700970Diffuser Case · crackedNR 1 ENGINE LOW OIL PRESSURE LIGHT CAME ON IN CLIMBOUT. OIL TEMPERATURE 153 DEGREES, CSD TEMPERATURE 120 DEGREES. LIGHT WOULD NOT GO OUT WITH ENGINE AT IDLE. SHUT DOWN NR 1 ENGINE AT 2140. LUBED FUEL PUMP AT 0340. OIL PRESSURE 26 PSI IN FLIGHT AFTER SHUTDSDR IXXA9700090Bracket · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND MID SHIP ACCESSORY COMPARTMENT KEEL BEAM BRACKET WITH STRESS CORROSION CRACK AT FUSELAGE STATION 640. REPAIR ACCOMPLISHED REMOVAL OF THE BRACKET, FABRICATION AND INSTALLATION OF NEW BRACKET IN ACCORDANCE WITH DOUGLAS ASDR IXXA9700089Fitting · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON A SUPPORT FITTING AT FUSELAGE STATION 1200, LONGERON 32 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF THE FITTING, FABRICATION AND INSTALLATION OF A NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8SDR IXXA9700088Fitting · crackedDURING ROUTING C-CHECK INSPECTION, FOUND A CRACKED SUPPORT FITTING AT FUSELAGE STATION 1180, LONGERON 27 LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION OF A NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8 SRM 5SDR IXXA9700095Plating · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND ON THE FUSELAGE PLATING AT FUSELAGE STATION 1900, LONGERON 9 LEFT. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND EXTERNAL REPAIR DOUBLER IN ACCORDANSDR IXXA9700103Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, A LONGERON ATTACH FITTING WAS FOUND CRACKED AT FUSELAGE STATION 1260, LONGERON 34 LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION OF NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SDR IXXA9700092Web · crackedDURING ROUTINE C-CHECK INSPECTION, THE CENTER WING FUEL TANK OUTER SURFACE WEB WAS FOUND CRACKED ON THE LEFT SIDE OF KEEL BEAM AT FUSELAGE STATION 810. REPAIR ACCOMPLISHED FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRAFT COSDR IXXA9700091Angle · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND CENTER WING FUEL TANK SUPPORT ANGLE CRACKED AT FUSELAGE STATION 781, LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED ANGLE, FABRICATION AND INSTALLATION OF A NEW ANGLE IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DC-8 SRM SDR IXXA9700102Fitting · crackedDURING ROUTINE C CHECK INSPECTION, A LONGERON ATTACH FITTING WAS FOUND CRACKED AT FUSELAGE STATION 360, LONGERON 33 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION OF NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SSDR IXXA9700101Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE LEFT FLOORBEAM SUPPORT FITTINGS WERE FOUND CRACKED BETWEEN FUSELAGE STATION 180 AND 240. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTINGS, FABRICATION AND INSTALLATION OF NEW FITTINGS IN ACCORDANCE WITH DOUGLAS AIRCRAFT CSDR IXXA9700094Bulkhead Angle · crackedDURING ROUTING C-CHECK INSPECTION, A ONE INCH CRACK WAS FOUND ON THE AFT PRESSURE BULKHEAD CIRCUMFERENTIAL MOUNT ANGLE AT FUSELAGE STATION 1766, STIFFENER 3 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED ANGLE, FABRICATION AND INSTALLATION OF A NEW MOUNT ANGLESDR RRXA97085Generator · failedHAD ZNS ON NR 3 GENERATOR, RESET FIELD AS PER QRH. 5 MINUTES LATER GENERATOR TRIPPED AGAIN. RETURNED TO OAK AS PER OPS. RESET NR 3 BUS FAULT, RESET FAULT SW FOR LANDING. MAINTENANCE TRANSFERED TO DMI IAW MEL 24-1 CONTROL NUMBER 703260, CAT C NR 3 GENERATORSDR ABXA9700163Rib · crackedRIGHT WING LEADING EDGE AT STATION XFS 591.25 IS CRACKED AT AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8.SDR RRXA97069Engine · oil leakWHILE EN ROUTE, CAPTAIN CALLED INTO EWA DISPATCH STATING THAT HE SHUT DOWN NR 3 ENGINE DUE TO LOW OIL QUANTITY INDICATOR. AS A RESULT, IT WAS DECIDED TO DIVERT TO IAH, WHERE EWA MECHANICS ARE ON HAND TO ASSESS DAMAGE. PERFORMED PRECAUTIONARY SHUT DOWN ON NR SDR ARWA9702006Bolt · lack of lubeAFTER T/O AND GEAR RETRACTED, DOOR NOT LATCH LIGHT REMAINED ON. RAN CHECKLIST, NO HELP. RETURNED TO MIA. FOUND BROKEN WIRE AT LEFT LANDING GEAR DOOR SW AND FROZEN BOLT AT RT MAIN GEAR LATCH ASSY. REPAIRED WIRE IAW 20-50-0 AND CLEAN AND LUBRICATED BOLT IAW SDR ABXA9701115Skin · corrodedDURING C-CHECK, FOUND LEFT ELEVATOR TO HAVE CORRODED AND CRACKED SKIN. REPAIRED AND REPLACED SKIN IAW DC9 SRM.SDR ARWA9702003Egt Indicator · failedWHEN LEAVING FL 280 FOR FL 310, NR 2 EGT IND STAYED AT 500, EVEN AFTER REACHING FL 310 AND RETARDING THROTTLE. PRECAUTIONARY SHUTDOWN OF NR 2 ENG, TIME 09207, OIL PRESS AT 24 PSI WINDMILLING, CLEARED SHORT AT LOWER ATT JUNCTION BLOCK BY CLEANING JUNCTION BLOCSDR RRXA97024Trim Cylinder · failedAFTER TAKEOFF GDL, LOST HYDRAULIC FLUID, RETURNED TO GDL. *** CORRECTIVE ACTION *** REMOVED AND REPLACED LEFT MLG BOGIE TRIM CYLINDER HYDRAULIC HOSE. SERVICED HYDRAULIC SYSTEM, LEAK AND OPS CHECKS GOOD. CHECKED FILTERS FOR CONTAMINATION, NONE FOUND. RETURNSDR ABXA9700024Relief Valve · defectiveON DESCENT FROM FL 280 TO FL 230, NR 3 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED; 35 PSI INDICATED. AFTER RETARDING THROTTLE TO IDLE AND LEVELING OFF AT FL 230, PRESSURE DROPPED FURTHER TO 32 PSI. SECURED ENGINE, OIL TEMP 90 DEGREES CELSIUS, QTY 3.5 GALS. DSDR ABXA9700023Engine · failedON CLIMBOUT WITH MCT SET, ALL ENGINE INDICATIONS NORMAL. A POWER LOSS WAS OBSERVED ON NR 3 ENGINE, WITH THE FOLLOWING INDICATIONS; N1-22 PERCENT, N2-0 PERCENT, FUEL FLOW-'0', OIL QUANTITY-5 GALS, AND OIL TEMP 25 DEGREES AND COOLING DOWN. ENGINE WAS SECURED ATSDR IXXA9700005Uplatch Switch · unsecureON CLIMBOUT, GEAR DOORS NOT LATCHED LIGHT WOULD NOT EXTINGUISH ON GEAR RETRACTION. LANDING GEAR WAS CYCLED AND THE DOORS LIGHT EXTINGUSHED. AFTER LANDING TOL, MAINTENANCE FOUND AND SECURED THE RIGHT HAND MAIN LANDING GEAR DOOR UPLATCH SWITCH. MAINTENANCE ACSDR IXXA9700004Wire · brokenAFTER TAKEOFF, GEAR UNSAFE LIGHT REMAINED ON AFTER RETRACTION. FLIGHT CREW CYCLED GEAR, LIGHT EXTINGUSHED, GEAR UPLATCH CHECK WAS NORMAL. THE FLIGHT CONTINUED TO TOL WITH AN UNEVENTFUL LANDING. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT THE LEFT MAIN LSDR ARWA9701003Clamp · looseON CLIMBOUT, EXPERIENCED LOUD FLAPPING NOISE BELOW COCKPIT FLOOR, UNABLE TO MAINTAIN PRESSURIZATION. CLOSED RT FLOW CONTROL VALVE AND NOISE CEASED, STILL UNABLE TO MAINTAIN CABIN PRESSURE. RETURNED TO SJU WITHOUT INCIDENT. MECHANIC FOUND LOOSE CLAMP AT RT FSDR RRXA97003Fitting · pulled looseSHUTDOWN NR 2 ENGINE DUE TO LOSS OF OIL QUANTITY AND PRESSURE. WINDMILLED FOR 62 MIN WITH ZERO OIL PRESSURE. MAINTENANCE PREPPED AIRCRAFT FOR THREE ENGINE FERRY TO BDL FOR ENGINE REMOVAL. FOUND OIL FILTER HOUSING FITTING PULLED OUT OF HOUSING.SDR RRXA97001Connector · looseENGINE FIRE WARNING INTERMITTENTLY ON NR 2 ENGINE DURING CLIMBOUT. COMPLIED WITH EWA ENGINE FIRE OR DAMAGE CHECKLIST, SHUT ENGINE DOWN. MAINTENANCE FOUND LOWER FIRE LOOP CANNON PLUG LOOSE. CLEANED AND RESECURED CANNON PLUG, NO DEFECTS FOUND. NR 2 ENGINE FISDR ABXA9700048Connector · dirtyNR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON, OIL PRESSURE 50 PSI. RETARDED THROTTLE TO IDLE, LIGHT STAYED ON. SHUT DOWN ENGINE AT 1210 Z. WINDMILLED WITH 34 PSI OIL PRESSURE, 34 PERCENT N-1, 38 PERCENT N-2. VERIFIED LOW OIL PRESSURE LIGHT ON WITH OIL PRESSUSDR ARWA9612002Battery Pack · dischargedEMERGENCY LIGHTS DISARM SWITCH WILL NOT DISARM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, SYSTEM OPS CHECKED NORMAL IAW 33-50-00.SDR RRXA96176Panels · crackedFERRY FLIGHT, DUE TO HORIZONAL STABILIZER DAMAGE. FOUND 2 EACH HORIZONAL STABILIZER LOWER PANELS DAMAGED AT STA XE160 AND XE171. CUT OUT DAMAGED PANEL AND STRINGER, FABRICATED NEW PANEL SECTIONS AND SPLICED IN IAW DOUGLAS DWG SRO8550001-7041.SDR ABXA9600686Engine · failedNR 4 ENGINE OIL PRESSURE LIGHT ILLUMINATED AT CRUISE, FL 330. QUANTITY WENT TO ZERO, TEMPERATURE WENT OFF SCALE HIGH. PERFORMED ENGINE SECURING. REPLACED NR 4 ENGINE IAW J CARD 7002.SDR CKSA96403Frame · corrodedDURING C-1 CHECK INSPECTION, FOUND LOWER AREA OF FRAME STA 1600 CORRODED FROM LONGERON 35L TO LONGERON 34R. REMOVED CORRODED AREA AND INSTALLED ZEE FRAME REPAIR IAW DC8 SRM 53-2-0 FIGURE 2. INSTALLED FASTENER IAW DC8 SRM 51-1-20D AND 51-1-21 ALODINED AND PRISDR CKSA96402Seat Track · corrodedDURING C-1 CHECK INSPECTION, FOUND FS 980 TO 1140 LONGERON -3RT SEAT TRACK AND MOUNT CORRODED MARKED L-177. REMOVED AND REPLACED SEAT TRACK AND REPAIRED IAW DC8 SRM 53-2-3 FIGURE 14. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. CORROSION CARD NR 5590-0551. NON-SDR CKSA96401Angle · crackedDURING C-1 CHECK INSPECTION, FOUND LOWER WING CENTER SECTION STA 781.5 RBL 64 HAS CRACKED SUPPORT ANGLE MARKED M6. REPLACED SUPPORT ANGLE IAW DC8 SRM 53-2-0. CORROSION CARD NR 2000 TO 0551. NON-ROUTINE TASK CARD NR 90982.SDR CKSA96400Fitting · corrodedDURING C-1 CHECK INSPECTION, FOUND FS 1160 LONGERON 31 LT THROUGH LONGERON 32 LT BATHTUB FITTING CORRODED. REMOVED CORROSION, TREATED, PRIMED IAW SRM DC8 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARDSDR CKSA96399Fitting · crackedDURING C-1 CHECK INSPECTION, FOUND FS 1230 LONGERON 35R THROUGH LONGERON 36 BATHTUB FITTING CRACKED. INSTALLED FITTING AND INSTALLED HI-LOCK IAW SRM 51-1-20D. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 90967.SDR CKSA96398Web · corrodedDURING C-1 CHECK INSPECTION, FOUND INNER GRANULAR CORROSION ON FORMER WEB, FORWARD SIDE, BETWEEN STRINGER 32 AND STRINGER 33R AT STA 120 MARKED H36. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER REPAIR IAW DC8 SRM 53-2-0 FIGURE 2. PART FABSDR CKSA96397Shear Tie · corrodedDURING C-1 CHECK INSPECTIO, FOUND SHEAR TIE AT STA 1700 BETWEEN STRINGER 22L AND STRINGER 23L IS CORRODED. REMOVED CORRODED SHEAR TIE FABRICATED SHEAR TIE IAW SRM 51-1-4. INSTALLED NEW SHEAR TIE IAW SRM 51-1-20D AND SRM 51-1-21. CORROSION CARD NR 5590-0551.SDR CKSA96396Blkhd Stiffener · corrodedDURING C-1 CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD, WEB AND VERTICAL STIFFENER HAS INNER GRANULAR CORROSION AT RBL 22 AT FLOOR LINE. REPAIRED VERTICAL STIFENER IN ACCORDANCE WITH AIA DRAWING AIA/E/2443 AND REPORT NR 96 AIA 197 DATED 12-12-96 EA 96-348. SDR CKSA96395Skin · corrodedDURING C-1 CHECK INSPECTION, FOUND CORROSION AT FS 680 BETWEEN STRINGER 33 AND 32R. CUT OUT CORRODED AREA, INSTALLED REPAIR IAW AIA/E/2430 AND EA 96-348 REPORT 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 5590-0551. NON-ROUTINE TASK CARD NR 91681, LEVEL 2.SDR CKSA96394Skin · corrodedDURING C-1 CHECK INSPECTION, FOUND LEFT HAND WING LEADING EDGE UPPER SURFACE FROM STA XFS302 TO XFS424 CORROSION EXCEEDED ALLOWABLE LIMITS. REFERENCE M-40 NR 88619. REPAIRED LEFT HAND WING LEADING EDGE UPPER SURFACE IAW AIA/EA SKETCH NR 2418 AND DC-8 SRM REPSDR CKSA96393Longeron · crackedDURING C-1 CHECK INSPECTION, FOUND LONGERON 36 CRACKED AND CORRODED STA 240 TO STA 300. REPAIRED LONGERON 36 AT STA 240 THROUGH STA 300 IAW AIA SKETCH AIA/E/2438 DATED 12-09-96 EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 5590-0551. NON-SDR CKSA96392Shear Tie · corrodedDURING C-1 CHECK INSPECTION, FOUND FS 1040 LONGERON 34R THROUGH 35 LT FRAME SHEAR TIES CORRODED BEYOND ALLOWABLE LIMITS. REPAIRED FRAME SHEAR TIES FS 1040 IAW AIA DRAWING NR AIA/E/2431, EA 96-348 REPORT NR 96 AIA 197 DATED 12-12-96. CORROSION CARD NR 5590-05
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