Douglas DC-10-30F
Service difficulty reports · 1,152
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 = 'DC1030F' 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 = 'DC1030F' 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 SCNA96115Battery Pack · dischargedEMERGENCY LIGHT FAILED TO TEST. REPLACED EMERGENCY BATTERY PACK, OPS TEST NORMAL.SDR 96FDEA00942Flap Track · grooveSNRM 6030, RT I/B FLAP I/B TRACK VERTICAL FACE UPPER AND LWR BEARING SURFACES DAMAGED WITH GROOVES AND GOUGED METAL APPROX .020 INCHES DEEP DUE TO I/B FLAP CARRIAGE SIDE LOAD BEARING FAILURE. *S/D REMOVED AND REPLACED RT I/B FLAP TRACK PER GMM 57-52-01, ISDR 96FDEA00941Thrust Link · looseSNRM 4361, NR 3 PYLON FWD ENG MOUNT AREA LOWER THRUST LINK LT SIDE OF PYLON HORIZONTAL ROW OF .3125 BOLTS ARE LOOSE, AS VIEWED FWD LOWER LT SIDE OF PYLON AT APPROX YN222 TO 226, 3 BOLTS LOOSE. *S/D* REPLACED NUTS WITH NEW AND RETORQUED PER EO 8-5410-7-4319.SDR 96FDEA00940Thrust Link · looseSNRM 4360, NR 3 PYLON FWD ENG MOUNT, LWR THRUST LINK RT SIDE OF PYLON HAS VERTICAL ROW OF .25 BOLTS AND HORIZONTAL ROW OF .3125 IN BOLTS LOOSE, TOTAL OF 18 BOLTS LOOSE AT APPROX PYLON STA YN 222 TO 226. *S/D* REPLACED NUTS WITH NEW AND RETORQUED PER EO 8-541SDR 96FDEA00939Thrust Links · looseSNRM 4359, NR 3 PYLON FWD ENG MOUNT LOWER THRUST LINKS, 7 MOUNTING BOLTS ARE LOOSE ON PYLON BOTTOM LT AND RT SIDES APPROXIMATE PYLON STA YN 222. *S/D* RT SIDE TORQUED PER MM 20-50-02, REMOVED AND REPLACED NUTS ON BOTTOM OF FWD THRUST LINK LT AND RT AND RETORSDR 96FDEA00935Screws · looseSNRM 4342, NR 3 PYLON HAD 8 TRI-WING SCREWS LOOSE ON PYLON AFT MOUNT BULKHEAD, STA YN420 RT SIDE OF PYLON.SDR 96FDEA00934Screws · looseSNRM 4343, NR 3 PYLON HAD 5 TRI-WING SCREWS LOOSE ON LT SIDE OF PYLON AT AFT MOUNT BULKHEAD, STA YN 420.SDR 96FDEA00933Bolt · shearedSNRM 4126. NR 1 PYLON FORWARD ENGINE MOUNT TRUSS FITTINGS HAVE NUMEROUS LOOSE BOLTS AT BOTTOM, TOP, AND SIDES. APPROXIMATELY 50 PERCENT OF THE FASTENERS ARE LOOSE. ONE BOLT IN THE BOTTOM RIGHT IS SHEARED. YN222 STA. S/D: TORQUED BOLTS PER E.O. 8-5410-7-4SDR 96FDEA00848Reverser Half · missingNR 2 THRUST REVERSER UNLOCK LIGHT ILLUMINATED AFTER LANDING AT ISD. FOUND NR 2 LT TRANSLATING SLEEVE MISSING FROM A/C. TRANSLATING SLEEVE WAS FOUND ON RUNWAY AFTER A/C LANDED. REPLACED NR 2 LT ENGINE THRUST REVERSER ASSY, AS PER WORK CARD NR 78T3101 AND 78TSDR 96FDEA00802Ground Prox Box · defectiveALL FOUR GEAR LIGHTS ILLUM WITH HANDLE UP, NO OTHER WARNINGS. RECYCLED GEAR IAW RED TAB PROCEDURES, GOT 4 GREEN ON BOTH PANELS WITH GEAR EXTENDED. AFTER THE GEAR WAS RETRACTED, THE FOUR RED LIGHTS REILLUMINATED, NO HORN. REMOVED AND REPLACED GROUND PROX BOXSDR 96FDEA00757Selector · malfunctionedLANDING GEAR WON'T COME DOWN, CYCLED GEAR AND STILL NO GEAR DOWN. USED ALTERNATE GEAR HANDLE AND GEAR CAME DOWN AND LOCKED. PRESS OK, QTY OK. REPLACED CENTER GEAR CONTROL VALVE AS PER MM 32-31-04. REPLACED L/GEAR SELECTOR VALVE AS PER MM 32-31-03. PERFORMSDR 96FDEA00730Cylinder · failedLOST SYS 3 HYD AFTER LANDING, MADE TURN ON TO TAXIWAY LOST ALL FLUID CONFIRMED EXTERNAL LEAK FROM A/C ON GROUND. REMOVED AND REPLACED NOSEWHEEL STEERING CYLINDER PER MM 32-52-01. RESERVICED NR 3 HYDRO SYS TO FULL, ALL SYSTEMS CHECK GOOD.SDR SCNA96036Aoa · failedSTALL WARNING ACTIVATED AFTER TAKEOFF, AIRCRAFT RETURNED TO BLOCK. REMOVED AND REPLACED ANGLE OF ATTACK SENSOR.SDR WRLA96013Adi · failedIMMEDIATELY AFTER TAKEOFF DURING INITIAL CLIMB, FLIGHT CREW NOTED CAPTAIN ATTITUDE DIRECTIONAL INDICATOR (ADI) FAILED (ATTITUDE FLAG IN VIEW). FLIGHT CREW ELECTED TO RETURN TO THE POINT OF DEPARTURE. FUEL WAS DUMPED TO BRING ACFT BELOW MAXIMUM LANDING. AIRCSDR WRLA96011Smoke Detector · damagedDURING TAKEOFF, FLIGHT CREW HEARD A LOUD NOISE (BANG) COMING FROM UPPER DECK CARGO AREA. FLIGHT CREW ELECTED TO DISCONTINUE TAKEOFF (MAX SPEED ATTAINED 120 KNOTS). AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. UPON INSPECTION, MAINTENANCE PERSONNEL FOSDR 95UAL900293Pneu Manifold · fail indicationNR 2 MANIFOLD INDICATION FAILURE. THE TRIP WAS CANCELED.SDR 95FDEA01535Prox Sensor · defectiveLT MAIN IND UNSAFE, BOTH PANELS WITH GEAR HANDLE UP. INITIALLY GEAR WENT UP SAFE, BUT AFTER ABOUT 5 SECONDS THE RED LIGHT CAME BACK ON, THIS OCCURRED ON TWO OCCASIONS. FOUND LT/MLG DOWN LOCK SENSOR WIRES DEFECTIVE. REMOVED AND REPLACED POSITION PROXIMITY SESDR 95FDEA01476Door · crackedCENTER LINE GEAR R/DOOR IS CRACKED AT FWD LOWER I/B FRAME. REMOVED AND REPLACED FRAME PER SRM 51-00-00 VOL 1 PAR 2 SEC C.SDR 95FDEA01475Gear Door · crackedCENTER LINE GEAR L/DOOR IS CRACKED AT FWD LOWER I/B FRAME. REMOVED AND REPLACED ANGLE PER SRM 51-00-00 VOL 1 PAR 2 SEC 3.SDR 95FDEA01457Skin · crackedRIGHT HORIZONTAL STABILIZER, UPPER AFT SKIN PANEL CRACKED AT I/B AFT CORNER O/B OF THE OPERATION BULKHEAD, CRACK LENGTH .6250 INCH. REPAIRED UPPER AFT SKIN STAB PANEL PER EA NR 8-5510-25166. INSTALLED AND SEALED ALL ACCESS AND L/E PANELS AS REQ IAW MM 55-10-SDR 95FDEA01428Duct · failedDURING T/O ROLL, NR 1 ENG N1 IND DROPPED APPROX 10 PERCENT. ADJUSTED THROTTLE TO MATCH N2 AND FUEL FLOW, NO CHANGE NOTED IN N1, EGT IND 910 DEGREES, APPROX 50 DEGREES HIGHER THAN ENG NR 2 AND NR 3. AT APPROX 300 FEET NR 1 FIRE WARNING AND BELL RECEIVED. ACSDR 95FDEA01364Fitting · crackedRT I/B FLAP I/B ACTUATOR ATTACHMENT TO FUSELAGE BOLTS NOT SECURED. CHECKED BARREL NUTS FOR WEAR, FOUND ACT LOWER ATTACH FITTING CRACKED AT LOWER BOLT HOLES.SDR 95FDEA01363Arm · crackedUPON DISASSEMBLY OF CONTROLS, ARM AP NR 7202-5 WAS FOUND CRACKED AT SPLINE SHAFT MOUNT END. CRACK ORIGINATED IN CLAMP UP BOLT PLANE AND FOLLOWS GRAIN OF PART LENGTH. THIS CONDITION FOUND ON 2 OF ARMS FROM THIS A/C AND THE ARMS WERE REPLACED.SDR 95FDEA01334Spar · corrodedNR 1 PYLON UPPER SPAR RT CHORD, AFT 16, HAS RUST ON TOP OF HORIZONTAL FLANGE AND INBOARD SIDE OF TOP VERTICAL FLANGE. CLEANED AND TREATED CORROSION PER SRM 51-21-01, PAGE 36.SDR 95FDEA01393Spar Web · crackedNR 1 ENG PYLON UPPER SPAR WEB CRACKED AT OUTBOARD CORNER (APPROX 5). REMOVED AND REPLACED SPAR WEB. REPAIRED PER EA 8-5410-20129. REPLACED NR 1 PYLON AFT BULKHEAD FITTING AND REPAIRED UPPER WEB. SEE EA FOR DETAILS.SDR 95FDEA01311Spar Web · crackedNR 1 ENG PYLON UPPER SPAR WEB CRACKED AT O/B CORNER, APPROX 5 INCHES. REMOVED AND REPLACED SPAR WEB.SDR 95FDEA1392Bulkhead · crackedNR 1 PYLON AFT SPHERICAL BEARING SUPPORT BULKHEAD, YN 417.212, HAS A 10 INCH CRACK AT INBOARD INSIDE RADIUS. CRACK WAS DISCOVERED BY AN INSPECTOR WHILE PERFORMING THE SB 54-74 INSPECTION. THE NR 3 PYLON WAS ALSO INSPECTED AND NO CRACKING WAS EVIDENT. CRACK SDR 95FDEA01274Bulkhead · crackedNR 1 PYLON AFT SPHERICAL BEARING SUPPORT BULKHEAD YN 417.212, HAS A 10 INCH CRACK AT I/B INSIDE RADIUS. CRACK WAS DISCOVERED BY AN INSPECTOR WHILE PERFORMING THE SB 54-74 INSPECTIOIN. THE NR 3 PYLON WAS INSPECTED AND NO CRACKING WAS EVIDENT. CRACK APPEARS TSDR 95FDEA01281Skin · lightning strikeLIGHTNING STRIKE, TOP OF UPPER RUDDER TAB RT SIDE, APPROX .25 INCH HOLE BURNED THROUGH ALUMINUM SKIN. FABRICATED DOUBLER PER SRM 55-00-01, WEIGHT CHANGE PLUS 1.502. RESTAMPED PLACARD TO ACTUAL WT OF RUDDER AS REQ SRM 55-40-02, PRIMED AND PAINTED PER SRM 51-2SDR 95FDEA01280Fitting · looseRT WING O/B FLAP I/B SUPPORT FITTING TO REAR SPAR IS SUSPECTED LOOSE, MEASURED GAP 0.003. REMOVED O/B FLAP AND INSPECTED SUPT FITTING HOLES FOR CRACKS, NO DEFECTS NOTED. INSTALLED NEW STUDS AND PLI WASHERS AS PER MM 20-20-01 PG 202. REINSTALLED FLAP, FITTINSDR 95FDEA01279Fitting · wornRT DETACHABLE ELEVATOR'S BAYONET LATCHES ARE LOOSE, WORN FITTINGS C/W S/B 55-9 AND EA NR 8-5520-25164. REPLACED FITTINGS AND LATCHES, OPENED AND CLOSED SKIN AND SEAL EDGES. ELEV OPS CHECK OK.SDR 95FDEA01278Fitting · wornLT DETACHABLE ELEVATOR, AFT BAYONET LATCH ASSY LOOSE IN FITTING, WORN C/W SB 55-9 AND EA NR 8-5520-25165. OPEN SKIN, REPLACED FITTINGS AND LATCHES. SKIN AND PANELS OPS CHECK OK.SDR 95FDEA01277Frame · crackedLT CENTER GEAR DOOR, 2 INCH CRACK AT FWD I/B FRAME. REMOVED AND REPLACED DAMAGED FRAME AS PER SRM 51-00-00 PG 2 ITEM C.SDR 95FDEA01276Frame · crackedRT CENTER GEAR DOOR, 2 INCH CRACK AT FWD I/B FRAME. REMOVED AND REPLACED DAMAGED FRAME AS PER SRM 51-00-00 PG 2 ITEM C.SDR 95FDEA01195Fitting · corrodedINSIDE AFT CARGO COMPT - FWD LOWER CORNER OF DOOR SILL - LONGERON 41 - END FITTING AT STA 1790 IS CORRODED - LEVEL 2. INSTALLED NEW FITTING.SDR 95FDEA01194Angle · corrodedINSIDE AFT CARGO COMPT STA 1795-1835, LONGERON 44L, NESTING ANGLE AND ATTACHING WEB TO CARGO DOOR LOWER TORQUE BOX HAS CORROSION - LEVEL 2. REMOVED AND REPLACED NESTING ANGLE AND ATTACH WEB.SDR 95FDEA01186Longeron · corrosionRUSTY FASTENERS IN LWR CENTER CARGO COMPT UNDER FLOOR SPACE AT FS 152-154L, LONGERONS 45-47L. REMOVED FASTENERS, BURNISHED OUT CORROSION, FABRICATED ANGLE AND INSTALLED IAW EO 8-5310-25134.SDR 95FDEA01189T Angle · crackedLEFT STAB L/E 2ND RIB, REMOVED SECTION O/B WEB UPPER T-CHORD IS CRACKED ON INSIDE. REMOVED T-CHORD, INSTALLED NEW T-CHORD P/N ALC-7502-11, PER SRM 51-00-01.SDR 95FDEA01188T Angle · crackedRT STAB L/E 2ND RIB, O/B SECTION UPPER WEB T-CHORD IS CRACKED, ENTIRE LENGTH INSIDE. REMOVED T-ANGLE, INSTALLED NEW PART ALC7502-12, FEDEX SRM 51-00-01.SDR 95FDEA01187Bulkhead · corrodedWING CTR SECT FUEL TANK BLKHD STA 1156 HAS INTERGRANULAR CORROSION AT VERTICAL STIFFENER O/B OF OPENING PNL143CZ, FWD FACE, LWR AREA. REMOVED CORROSION FROM AFFECTED AREA IAW DC10 SRM 51-21-01. THICKNESS LIMIT CK'D OK. ALONDINED AND PAINTED AFFECTED AREA IASDR 95FDEA01190T-Chord · crackedLT/STAB L/E 2ND REMOVED SECTION O/B WEB LWR T-CHORD IS CRACKED ON INSIDE 6. STOP DRILLED CRACK, FABRICATED SHIMS AND REPAIRED ANGLE AS PER EA 8-5510-25132.SDR 95FDEA01192Bracket · crackedRIGHT WING O/B SLAT DRIVE OUTER BRACKET CRACKED, LOWER FWD FLANGE RADIUS. REMOVED AND REPLACED BRACKET WITH NEW BRACKET MODIFIED TO EO 8-2780-7-2319C SPEC. MM 27-83-02 (REF TO CONTROL ITEM 4, PART NR 4).SDR WRLA95029Tens Regulators · lack of lubeWHILE TAXIING OUT FROM GATE, CAPTAIN PERFORMED FLIGHT CONTROL CHECK. NR 5 SPOILER SEGMENT RIGHT WING WOULD NOT FULLY DEPLOY. CAPTAIN ELECTED TO RETURN TO GATE FOR MAINTENANCE. MAINTENANCE CLEANED AND LUBED TENSION REGULATORS AND CABLE RUNS. OPS CHECK OK. SDR WRLA95024Pitch Computer · failedUPON COMPLETION OF INITIAL CLIMB, NR 1 AUTOPILOT WOULD NOT CAPTURE DESIGNATED ALTITUDE. AUTOPILOT WOULD NOT HOLD SELECTED ALTITUDE OR SPEED. NR 2 AUTOPILOT ON DEFERRAL. CREW DIVERTED ACFT FOR T/S. FLT CREW USED ABNORMAL PROCEDURES & DUMPED 50,000 POUNDS OFSDR WRLA95021Pitch Computer · failedDURING INITIAL CLIMB, CREW NOTED NR 1 AUTOPILOT UNUSABLE (PITCHING VIOLENTLY). AS NR 2 AUTOPILOT WAS ALREADY ON DEFERRAL, CREW ELECTED TO RETURN TO DEPARTURE AIRPORT. CREW UTILIZED ABNORMAL PROCEDURES INCLUDING DUMPING OF FUEL TO BRING ACFT TO BELOW MAXIMUM SDR WRLA95019Connector · dirtyDURING TAKEOFF, AT 140KTS, CAPTAIN NOTED 'ENGINE FAILED' LIGHT ON. CAPTAIN ABORTED TAKEOFF, STOPPING AIRCRAFT NORMALLY WITH THRUST REVERSE AND BRAKING. AIRCRAFT TAXIED BACK TO GATE WITHOUT FURTHER INCIDENT. CREW DEBRIEFED WITH MAINTENANCE AND STATED THAT THSDR WRLA95018Sense Line · blockedDURING TAXI OUT, FLIGHT CREW NOTICED NR 1 N1 AT 16 PERCENT, NR 1 EGT AT 480 DEGREES, NR 1 N2 AT 48 PERCENT, AND FUEL FLOW WAS AT 1,000 LBS. THROTTLE MOVEMENT HAD NO EFFECT. CAPTAIN ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENSDR WRLA95016Connector · failedDURING TAXI, FLIGHT CREW PERFORMED FLIGHT CONTROL DEFLECTION CHECK, DID NOT GET FULL DEFLECTION OF SPOILERS. CREW ELECTED TO RETURN TO GATE FOR TROUBLESHOOTING/CORRECTION. ACFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. AFTER EXTENSIVE TROUBLESHOOTING, MAINSDR 95FDEA00214Fire Warning · malfunctionedTHE APU FIRE LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. IT ALSO ILLUMINATED DURING TAKEOFF OUT OF MEM. FOUND APU FIRE LIGHT ASSY RETAINER PIN MISALIGNED, REMOVED AND REPLACED LIGHT ASSY. OPS CKD GOOD.SDR WRLA95007Quick Disconnect · looseDURING CLIMB, CREW NOTICED THAT ALL CLOCKS STOPPED. INSPECTION OF BATTERY INDICATION BY THE FLIGHT CREW REVEALED NO VOLTS AND AMPS. THE PILOT IN COMMAND PULLED AND RESET BATTERY CHARGER CIRCUIT BREAKER AND VOLTS WENT TO 35 VOLTS AND NO AMPS, BUT THEN RETURNE
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