# Service difficulty reports: Douglas DC-10-40 A list on [Douglas DC-10-40](https://openairdocs.org/model/douglas-dc-10-40.md). Newest first. General aviation reporting is voluntary. Page 1 of 13 · 614 reports - [SDR 0202021162](https://openairdocs.org/sdr/0202021162.md): Landing Gear · malfunctioned · Jun 11, 2002 · N162US · Doug DC1040 · Main Landing Gear > ON TAKEOFF UPON GEAR RETRACTION, THE LEFT MAIN GEAR RED LIGHT REMAINED ON. PROCEEDED WITH COCKPIT OPERATING MANUAL PROCEDURE. VISUALLY CHECKED GEAR WHICH APPEARED DOWN. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN - [SDR 0201831149](https://openairdocs.org/sdr/0201831149.md): Indicator · sticks · May 30, 2002 · N149US · Doug DC1040 · Hydraulic Pressure Indicator > ON TAKEOFF ROLL, THE NR 1 HYDRAULIC SYSTEM QUANTITY INDICATOR DROPPED TO 2 GALLONS. FLIGHT CREW FOLLOWED COM PROCEDURE AND RETURNED TO MSP. FLIGHT LANDED WITHOUT INCIDENT. ON TAXI IN, THE NR 1 QUANTITY WENT TO 6 GALLONS. MAINTENANCE SERVICED AND LEAK CHECK - [SDR 0200811161](https://openairdocs.org/sdr/0200811161.md): Projector · Mar 14, 2002 · N161US · Doug DC1040 · Entertainment System > During cruise electrical odor noticed around door 3 area when overhead projector on. Flight continued to DTW and landed without incident. Maintenance replaced overhead projector.See Logpage 6991285.No previous history in last 30 days. - [SDR 0103161156](https://openairdocs.org/sdr/0103161156.md): Duct · broken · Sep 3, 2001 · N156US · Doug DC1040 · Pneumatic Distribution System > ON CLIMBOUT AT MSP, NR 1 AND NR 2 MANIFOLD FAIL LIGHTS ILLUMINATED, ACCOMPANIED BY A LOUD BANG AFT OF NR 2 DOOR. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PNEUMATIC DUCT BROKEN AT FLANGE. REPLACED DUCT, OPERATIONAL CHECK OK. - [SDR 0101951153](https://openairdocs.org/sdr/0101951153.md): Transmitter · malfunctioned · May 23, 2001 · N153US · Doug DC1040 · Engine RPM Indicating System > AT APPROXIMATELY 80 KTS ON TAKEOFF ROLL, THE NR 3 ENGINE FAIL LIGHT ILLUMINATED. THE CREW OBSERVED THE NR 3 N1 AND N2 INDICATIONS DECREASING AND ABORTED TAKEOFF AT 100 KTS. THE EPR INDICATION WAS REPORTED AS NORMAL. MAINTENANCE REPLACED THE N1 TRANSMITTER A - [SDR 0102391153](https://openairdocs.org/sdr/0102391153.md): Stiffener · corroded · May 18, 2001 · N153US · Doug DC1040 · Wing Miscellaneous Structure > In L check, found corrosion on lower end of stiffener outboard of panel 143CZ of wing center section. Repaired per EA11-182723. - [SDR 0102381153](https://openairdocs.org/sdr/0102381153.md): Skin · cracked · May 18, 2001 · N153US · Doug DC1040 · Wing Miscellaneous Structure > During L check, found crack in upper corners of cutout on wing leading edge. Repaired per EA11-183471. - [SDR 0101881155](https://openairdocs.org/sdr/0101881155.md): A/C Pack · contaminated · May 17, 2001 · N155US · Doug DC1040 · Cabin Cooling System > DURING CLIMB, FLIGHT ATTENDANTS REPORTED FUMES AND FINE MIST IN CABIN. FOLLOWED COM PROCEDURE. SMOKE DISSIPATED AFTER NR 1 PACK TURNED OFF. FLIGHT CONTINUED TO MCO FOR AN UNEVENTFUL LANDING. MAINTENANCE FOUND NR 1 PACK CONTAMINATED WITH OIL. REPLACED ALL - [SDR 0101871155](https://openairdocs.org/sdr/0101871155.md): Harness · burned · May 16, 2001 · N155US · Doug DC1040 · Buffet/Galleys > DURING CLIMBOUT OF MSP, CABIN CREW REPORTED SMOKE AND ODOR IN MID CABIN. FOLLOWED COM PROCEDURE WITH NO NOTICEABLE CHANGE IN CONDITION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE DRAINED GEARBOX AND RESERVICED. CHANGED SOCKS AND BURNED - [SDR 0101461157](https://openairdocs.org/sdr/0101461157.md): Longeron · corroded · Apr 18, 2001 · N157US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING H-CHECK, FOUND CORROSION ON L43R AT BS 1783-1786. REPAIRED PER EA 11-182576. - [SDR 0101501159](https://openairdocs.org/sdr/0101501159.md): Coalescer Bag · contaminated · Apr 18, 2001 · N159US · Doug DC1040 · Humidity Control System > DURING TAXI OUT, LAV-C SMOKE ALARM SOUNDED ACCOMPANIED BY AN OILY ODOR IN CABIN. STARTED REMAINING ENGINE AND RAN ALL THREE PACKS. ODOR DISSIPATED AND FLIGHT DEPARTED. DURING CLIMB ODOR RETURNED AND REMAINED BETWEEN DOOR 2 AND 3. RETURNED TO SEA AND LANDED - [SDR 0101331147](https://openairdocs.org/sdr/0101331147.md): Clamp · failed · Apr 4, 2001 · N147US · Doug DC1040 · Pneumatic Distribution System > WHILE IN CRUISE AT FL260, THE NR 2 ENGINE FIRE WARNING ACTIVATED. THE ENGINE WAS SECURED PER COM AND ONE FIRE BOTTLE WAS DISCHARGED. AN EMERGENCY WAS DECLARED WITH THE FLIGHT LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE TWO PNEUMATIC DUCT CLAMPS WHICH - [SDR 0101451157](https://openairdocs.org/sdr/0101451157.md): Door Frame · corroded · Mar 23, 2001 · N157US · Doug DC1040 · Fuselage Main, Structure > DURING H-CHECK, FOUND CORROSION ON FORWARD FRAME OF CENTER CARGO DOOR JAMB AT BS 1708 BETWEEN L42R AND L44R. REPAIRED PER EA 11-183322. - [SDR 0101111162](https://openairdocs.org/sdr/0101111162.md): Accelerometer · failed · Mar 23, 2001 · N162US · Doug DC1040 · Auto Throttle System > WITH NR 1 AUTOPILOT IN COMMAND AND IAS HOLD ENGAGED AT FL 250, AIRCRAFT BEGAN A RAPID DESCENT AND NR 1 AUTOPILOT DISCONNECTED. AIRCRAFT LEVELED OFF AT FL 237 AND FLIGHT CONTINUED WITH MANUAL CONTROL. FLIGHT LANDED AT MCO WITHOUT INCIDENT. REPLACED ACCELEROM - [SDR 0101011154](https://openairdocs.org/sdr/0101011154.md): Light · intermittent · Mar 16, 2001 · N154US · Doug DC1040 · Passenger Compartment Lighting > DURING TAXI OUT, LEFT AFT CABIN READING LIGHTS WERE FLASHING. FLASHING STOPPED AFTER RESETTING READING LIGHT AND CALL LIGHT CIRCUIT BREAKERS BUT FLIGHT ATTENDANT NOTED ELECTRICAL SMOKE. AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. REPLACED OVERHEAD DECOD - [SDR 0101241141](https://openairdocs.org/sdr/0101241141.md): Skin · cracked · Mar 1, 2001 · N141US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING LINE CHECK, FOUND CRACK IN NOSE LANDING GEAR CUTOUT RT FORWARD CORNER SKIN AT BS 464. REPAIRED PER EA 11-182711. - [SDR 0101231146](https://openairdocs.org/sdr/0101231146.md): Longeron · corroded · Feb 28, 2001 · N146US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING M-CHECK, FOUND CORROSION ON VERTICAL LEG OF LONGERON AT NUMBER 3 AIR CONDITIONING EXHAUST DOOR CUTOUT AT BS 515-520 JUST ABOVE THE LOWER EDGE. REPAIRED PER EA 11-180800. - [SDR 0100721148](https://openairdocs.org/sdr/0100721148.md): Coalescer Bag · dirty · Feb 17, 2001 · N148US · Doug DC1040 · Humidity Control System > AFTER TAKEOFF, AIR CONDITIONING PACKS PRODUCED A BLUE CLOUD OF BILLOWING SMOKE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND NR 2 AND NR 3 COALESCER BAGS DIRTY. REPLACED COALESCER BAGS AND PERFORMED PACK BURNOUT PROCEDURE. REPLACED AIR CYCLE M - [SDR 0100571158](https://openairdocs.org/sdr/0100571158.md): Engine · leaking · Feb 16, 2001 · N158US · Doug DC1040 · Turbine Engine Oil System > DURING CLIMB AFTER TAKEOFF, THE CREW REPORTED SMOKE ENTERING THE CABIN FROM A PNEUMATIC SOURCE. THE FLIGHT RETURNED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE NR 1 ENGINE TO BE LEAKING OIL AND CONTAMINATING THE - [SDR 0101221146](https://openairdocs.org/sdr/0101221146.md): Doubler · corroded · Feb 15, 2001 · N146US · Doug DC1040 · Fuselage Main, Structure > DURING M-CHECK, FOUND CORROSION ON FORWARD CARGO DOOR JAMB DOUBLER AT BS 910 ABOVE L43R. REPAIRED PER EA 11-180797. - [SDR 0101201146](https://openairdocs.org/sdr/0101201146.md): Floorbeam · damaged · Jan 29, 2001 · N146US · Doug DC1040 · Fuselage Main, Floor Beam > DURING M-CHECK, MAIN CABIN FLOORBEAM AT BS 1293 WAS FOUND SEVERED AT LBL 106 AND CRACKED AT RBL 106 JUST INSIDE OF NR 3 LT AND NR 3 RT DOORS. REPAIRED PER EA 11-180795. - [SDR 0101431146](https://openairdocs.org/sdr/0101431146.md): Beam · corroded · Jan 26, 2001 · N146US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND CORROSION ON LOWER END OF BEAM AT BS 1521 PRESSURE BULKHEAD. REPAIRED PER EA 11-182647. - [SDR 0100481149](https://openairdocs.org/sdr/0100481149.md): Stiffener · corroded · Jan 18, 2001 · N149US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING L-CHECK, FOUND CORROSION ON THE LOWER END OF VERTICAL STIFFENER UNDER WING FUEL TANK FORWARD PRESSURE BULKHEAD AT BS 1156 L45L-L45R. REPAIRED PER EA 11-180793. - [SDR 0100061152](https://openairdocs.org/sdr/0100061152.md): Door · unsecure · Jan 4, 2001 · N152US · Doug DC1040 · Accessory Compartment Doors > AIRCRAFT WOULD NOT PRESSURIZE DURING CLIMBOUT OF MCO. FLIGHT RETURNED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CENTER ACCESSORY DOOR UNSECURED. ACCESSORY DOOR WARNING SWITCH INOPERATIVE DUE TO BROKEN WIRE. REPAIRED BROKEN WIRE AND SECURED ACCE - [SDR 0004391158](https://openairdocs.org/sdr/0004391158.md): Service difficulty · Dec 1, 2000 · N158US · Doug DC1040 · Landing Gear Position and Warning > AFTER TAKEOFF, FOUR GEAR UNSAFE LIGHTS ILLUMINATED WHEN GEAR SELECTED UP. FOLLOWED COM PROCEDURE. VERIFIED GEAR UP VISUALLY. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. FOUND GEAR HANDLE INTERLOCK RELAY INOPERATIVE. REPLACED RELAY. OPERATIONAL CHECK OK. - [SDR 20001214SH005](https://openairdocs.org/sdr/20001214SH005.md): Fitting · loose · Nov 14, 2000 · N154US · Doug DC1040 · Engine Mount Section > NWA MECHANIC NOTICED GAP BETWEEN THE AFT MOUNT SUPPORT FITTING AND THE AFT ENGINE MOUNT FITTING ON THE NR 3 ENGINE DURING ENGINE INSTALLATION. INSPECTION OF ALL DC-10-40 FLEET OF THE ENGINE MOUNTS AT THE NEXT ''A'' CHECK OR WITHIN 500 FLIGHT HOURS. (X) - [SDR 0004231141](https://openairdocs.org/sdr/0004231141.md): Pump · failed · Nov 9, 2000 · N141US · Doug DC1040 · Hydraulic Pump (Electric/Engine), Main > DURING CRUISE, NR 1 SYSTEM HYDRAULIC QUANTITY DECREASED. FOLLOWED COM PROCEDURE, DEPRESSURIZED AND ISOLATED NR 1 SYSTEM. QUANTITY STABILIZED AT 3.5 GALLONS. UPON APPROACH TO HNL, RESTARTED NR 1 SYSTEM AND QUANTITY WENT TO ZERO. REQUESTED EMERGENCY EQUIPMEN - [SDR 20001127SH009](https://openairdocs.org/sdr/20001127SH009.md): Mount · mismanufactured · Nov 7, 2000 · N154US · Doug DC1040 · Engine Mount Section > SOME DC-10-40 AFT ENGINE MOUNTS WERE MANUFACTURED WITH AN INCORRECT DEPTH OF THE MOUNT BOLT RECESS. THIS CAN RESULT IN A GAP BETWEEN THE PYLON MOUNT FITTING AND THE AFT ENGINE MOUNT DUE TO THE BOTTOMING OUT OF THE MOUNT BOLTS. THE GAP IS BELIEVED TO EXIST BE - [SDR 0004171154](https://openairdocs.org/sdr/0004171154.md): Mount · out of tolerance · Oct 17, 2000 · N154US · Doug DC1040 · Engine Mount Section > DURING NUMBER 3 ENGINE CHANGE A.20 INCH GAP WAS DISCOVERED AT AFT MOUNT, P/N ASL7067-1, S/N 0026 AFTER NEW ENGINE INSTALLED. ENGINE REMOVED AND REPLACED MOUNT WITH P/N ASL7067-1, S/N 0066. ENGINE REINSTALLED. - [SDR 20010125SG019](https://openairdocs.org/sdr/20010125SG019.md): Skin · corroded · Oct 12, 2000 · N142WE · Doug DC1040 · Nacelle/Pylon, Plate/Skin > DURNIG C-CHECK AT ALITALIA, THE FITTING ELEMENT INSIDE THE AIR INTAKE DUCT ON THE NR 2 ENGINE SKIN PANEL ATTACHED TO BANJO''S 1, 2, 3 STRUCTURE IS CORRODED. REPAIRED IAW EO CH-00-015, BOEING TLX CAC-FCO 00-00008H, AND DRAWING AJC 7998. AN FAA FORM 8110-3 WAS - [SDR 20010125SG018](https://openairdocs.org/sdr/20010125SG018.md): Skin · corroded · Oct 12, 2000 · N142WE · Doug DC1040 · Nacelle/Pylon, Plate/Skin > DURING C-CHECK AT ALITALIA, THE FITTING ELEMENT INSIDE THE AIR INTAKE DUCT ON THE NR 2 ENGINE SKIN PANEL ATTACHED TO BANJO''S 1, 2, 3 STRUCTURE IS CORRODED. REPAIRED IAW EO CH-00-015, BOEING TLX CAC-FCO 00-00008H, AND DRAWING AJC 7998. AN FAA FORM 8110-3 WAS - [SDR 0003621157](https://openairdocs.org/sdr/0003621157.md): Frame · cracked · Sep 12, 2000 · N157US · Doug DC1040 · Fuselage Main, Frame > DURING L CHECK FOUND CRACK ON FRAME AT BS 458 STRINGER 40L. REPAIRED PER EA 11-179142. - [SDR 0003351153](https://openairdocs.org/sdr/0003351153.md): Connector · loose · Sep 8, 2000 · N153US · Doug DC1040 · Landing Gear Position and Warning > ON FINAL WHEN GEAR HANDLE WAS PLACED IN THE DOWN POSITION, GREEN LIGHTS DID NOT ILLUMINATE. RECYCLED GEAR AND ALL GREEN LIGHTS ILLUMINATED. FLIGHT CONTINUED TO NORMAL LANDING. MAINTENANCE RESEATED PROXIMITY SENSOR BOX. LEFT TEST CHECKED OK. AIRCRAFT RETUR - [SDR 0003281149](https://openairdocs.org/sdr/0003281149.md): Tail Cone · separated · Sep 6, 2000 · N149US · Doug DC1040 · Aerodynamic Fairings > DURING CLIMB, A BUMP/NOISE WAS NOTICED. FLIGHT CREW DETERMINED IT WAS EITHER WAKE TURBULENCE OR CONTAINER SHIFT. FLIGHT CREW NOTICED NO PROBLEMS AND ALL INDICATIONS WERE NORMAL. FLIGHT CONTINUED TO DESTINATION. UPON LANDING, THE TOWER REPORTED A PROBLEM WI - [SDR 0002831156](https://openairdocs.org/sdr/0002831156.md): Frame · cracked · Aug 3, 2000 · N156US · Doug DC1040 · Fuselage Main, Frame > DURING L CHECK FOUND CRACK IN RIGHT HAND MAIN LANDING GEAR WHEEL WELL FRAME AT BS 1505. REPAIRED PER EA 178315. - [SDR 0002741160](https://openairdocs.org/sdr/0002741160.md): Line · leaking · Jul 28, 2000 · N160US · Doug DC1040 · Hydraulic System, Main > ABORTED TAKEOFF AT 80 KNOTS DUE TO COMPLETE LOSS OF NR 1 HYDRAULIC SYSTEM. REPAIRED LEAKING NR 1 SYSTEM BRAKE RETURN LINE. REPLACED BOTH NR 1 SYSTEM ENGINE DRIVEN PUMP. OPERATIONAL CHECK OK. - [SDR 0002651155](https://openairdocs.org/sdr/0002651155.md): Unknown · odor · Jul 27, 2000 · N155US · Doug DC1040 · Air Distribution System > AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED PUNGENT SMELL IN AFT CABIN. AFTER VERIFICATION BY SECOND OFFICER, FLIGHT DIVERTED TO PSM AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED SYSTEM PER MAINTENANCE MANUAL AND FOUND ALL NORMAL. AIRCRAFT RETURNED TO SERVI - [SDR 20001128AP001](https://openairdocs.org/sdr/20001128AP001.md): Spar Cap · corroded · Jun 21, 2000 · N141WE · Doug DC1040 · Wing Spar > DURING C-CHECK, FOUND CORROSION ON LT WING UPPER REAR SPAR CAP AFT FLANGE AT THREE LOCATIONS, STATIONS ORS 433, 451 AND 455. FOUND CORROSION WAS REMOVED AND FASTENERS WERE REPLACED IAW EO CH-00-007 AND BOEING TLX ALI-FCO 00-0244H DTD 10 APR 00. RELEASED AIRC - [SDR 20001127AP015](https://openairdocs.org/sdr/20001127AP015.md): Skin · corroded · Jun 21, 2000 · N141WE · Doug DC1040 · Wing, Plate/Skin > DURING C-CHECK, FOUND CORROSION ON THE LT WING TRAILING EDGE UPPER SKIN AT STATION XRS 230. CORROSION WAS REMOVED AND FASTENERS WERE REPLACED IAW EO CH-00-009 AND BOEING TLX CAC-FCO 00-00004H DTD 14 APR 00. RELEASED AIRCRAFT FOR REVENUE SERVICE. (M) - [SDR 20001127AP014](https://openairdocs.org/sdr/20001127AP014.md): Skin · corroded · Jun 21, 2000 · N141WE · Doug DC1040 · Wing, Plate/Skin > DURING C-CHECK, FOUND CORROSION ON THE RIGHT WING FIXED LEADING EDGE AT STATION XOS 420-25. CORROSION WAS BLENDED OUT AND FASTENERS WERE REPLACED IAW EO CH-00-006 AND BOEING TLX CAC-FCO 00-00002H DTD 14 APR 00, AND SRM 57-10-00 VOL 1 FIG 15A SHEET 2. RELEASE - [SDR 20001127AP013](https://openairdocs.org/sdr/20001127AP013.md): Spacer · corroded · Jun 21, 2000 · N141WE · Doug DC1040 · Landing Gear Retraction/Extension System > DURING C-CHECK, THE RIGHT MLG UPPER SPACER IS CRACKED BY CORROSION AT STATION XW=212 TO XW=214. INTERIM REPAIR WAS MADE IAW EO CH-00-0010 AND BOEING TLX CAC-FCO 00-00007F DTD 18 APR 00. REPETITIVE INSPECTION ARE REQUIRED AT C-CHECK INSPECTIONS, NOT TO EXCEED - [SDR 20001127AP012](https://openairdocs.org/sdr/20001127AP012.md): Skin · corroded · Jun 21, 2000 · N141WE · Doug DC1040 · Wing, Plate/Skin > DURING C-CHECK, FOUND CORROSIONI ON LT WING LOWER AFT SKIN AT STATION XORS 340.00. FOUND CORROSION BLENDED OUT AND SHOTPEENED IAW EO CH-00-0011 AND BOEING TLX TAU-FCO 00-00097H DTD 17 APR 00. RELEASED AIRCRAFT FOR REVENUE SERVICE. (M) - [SDR 20001127AP011](https://openairdocs.org/sdr/20001127AP011.md): Spar Cap · corroded · Jun 21, 2000 · N141WE · Doug DC1040 · Wing Spar > DURING C-CHECK, FOUND CORROSION ON RIGHT WING REAR SPAR CAP AFT TANG UPPER SURFACE BETWEEN STATION XORS 917 TO 885. FOUND CORROSION BLENDED OUT IAW EO CH-00-012 AND BOEING TLX CAC-FCO- 00-00006H DATED 17, APR 00, AND SRM VOL 2 CHAPTER 51-21-02. RELEASED AIRC - [SDR 20001127AP010](https://openairdocs.org/sdr/20001127AP010.md): Structure · corroded · Jun 21, 2000 · N142WE · Doug DC1040 · Trailing Edge Flaps > DURING MAINTENANCE AT MIA, WHILE SB DC10-57A143, INTERGRANULAR CORROSION WAS FOUND ON THE FORWARD HORIZONTAL FLANGE (UPPER/INTERIOR SIDE) OF ARC1713-2 RIGHT OUTBOARD FLAP LOWER REAR SPAR CAP AT STATIONS XOF 549.672-557.489 AND XOF 722.235-2 - 728.653. REPAIRE - [SDR 0002321235](https://openairdocs.org/sdr/0002321235.md): Frame · corroded · May 16, 2000 · N235NW · Doug DC1040 · Fuselage Main, Frame > DURING -H- CHECK FOUND CORROSION ON BS 1521 PRESSURE WEB TEE CHORD. REPAIRED PER EA 12-170456. - [SDR 0001491154](https://openairdocs.org/sdr/0001491154.md): Unknown · odor · Apr 28, 2000 · N154US · Doug DC1040 · Air Distribution System > AFTER TAKEOFF, STRONG FUMES WERE REPORTED IN THE AIRCRAFT CABIN. FLIGHT CREW DUMPED UNKNOWN QUANTITY OF FUEL AND RETURNED TO DEPARTURE AIRPORT. APU ON MEL FOR POSSIBLE OIL LEAK. MAINTENANCE PERFORMED PACK BURNOUT PROCEDURES. - [SDR 0000991152](https://openairdocs.org/sdr/0000991152.md): Engine · stalled · Mar 22, 2000 · N152US · Doug DC1040 · Engine (Turbine/Turboprop) > DURING TAKEOFF ROLL AT 125 KTS, THE NR 2 ENGINE AUDIBLY AND VISIBLY COMPRESSOR STALLED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE PER TAFI INCLUDING A BOROSCOPE INSPECTION WITH NO DEFECTS NOTED. AN ENGIN - [SDR 0001001150](https://openairdocs.org/sdr/0001001150.md): Pump · failed · Mar 20, 2000 · N150US · Doug DC1040 · Hydraulic Pump (Electric/Engine), Main > DURING CRUISE AT FL350, THE NR 3 ENGINE RIGHT HYDRAULIC PUMP TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED COM PROCEDURE AND RETURNED TO MSP. FLUID QUANTITY IN NR 3 SYSTEM WENT TO ZERO. FLIGHT LANDED IN MSP WITHOUT INCIDENT. REPLACED BOTH HYDRAULIC PUMPS AN - [SDR 20000414AP002](https://openairdocs.org/sdr/20000414AP002.md): Flange · corroded · Mar 2, 2000 · N142WE · Doug DC1040 · Wing Miscellaneous Structure > DURING MAINTENANCE AT MIA, WHILE COMPLYING WITH SB DC10-57A143, INTERGRANULAR CORROSION WAS FOUND ON THE FORWARD HORIZONTAL FLANGE (UPPER/INTERIOR SIDE) OF ARC1713-2 RIGHT OUTBOARD FLAP LOWER REAR SPAR CAP AT STATIONS XOF 549.672 - 557.489 AND XOF 722.235 - 72 - [SDR 0000791162](https://openairdocs.org/sdr/0000791162.md): Fcu · malfunctioned · Mar 1, 2000 · N162US · Doug DC1040 · Fuel Control/Turbine Engines > WHILE DESCENDING AT FL290, THE NR 2 ENGINE FLAMED OUT. THE ENGINE OUT CHECKLIST WAS COMPLETED AND THE ENGINE WAS RESTARTED. OPERATION FOR THE REMAINDER OF THE FLIGHT WAS NORMAL MAINTENANCE PERFORMED A BOROSCOPE INSPECTION WITH NO TROUBLE FOUND. THE FUEL CON Next page: https://openairdocs.org/model/douglas-dc-10-40/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'DC1040' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/douglas-dc-10-40/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.