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 2006Track · damagedPOST FLIGHT INSPECTION NR 2 THRUST REVERSER AND TRANSLATING RING DAMAGED.LOWER T/R TRACK STOP AND ATTACHING HARDWARE MISSING. DOUGLAS SERVICE BULLETIN 78-100 IDENTIFIES THIS PROBLEM.SDR ARWA20040401Bleed Valve · surgesON TAKEOFF ROLL NR 3 ENGINE EPR INDICATOR SUDDENLY INCREASED TO 2.02 UNITS AFTER ALL ENGINES HAD BEEN SPOOLED AND STABLE AND ALL POWER LEVERS ALIGNED. EGT ALSO INCREASED TO MAX TAKEOFF LIMITS. ABORTED TAKEOFF AT 80 KIAS AND REJECTED TAKEOFF CHECKLIST WAS ACCOSDR ABXA040116Engine · defectiveUPON INITIAL CLIMBOUT, NR 2 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. NR 2 ENGINE OIL PRESSURE WAS NOTED TO BE 28 PSI AND OIL QUANTITY DECREASING. SHUT DOWN ENGINE AT 0424Z. N1 AND N2 RPM'S NOTED: 22/35. ENGINE OIL PRESSURE IN CRUISE: 3 PSI. REPLACEDSDR ABXA040124Skin · corrodedAFT ACCESSORY INNER SKIN AT LONGERON 27 RIGHT, LONGERON 26 RIGHT, STA 1660 - 1680 WAS CORRODED. REPAIRED AREA IAW REA D853-4866MR.SDR ABXA040129Skin · corrodedMAIN CABIN CENTER WING BOX HAD CORROSION AT LEFT BUTT LINE 8, STA 850. REPAIRED AREA IAW REA D857-48869MR.SDR ABXA040119Longeron · crackedLONGERON 24 LEFT CRACKED, LOWER INNER FLANGE OF BOTTLE BOLT CAVITY. REPAIRED LONGERON 23 LEFT IAW DC-8 SRM 53-2-2 AND REA D853-48861MR.SDR ABXA040118Keelbeam · corrodedMID SHIP ACCESSORY COMPARTMENT, FS 640 - 660, L-36 KEEL BEEM EXTENSION CORRODED. REMOVED CORROSION IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR DOUBLER IAW ABX REA D853-48863MR, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8.SDR ABXA040125Frame · corrodedAFT LOWER CARGO STA 1140, ABOVE LONGERON 35 RIGHT, RIVNUT INSTALLED THROUGH PORTION OF FASTENER HEAD. REPAIRED AREA IAW REA D853-48864MR.SDR ABXA040126Fastener · wrong partATTACH ANGLE TO FLOOR SUPPORT CENTER WING BOX, RIGHT SIDE 857, ANGLE HAD IMPROPER FASTENER INSTALLED. REPAIRED AREA IAW REA D857-48854MR.SDR ABXA040128Fitting · crackedLONGERON 24 LEFT, STA 980, UPPER LIP CRACKED. REPAIRED AREA IAW REA D853-48872MR.SDR ABXA040123Spar Cap · crackedTOP SIDE OF CENTER WING BOX, STA 857, LEFT BUTT LINE 24, UPPER SPAR CAP HAD A 3 INCH CRACK. REPAIRED AREA IAW DC-8 SRM 51-1-24, 51-1-20D AND 31-3-1.SDR ABXA040122Web · corrodedMAIN CABIN FS 280 AND RIGHT CUSP HAD CORROSION. REPAIRED AREA IAW REA D853-48860MR.SDR ABXA040121Pressure Panel · corrodedRIGHT WHEEL WELL, CORROSION ON SPOILER CABLE BRACKET FOOT END AROUND ATTACH BOLTS, JUST ABOVE LONGERON 24, FS 920. REPAIRED AREA IAW DC-8 REA D853-48868MR.SDR ABXA040120Fitting · corrodedAIR CONDITION ACCESSORY COMPARTMENT AT STA 70, LONGERON 34 RIGHT TO LONGERON 35 RIGHT, BULKHEAD ATTACH FITTING CORRODED. REPAIRED CHORD AND LONGERON FITTING IAW DC-8 SRM 51-1-24, 53-2-5 AND 51-1-8.SDR ABXA040130Floorbeam · corrodedRIGHT PRESSURE DECK MAIN CABIN LOWER SIDE OF FLOORBEAMS AT STA 920 AND 940 ARE EXFOLIATED. REPAIRED AREA IAW REA D853-48871MR AND REA D853-48873MR.SDR ABXA040127Attach Angle · corrodedATTACH ANGLE TO UPPER PRESSURE DECK FLOOR FROM STA 960 - 980, 100 INCHES FROM RIGHT CUSP, HAD CORROSION. REPAIRED AREA IAW REA D853-48865MR.SDR 1982Wire · shortedNR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. PERFORMED PRECAUTIONARY SHUTDOWN NR 1 ENGINE AT 2245Z, OIL PRESSURE 45PSI,OIL TEMP 95 DEGREES C, WINDMILLING OIL PRESSURE 32 PSI.SDR ARWA20040301Fitting · crackedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; NR 3 PYLON STATION YN 300 APPROX. FOOT STOOL FITTING LEFT SIDE WITH CRACK. REMOVED AND REPLACED FOOT STOOL FITTING FROM NR 3 PYLON IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-000084, DATED 22-MAR-04, DOUGLASSDR ABXA040111Fuel Control · defectiveNR 4 ENGINE, AFTER SETTING POWER FOR CRUISE, NR 4 ENGINE ROLLED BACK .15 EPR. EGT, FUEL FLOW N1 AND N2 ALL DROPPED. THROTTLE DID NOT MOVE. REPLACED NR 4 ENGINE FUEL CONTROL UNIT IAW 73-20-01. REPLACED NR 4 LOW PRESSURE FUEL FILTER. PERFORMED LEAK CHECK OFSDR ABXA040110Bleed Valve · defectiveAFTER TAKEOFF 2000 FEET, HEARD SHARP LOUD BANG/POP. NR 2 EPR DROPPED .18 AND BACK. FELT SLIGHT LEFT YAW. REPLACED NR 2 ENGINE COMPRESSOR BLEED VALVE AND CONTROL IAW 75-30-03-2-0002. NR 2 ENGINE LOW PRESSURE BLEED VALVE CHECKED GOOD IAW DC8 AMM 71-00-00. RSDR ABXA040096Crank Assy · brokenSPOILER EXTEND LIGHT STAYED ON AFTER RETRACTION. NORMAL SPOILER HYDRAULIC PRESSURE INDICATION. MAINTENANCE FOUND RIGHT WING INBOARD TWO SPOILER DRIVE ARMS THAT ATTACH TO SPOILER CABLES BROKEN. REPLACED REAR SPAR ACTUATOR CRANK ASSEMBLIES ON INBOARD SPOILER SDR ABXA040107Actuator · bypassingON CLIMBOUT, THE AIRCRAFT EXPERIENCED A VIOLENT LATERAL FLUTTER. THE AUTOPILOT WAS OFF, YAW DAMPER ENGAGED. THE YAW DAMPER WAS DISENGAGED BY PILOT WITH NO NOTEABLE DIFFERENCE. DEPOWERED THE RUDDER HYDRAULICS AND THE FLUTTER STOPPED. FURTHER TROUBLESHOOTINGSDR 1965Crank Assy · fracturedFLIGHT CREW REPORTED WING SLOT LIGHT ON WITH FLAPS EXTENDED. FOUND RIGHT AHND EXTENDED LEADING OOUTBOARD SLOT DOOR INOPERATIVE DUE TO FRACTURED AND BROKEN CRANK ASSEMBLY AT STA.XS476SDR 0378Frame · crackedDURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT FORWARD FRAME FITTING CRACKED AT FS299 BETWEEN LONGERON 32R AND 33R.SDR 0377Doubler · crackedDURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT INTERIOR SKIN DOUBLER CORRODED AND CRACKED AT FS270 LONGERON 31L AND IDENTIFIED AS LEVEL 2 CORROSION.SDR 0375Frame · corrodedDURING CPCP TASK 5570-0551 FORWARD LOWER CARGO COMPARTMENT CIRCUMFERENTIAL FRAME LOWER LEG CORRODED AT FS 80 BETWEEN LONGERON 36R AND 35R AND IDENTIFIED AS LEVEL 2 CORROSION.SDR 0370Fitting · crackedDURING CPCP TASK 5590-0551 AFT CARGO FS 1160 LONGERON 35R AND 34R FITTING CRACKED AND IDENTIFIED AS LEVEL 2 CORROSION.SDR 0369Clip · crackedDURING CPCP TASK 5690-0551 AFT CARGO FS 1210 LONGERON 33R CORRODED AND CRACKED 2 EACH FITTING CLIPS AND INDENTIFED AS LEVEL 2 CORROSIONSDR 0355Skin · corrodedDURING CPCP TASK 5600-0551 FOUND AFT ACCESSORY COMPARTMENT FS 1640 BETWEEN LONGERON 32R AND 33R. FASTENERS PULLING THROUGH FUSELAGE SKIN AND IDENTIFIED AS LEVEL 2 CORROSION.SDR 0354Duct · delaminatedNR 2 ENGINE LT ENGINE COWL TRANSITION DUCT DELAMINATED ON INBOARD SIDE.SDR 0479Fitting · crackedDURING FUEL TANK MAINTENANCE DETECTED LT WING NR 2 MAIN FUEL TANK CRACKED STRINGER END FITTING AT STA.XRS 78,S61.SDR 0390Hinge Fitting · crackedVISUALLY DETECTED LT OB AILERON CENTER HINGE FITTING CRACKED.SDR 0380Skin · crackedVISUALLY DETECTED CRACK IN PREVIOUS DOUBLER LEFT WING LEADING EDGE AT NR 2 ENGINE PYLON CUTOUT.SDR 0324Fitting · corrodedEXTERNAL FUSELAGE SKIN HAS A BULGE AT FS 324 LONGERON 33R FOUND DURING C-CHECK. FOUND FORWARD LOWER BELLY CARGO (A-PIT) DOOR STRUCTURE FITTING CORRODED.SDR 020104Fitting · corrodedEXTERNAL FUSELAGE SKIN HAS A BULGE AT FS 315 LONGERON 33R FOUND DURING C-CHECK. FOUND FORWARD LOWER BELLY CARGO (A PIT) DOOR STRUCTURE FITTING CORRODED-TASK CARD #0323.SDR ABXA040065Uplock · damagedGEAR UPLATCH CHECK FAILED. RIGHT MAIN LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED WITH LANDING GEAR RED UNSAFE LIGHT. IAS DID NOT EXCEED 230 KTS. DEFERRED MAIN LANDING GEAR DOOR UPLATCH SYSTEM IAW DC-8 MEL 32-14, CAT A, CODE 1. PLACARD INSTALLED. MUSTSDR 0471Longeron · corrodedDURING CPCP TASK NR 5570-0551 FORWARD LOWER CARGO COMPARTMENT CORROSION ON LONGERON 30L AT FS 270 AND IDENTIFIED AS LEVEL 2 CORROSION.SDR ABXA040064Seat · lack of lubeFIRST OFFICER'S SEAT INTERMITTENTLY SLIPPED OUT OF SELECTED FLOOR LATCHED POSITION. CLEANED AND LUBED FIRST OFFICER'S SEAT TRACKS. SYSTEM OPS CHECKED GOOD IAW DC-8 MM 28-11-01-2-0001.SDR ARWA20040202Web · corrodedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; FUSELAGE INTERIOR BETWEEN STA 1060.000 AND STA 1080.000 LT CUSP WITH CORROSION. ACCOMPLISHED REPAIR IN ACCORDANCE WITH BOEING ROD SKETCH 04-05-18-001. ISSUED FAA FORM 8110-3 APPROVING THIS REPAIR.SDR ARWA20040201Cargo Track · corrodedDURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; AFT LOWER CARGO COMPARTMENT BETWEEN STA 940.000 AND STA 1500.000, RBL 58.5 INCHES TRACK WR SECTION WITH CORROSION. REMOVED CORROSION IN ACCORDANCE WITH DC-8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IN ACCORDANCE SDR ABXA040039Link · looseUPLATCH CHECK FAILED ON INITIAL CHECK. GEAR WAS CYCLED THROUGH ONCE THEN UPLATCH CHECK WAS ACCOMPLISHED. UPLATCH CHECK WAS SATISFACTORY. FOUND LEFT MAIN LANDING GEAR LOWER SIDE BRACE LOWER LINK AND LOWER SIDE BRACE UPPER LINK WITH EXCESSIVE PLAY. REPLACE USDR ABXA040038Light · will not testEMERGENCY EXIT LIGHT, DISARM CHECK, WOULD NOT TEST. RELAMPED, OPS CHECKED NORMAL.SDR ARWA20040102Door Frame · crackedDURING AN A-CHECK INSPECTION, AFT LOWER CARGO COMPARTMENT AFT DOOR JAMB TOP FORWARD CORNER WITH CRACK STA 1440.000. TRIMMED OUT CRACK & FABRICATED FILLER, DOUBLER AND TRIPLER IAW DC8SRM 53-2-0, TR 53-188 AND SRM 51-1-21, 51-1-20D & 51-1-11.SDR ARWA20040104Keelbeam · crackedDURING A C-CHECK INSPECTION, THE FOLLOWING WAS FOUND; LT MAIN LANDING GEAR W/W STATION 920, KEELBEAM LT TEE EXTRUSION WITH 3 INCH CRACK. REPAIRED KEEL WEB STIFFENER AT STA 920 IN ACCORDANCE WITH BOEING MESSAGE INW-SCL-04-00005H, DATED 02 MARCH 04, DC8 SRM 51-2SDR ARWA20040101Skin · damagedDURING A-CHECK INSPECTION, THE FOLLOWING WAS FOUND, FUSELAGE EXTERIOR STA 1690 BETWEEN L-35R AND L-36 SKIN BROKEN, NEAR BUTT JOINT. PERFORMED REPAIR OF THE SKIN NEAR BUTT JOINT AT STA 1690, BTW LONGERON 35R & 36R IAW DC8SRM 53-2-1, FIG8, SHEET 1,2, PAGES 123/SDR ABXA040036Wire · burnedNR 3 GENERATOR UNPARALLED LIGHT ILLUMINATED IN FLIGHT, NO VOLTS, NO FREQS. RESET, NO VOLTS, NO FREQS, DISCONNECTED. REPLACED NR 3 ENGINE GENERATOR IAW 24-20-01-4-0002. DURING OPS CHECK, NOTED SPARKS COMING FROM THE TOP OF ENGINE. FOUND T1, T2, AND T3 WIRESSDR ARWA20031207Bulkhead · corrodedNR 970. DURING (C) CHECK INSPECTION, NLG WW RT TUNNEL STATION 8.000 PRESSURE BULKHEAD FORWARD FACE. NOSE LANDING GEAR RT FITTING WITH CORROSION AT L-31.SDR ARWA20031206Connector · damagedMASTER FIRE WARNING ILLUMINATED NR 2 FIRE SHUTOFF LEVER LIGHT ON, DISCHARGED BOTH FIRE BOTTLES. THREE ENGINE APPROACH AND LANDING WAS COMPLETED. DURING TROUBLESHOOTING FOUND NR 2 ENGINE FIRE WARNING CONNECTION P1-136 DAMAGE. REMOVED AND REPAIR CONNECTION IASDR ABXA030475Arm · wornRED GEAR UNSAFE LIGHT CAME ON AFTER GEAR RETRACTION WITH RT GEAR DOOR LIGHT ON FLIGHT ENGINEER'S PANEL. RECYCLED GEAR, ALL INDICATIONS NORMAL. MAINTENANCE FOUND DOOR ROLLER OUT OF ADJUSTMENT AND AFT ARM WORN. REPLACED ARM, ADJUSTED MAIN GEAR DOOR UPLATCH MESDR ABXA030474Proximity Sensor · dirtyLANDING GEAR UNSAFE LIGHT ILLUMINATED IN CRUISE. NOT LATCHED LIGHT ON FLIGHT ENGINEER'S PANEL ILLUMINATED WITH SELECTION RT GEAR POSITION. PERFORMED ABNORMAL. LIGHTS EXTINGUISHED WHEN LANDING GEAR WAS CYCLED. MAINTENANCE FOUND RT MAIN LANDING GEAR DOOR NOT
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