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 98FDEA00765Ins · inop98-312 - COULD NOT GET INS UNIT TO R-NAV UPDATE. GOT R-NAV YELLOW LIGHTS BUT WOULD NEVER GO TO GRN. UPDATED ALL 3 INS WITH SOFTWARE FX9813 PER MM 34-43-00-3. CKD SYS PER MM 34-43-00-1 ON GRD ALL CKD OK. OK TO CONT.SDR 98FDEA00760Skin · damagedON WALKAROUND FOUND LT NR 1 L/E SLAT INBD FAIRING MISSING. ALSO, DAMAGE TO L/E SLAT ASSY. *S/D* REPLACED NR 1 L/E SLAT (LT) ASSY WITH FAIRING PER MM 27-80-01-4.SDR 98FDEA00729Sensor · out of adjust98-296 - AFT GEAR RETRACT, LMLG REMAIN ILLUM RED. RECYCLE GEAR 3 TIMES LIGHT REMAIN ON. DID REPOSITION OF STOP SENSOR IN LT MAIN LAND GEAR UP AND DOOR LATCH SENSOR. READJUST CLEARANCE AT TARGET AND PROXIMITY SENSOR AND THEN PERF OPER CK OF L/G SWING AS PER SDR 98FDEA00715Control · inopNR 5 BRAKE TEMP 150 DEG, LEFT GEAR DOWN. REMOVED AND REPLACED NR 5 BRAKE ASSY TEMP SENSOR AND ANTISKID CONTROL UNIT, PERF BITE TEST.SDR 98FDEA00692Temp Gauge · inopNR 3 HYDRAULIC TEMP HAD SLOWLY INCREASED IN TEMP AFTER T/O. TEMP 108C, NO TEMP LIGHT, PRESS TO TEST WAS OK. REMOVED AND REPLACED HYDRAULIC GAUGE AFTER TROUBLESHOOTING, RAN SYS, OK FOR SERVICE MM 29-33-01.SDR 98ZZZX4188Transformer · failedDURING MAINTENANCE, AIRCRAFT POWER WAS SELECTED TO GROUND SERVICE OPERATION. LATER, DISCOVERED SMOKE IN COCKPIT AND SMELL OF ELECTRICAL BURNING. UPON TROUBLESHOOTING, FOUND SMELL OF ELECTRICAL BURNING COMING FROM E/E COMPARTMENT LEADING TO ONE OF THE TRANSFOSDR G60A028Valve · failedWHILE RETURNING TO ANC, UPON COMPLETION OF THE FUEL DUMP PROCEDURES, THE LEFT FUEL DUMP VALVE INDICATED A FAILURE TO CLOSE. GROUND MAINTENANCE REMOVED AND REPLACED THE GATE VALVE SHUTOFF ASSY IAW MM 28-30-02. OPERATIONAL CHECK NORMAL. (M)SDR G6OA028Valve · failedWHILE RETURNING TO ANC, UPON COMPLETION OF FUEL DUMP PROCEDURES, THE LEFT HAND FUEL DUMP VALVE INDICATED A FAILURE TO CLOSE. (X)SDR 98ZZZX3587Spar · corrodedRT WING UPPER SURFACE JUST INBOARD AND FORWARD OF NR 2 SPOILER HAS CORROSION THAT RUNS FROM (XORS 480) TO (XORS 492). REPAIR WAS C/W BY DOUGLAS PROVIDED E.A. NOTE: MAXIUM DEPTH OF CORROSION WAS .050 INCH.SDR 98FDEA00514Light · inoperativeIN CRUISE FLT LEVEL 370, AIR COND DOOR LIGHT ILLUM. CONSULT RED TABS, RETURNED TO ANC. DOOR LIGHT WENT OUT AT 6.5 PSI. BEG TO BLINK WHEN INCREASE PSI AT 7.0 PSI. A/C RELEASED PER MEL 52-4D. A/C COND DOOR CAUTION LIGHT INOP. C/W MSP 52-4C, DOORS ARE VERIFSDR G60A025Sensor · failedTHE L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST SWITCH WAS INOPERATIVE. THIS WAS DEFERRED IAW MEL 25-24. GROUND MAINTENANCE REMOVED AND REPLACED THE PRESSURE SENSE ASSY IAW MM 25-60-03. OPERATIONAL CHECK NORMAL. (M)SDR 98FDEA00455Flex Duct · tornSTA-ORD - UNABLE TO CONTROL CABIN PRESS IN ANY MODE. CABIN ALT CLIMB AT RATE EXCEED AUTO-SCHEDULE AND AT LEVEL OFF CONTINUE TO CLIMB AT 300 TO 400 FPM. UNABLE TO GAIN CONTROL USING STBY PRESS OR MANUAL PRESS PER RED TABS. CABIN ALT EXCEED 10000 AND EMERGENCSDR G6OA023Ecu · lightning strikeDURING CLIMB-OUT FROM CDG, THE FLIGHT CREW REPORTED LIGHTNING STRIKE. NR 1 ENGINE PARAMETERS WERE OUTSIDE THE NORMAL PARAMETERS. NR 1 ENGINE WAS SHUT DOWN, FUEL DUMPED IAW AOM VOL 1 AND RETURNED TO CDG. GROUND MAINTENANCE ACCOMPLISHED LIGHTNING STRIKE INSPESDR 98FDEA00429Hydraulic Sys · high temp98-0167 STA-DXB: DURING TAXI OUT HYD SYS NR 2 READ 50-50 DEG AFTER APPROX 8 MIN OF FLT TEMP NR 2 HAD INCREASE TO 60 DEG TMP SHORTLY INCREASE TO 70 DEG RED TABS REFER TO ND TEMP INCREASE WITHIN 5 MIN TO 90 CONT RED TAB PROC WITH NR 2 SYS SHUT DOWN. WHEN TMP ASDR 98FDEA00413Fire Bottle · dischargedENGINE NR 2, NR 1 BOTTLE LOW PRESSURE LIGHT ILLUMINATING JUST PRIOR TO DEPARTURE. FOUND NR 1 BOTTLE OF APU FIRE EXTINGUISHER SYSTEM HAD DISCHARGED THRU APU PORT (NR 2 ENG FIREX CONTAINER 1). REPLACED NR 2 ENG FIREX CONTAINER 1 PER M/M 26-21-02 AND SQUIB FOR SDR 98FDEA00394Angle · crackedUPPER VERTICAL FIN BASE ANGLE HAS CRACK INDICATION BETWEEN THE NR 4, 5 FASTENER HOLES FROM THE RT SIDE REF WC 8-553074303B1 - P1 EA 8-5530-3855 DATED 6/8/98 WRITTEN BASE ANGLE WILL BE REPETITIVE INSPECTED AT INTERVALS NOT TO EXCEED 1800 HRS. BASE ANGLE TO BE SDR 98FDEA00364Fire Loop · malfunctionedNR 1 ENG FIRE DETECT SYS LOOP-B LT ON IN FLT, RED TABS ACCOMPLISHED, CHECKED OK. APPROX 2 HRS LATER NR 1 ENG FIRE LIGHTS ON. ACCOMPLISHED RED TABS, EMERGENCY LANDING ABQ. LANDED OVERWEIGHT.SDR 98FDEA00344Hyd Fuse · blownGEAR HANDLE W/N COME UP AFTER T/O, STEERING HANDLE CENTERED, GROUND TENSION CHECKED OK ON TAT. PRESSED HANDLE RELEASE AND HANDLE STILL W/N COME UP. REMOVED AND REPLACED TRIM CYLINDER INTERLOCK FUSE, SYS OPS CK NORMAL PER MM 32-31-06-02.SDR 98FDEA00342Spar Cap · crackedFOUND .5 INCH CRACK IN UPPER REAR SPAR CAP OUTER SECTION SKIN PANEL (RIGHT HAND SIDE). REF: EO 8-5510-7-3310 PART 4. REPAIRED PER EA 8-5510-38504- HORIZONTAL STAB RT UPPER AFT SKIN PANEL REPAIR.SDR 98FDEA00341Bolt · looseSNRM N 00874, A/C 304, FOUND 9 EA BOLTS LOOSE AT BOTTOM OF PYLON FWD MOUNT. REMOVE, INSPECTED AND INSTALLED 9 EA BOLTS PER M/M 20-50-0212.SDR 98FDEA00266Warning Syst · malfunctionAFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. DISCOVERED 6 FT AFT CABIN DOOR OPEN APPROX 2.5 INCHES. DUMPED FUEL AND LANDED VCP WITHOUT INCIDENT. RESET DOOR PER M/M 52-10-01-2 ARMS OK. CHECKED FOR ELECTRICAL ANOMOLIES TO LOCK PIN RELEASE AND ACTUATOR. FOUSDR 98FDEA00257Gear Handle · lack of lubeLANDING GEAR HANDLE WAS PLACED IN DOWN POS. ALL 8 LANDING GEAR POSITION INDICATORS STAYED RED. RECYCLED LANDING GEAR HANDLE, NO HELP. RED TAB PROCEDURE FOLLOWED. ATL LANDING GEAR EXTENSION HANDLE WAS PULLED. ALL 8 GEAR POSITION INDICATORS WENT GREEN. CLESDR 98FDEA00250Slider · brokenSHORT FINAL, LEFT AFT CARGO DOOR LIGHT ON F/E PANEL ILLUM FOLLOWED BY IMMEDIATE PRESSURE DROP IN CABIN. ACFT WAS ALREADY CONFIGURED FOR LANDING, LANDED SUCCESSFULLY, NO FURTHER PROBLEMS. DOOR 4L SWITCH NOT WORKING DUE TO TRACK CAM AND SLIDER BROKEN. REPLACESDR 98FDEA00254Switch · failedLANDING GEAR HANDLE WAS PLACED DOWN, ALL INDICATORS REMAINED RED. LANDING GEAR HANDLE WAS CYCLED TWICE, NO JOY. ALTERNATE EXTENSION HANDLES WERE ACTUATED IN ACCORDANCE WITH ED TAB PROCEDURES. ALL INDICATORS WENT GREEN. REPEAT. INSTALLED GEAR PINS, REPLACESDR 98FDEA00249Control Unit · failedON FINAL LANDING GEAR CAME DOWN BUT NO GREEN GEAR LIGHT DOWN LIGHT. RECYCLED LANDING GEAR UP AND THAN DOWN AND THAN RECEIVED 4 GREEN LIGHTS. REMOVED AND REPLACED CONTROL UNIT PER M/M 32-61-01, BITE TEST GOOD.SDR 98FDEA00227Hose Assy · brokenAPPROXIMATELY 20 MIN INTO FLIGHT, NR 2 HYD QUANTITY AND PRESSURE WENT TO ZERO. ENGINE RAN APPROXIMATELY 55 MINUTES BEFORE SHUTING DOWN. T/S FOUND NR 2 ENG FIRE-RESISTANT HOSE ASSY BROKEN. REPLACED NEW HOSE ASSY AND REPLACED BOTH ENG DRIVE PUMP AND FILTERS CSDR G6OA019Exhaust Fairing · missingON PREFLIGHT INSPECTION, GROUND MAINTENANCE NOTED THE NR 1 ENGINE AFT CENTER BODY EXHAUST NOZZLE FAIRING MISSING. GROUND MAINTENANCE REPLACED THE NR 1 ENGINE AFT CENTER BODY EXHAUST NOZZLE PER MM 78-11-02. AIRCRAFT RETURNED TO SERVICE. (M)SDR G60A018Fairing · crackedGROUND MAINTENANCE FOUND PART OF THE LEFT AFT HORIZONTAL STABILIZER TRAILING EDGE UPPER SIDE MISSING. GROUND MAINTENANCE PERFORMED AN INTERIM REPAIR IAW BOEING TELEX SEQUENCE 9809446. AIRCRAFT RETURNED TO SERVICE. (M)SDR 98FDEA00148Fire Bottle · dischargedON PRE FLT CK, FOUND NR 2 ENG FIRE AGT 2 LOW LIGHT CAME ON. ON CK FOUND NR 2 ENG NR 2 BOTTLE DISCHARGE CARTRIDGE DISCHARGED. REMOVED AND REPLACED NR 2 FIRE BOTTLE AND CARTRIDGE AS PER M/M 26-21-02 AND M/M 26-21-01. ALSO, WIRING AND AGENT DISCHARGE S/W (S1-1SDR 98FDEA00144Electronic Unit · failedAFTER TAKEOFF, GEAR HANDLE UP GAVE RED LEFT MAIN INDICATION ON F/O PANEL AND UP FRONT. RAN RED TAB, NO HELP. CHECKED WIRING INTEGRITY FROM S3-682 TERMINAL 4 AND 5 (PROX ELETR UNIT) AS PER WDM 32-61-04 PG 2, FOUND OK. REMOVED AND REPLACED PROXIMITY ELECTRONISDR 98FDEA00142Prox Sensor · damagedBOTH FRONT AND BACK LEFT MAIN GEAR INDICATOR UNSAFE LIGHTS ILLUMINATED AFTER TAKEOFF. FOLLOWED RED TAB. FRONT LIGHT EXTINGUISED, BACK LIGHT REMAINED ILLUM UNTIL LEVEL OFF. PRIOR TO LANDING BOTH FRONT AND BACK LIGHT MAIN GEAR UNSAFE LIGHTS ILLUM, UNTIL LANDISDR 98ZZZX1068Fairing · damagedGROUND EQUIPMENT DAMAGED FIBERGLASS FAIRING FORWARD OF AFT CARGO DOOR OPENING. DAMAGE IS 2.5 INCHES BY 1.5 INCHES BY 0.5 INCH DEEP. TERMPORARY REPAIR CARRIED OUT BY GEMINI.SDR 98FDEA00118Pressurization · malfunctionedDURING CLIMBOUT, CABIN ALT BEGAN CLIMB AT SAME RATE AS A/C. PROBLEM START AT 5000 MSL: AUTO PRESS MODE WAS BEING USED. CABIN ALT RAPID REACH 5000 AND CONT TO CLIMB WITH A/C. USE OF SEMIAUTO STBY AND MANUAL MODES HAD NO EFFECT. CREW LEVEL OFF AT 10000 MSL SDR 98FDEA00117Gcu · failedAFTER T/O, NR 2 GEN OFF LIGHT ILLUMINATED FOLLOWED WITH FLAP DISAGREE FLG IN VIEW AND C/B POPS. ALSO, CAN'T PRESS A/C ON LANDING APPROX 1000 FT, NR 2 ISOL, LIGHT ILLUMINATED RED TAB. REMOVED AND REPLACED NR 2 GCU AND BCU PER M/M 24-21-01. GND OPS PER JRH 8-SDR 98ZZZX1047Tire · blownON ARRIVAL NADI, FOUND LEFT MAIN LANDING GEAR AFT WHEELS (5 AND 6) BLOWN. BOTH AFT WHEEL HUBS SEVERELY DAMAGED. LT INBOARD T/E FLAPS SUSTAINED CRACKS, DENTS, AND PUNCTURES ON UNDER SURFACE IN SEVERAL PLACES. MINOR DAMAGES WERE NOTED ON LEFT BOGIE HYDRAULIC SDR 98FDEA00230Fire Bottle · blownDURING B CHECK, FOUND NUMBER 2 LEFT ENGINE FIRE BOTTLE NUMBER 2 CARTRIDGE BLOWN DURING REMOVAL AND REPLACEMENT OF EXPIRED CARTRIDGE. REMOVED AND REPLACED NR 2 ENGINE LEFT FIRE BOTTLE AND CARTRIDGES PER M/M 26-21-02 AND M/M 26-21-01.SDR 98FDEA00040Coupling · leakingFUEL LEAKING OUT OF AFT PYLON J-BOX. RAN ENG AND INSPECT FUEL SYS AND FUEL NOZZLES, NO LEAKS NOTED. REMOVED PYLON CAPS AND SIDE PANEL TO INSPECT FUEL LINE. CAP LOOSE, NO LEAKS NOTED. FOUND DAMAGED FWD GAMMA COUPLING OF NR 3 ENGINE. REMOVED AND REPLACED BOSDR G60A017Pawl · wornIN THE PROCESS OF TROUBLESHOOTING, APU STARTING FAULT. THE PAWLS OF THE STARTER ADAPTER WERE FOUND TO BE WORN. PARTS WERE ORDERED IDENTIFIED BY P/N FORM DC-10 IPC 49-44-01 ITEM 80. WHEN THE PARTS WERE RECEIVED THERE WAS ONLY AND ADAPTER WITHOUT THE PAWL. WSDR 97FDEA00907Control Unit · failed97-0260 - ON T/O CTR AND RT GEAR RED LIGHTS WERE SLOW TO EXTINGUISH, LEFT GEAR LIGHT WENT FROM EXTINQUISHED TO RED RECYCLE GEAR AND ALL LIGHTS EXTINGUISHED. ON LANDING, ALL GEAR LIGHTS AND WARNING HORNS INDICATED UNSAFE, RECYCLED GEAR AND INITIALLY LEFT AND RSDR 97FDEA00883Skin · damagedFOUND DAMAGED SKIN OF NR 3 AIR CONDITION COMPARTMENT ACCESS DOOR AT ARRIVAL. INSPECTED INSIDE OF NR 3 PACK COMPARTMENT, FOUND OK. OPS TESTED NR 3 PACK, FOUND NO VIBRATION. INSPECTED INSTALLATION AND CONDITION OF THE RT LANDING LIGHT, FOUND GOOD. DAMAGED SDR 97FDEA00841Cadc · malfunctionedDURING T/O ROLL, F/O AIRSPEED INDICATOR REMAINED AT ZERO. ON CLIMBOUT, IT BEHAVED AS AN ALTIMETER. RETURNED AND LANDED AT LAX. REMOVED AND REPLACED NR 2 CADC. FOUND FLEX LINE LOOSE ON FRONT OF NR 2 DIGITAL AIR DATA COMPUTER NR 2 CADC, OPS CK OK IAW MM 34-1SDR 97FDEA00817Actuator · failedWHEN LANDING GEAR WAS DEPLOYED FOR LANDING AT PDX, A LOUD AND HEAVY THUMP WAS HEARD AND FELT AS THE CTR. GEAR IMMEDIATELY CAME DOWN. THE REMAINING GEAR SEEMED TO TAKE MORE TIME THAN USUAL. FOUND RETRACT CYLINDER ROD END STRIPPED OUT AND DAMAGED CENTER LANDISDR 97FDEA00821Uplatch Sensor · malfunctionUPON GEAR RETRACT, MOMENTARY UNSAFE LEFT GEAR IND IAS 220. LIGHT CAME BACK ON AT TOD (FL190) AND REMAINED ON THROUGH DESCENT. CYCLED GEAR SEVERAL TIMES. LIGHT WILL COME ON WITH APPLICATION OF SPEED BRAKES DURING FLIGHT AS WELL. FOUND LOOSE TERMINAL AT TERMSDR 97FDEA00820Prox Cntrl · dirtyWHEN GEAR WERE RAISED AT T/O, THE RT MAIN GEAR INDICATED UNSAFE UP AT BOTH THE FWD AND S/O PANEL RED TABS WERE COMPLETED. PROCEEDED TO DESTINATION AT MAX GEAR EST, SPEED (260 KIAS). DO NOT SUSPECT GEAR IS DOWN. NO CONTROL PROBLEMS. BOTH LIGHTS REMAINED ILLSDR 97FDEA00819Prox Unit · malfunctionAFTER T/O GEAR UP, RT MAIN RED LT ON FWD PANEL REMAINED ILLUMINATED. BOTH RED MAIN GEAR LIGHTS ON S/O'S PANEL REMAINED ON. RECYCLED ALL GEAR LIGHTS IN GREEN, GEAR UP SAME RESULTS, 1 RED FWD 2 RED AFT RAN RED TABS STAYED BELOW 260 KTS APPROX 10 MIN INTO FLT RSDR 97FDEA00799Prox Unit · malfunctionAFTER T/O, LANDING GEAR HANDLE UP, BOTH RED LIGHTS FOR RIGHT GEAR ILLUMINATED. GEAR HANDLE DOWN, ALL GREEN LIGHTS WENT OUT FOLLOWED BY RT GEAR RED ON FWD PANEL. AFTER ABOUT ONE MIN LIGHT WENT OUT. COMPLIED WITH RED TAB PROCEDURES. *S/D* CK'D ALL SENSORS ASDR 97FDEA00798Gear Indication · malfunctionDEPARTING MEM RETRACTED LANDING GEAR, BOTH FRONT AND REAR PANELS SHOW A RED LIGHT ON RIGHT MAIN GEAR. COMPLIED WITH CHECKLIST. LIGHT WENT OUT PROCEED AT NORMAL SPEED. PERFORMED VISUAL INSPECTION OF RT MAIN LANDING GEAR SENSORS AND ASSOCIATED WIRING CONDUIT SDR 97FDEA00732Landing Gear · damagedHARD LANDING, A HARD LANDING INSP WAS PERFORMED. THE INSP FOUND NOSE LAND GEAR COVERED IN 5605. MX DISASSEMBLED AND REPACKED SAME. LEFT MAIN TIRES NR 5 AND NR 6 BLOWN AND WHEELS BENT. THE NR 1, 2, 5 AND 6 WHEELS TIRES AND BRAKES WERE REPLACED. LEFT STRUTSDR 97FDEA00722Throttle Rod · failed97-0200 - NR 1 ENGINE ROLLED BACK. NR 1 ENGINE WAS SHUTDOWN IN ACCORDANCE WITH RED TABS. ALT FL310. N1 50.0 PERCENT EGT 380 N2 75 PERCENT FF 2160. NOTE: WENT TO IDLE NO THROTTLE RESPONSE.OPEN FAN COWL ON NR 1 ENG AND FOUND THE THROTTLE ROD DISCONNECTED FRSDR 97FDEA00792Door · damaged97-0215 NRT STBD SIDE AIR CONDITIONING DOOR FOUND DAMAGE ON PRE FLIGHT. CANNIBALIZED THE NR 3 AIR COND COMP DOOR ASSY BETWEEN A/C N313FE'S AIR COND COMP DOOR. DOOR OPERATION CHECKS OK. THIS IS A DUPLICATE TO CORRECT THE OPERATOR CONTROL NR IT WAS SENT AS 97
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