# Service difficulty reports: N154US, cancelled Nov 26, 2001 A list on [N154US, cancelled Nov 26, 2001](https://openairdocs.org/deregistered/N154US-2001-11-26.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [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 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 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 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 9905221154](https://openairdocs.org/sdr/9905221154.md): Oven · fire · Nov 11, 1999 · N154US · Doug DC1040 · Buffet/Galleys > AFTER PUSHBACK, FLIGHT ATTENDANT REPORTED FIRE IN AFT GALLEY. ONE HALON BOTTLE WAS DISCHARGED. AIRCRAFT RETURNED TO GATE. FIRE WAS CAUSED BY PAPER/TRASH BEHIND THE OVENS AND COFFEEMAKER. AFTER CLEANUP, GALLEY EQUIPMENT WAS CHECKED FOR PROPER OPERATION. CH - [SDR 9903141154](https://openairdocs.org/sdr/9903141154.md): Prbc Valve · malfunctioned · Aug 5, 1999 · N154US · Doug DC1040 · Compressor Bleed Valve > UPON POWER REDUCTION AT FL330, THE NR 1 ENGINE COMPRESSOR STALLED AND THEN FLAMED OUT. THE ENGINE WAS SECURED, AND RESTARTED NORMALLY AT FL300. ENGINE OPERAITON WAS NORMAL FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED THE ENGINE PER TAFI WITH NO DE - [SDR 9902361154](https://openairdocs.org/sdr/9902361154.md): Valve · contaminated · Jul 2, 1999 · N154US · Doug DC1040 · Cabin Pressure Control System > DURING CRUISE FROM DTW TO SFO, UNABLE TO MAINTAIN CABIN PRESSURE IN AUTO, STANDBY, OR MANUAL. AFTER DESCENT TO FL140, ABLE TO USE MANUAL CONTROL. FLIGHT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. FOUND INSULATION STUCK IN LOWER PRESSURE RELIEF VALVE AND U - [SDR 9901901154](https://openairdocs.org/sdr/9901901154.md): Indication · malfunctioned · May 6, 1999 · N154US · Doug DC1040 · Landing Gear Position and Warning > ON SELECTING GEAR DOWN DURING APPROACH TO HNL, ALL FOUR LIGHTS REMAINED RED AND ANTISKID WOULD NOT TEST. RECYCLED GEAR AND ALL OPERATED NORMALLY WITH NORMAL ANTI-SKID INDICATIONS. FLIGHT LANDED WITHOUT INCIDENT. OPERATIONAL CHECK OK. AIRCRAFT APPROVED FOR - [SDR 9900441154](https://openairdocs.org/sdr/9900441154.md): Valve · leaking · Feb 5, 1999 · N154US · Doug DC1040 · Stabilizer Control System > HYDRAULIC QUANTITY DECREASED TO ZERO DURING FLIGHT. FLIGHT DIVERTED TO PHX AND LANDED WITHOUT INCIDENT. FOUND LOWER HORIZONTAL STABILIZER CONTROL VALVE LEAKING. REPLACED CONTROL VALVE, LEAK AND OPERATIONAL CHECK OK. - [SDR 9806741154](https://openairdocs.org/sdr/9806741154.md): Compressor · stalled · Apr 15, 1998 · N154US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 1 ENGINE COMPRESSOR STALLED. EGT REACHED 930C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER MAINTENANCE MANUAL AND RAN ENGINE TO TAKEOFF POWER WITH NO DEFECTS NOTED. THE AIRCRAFT - [SDR 9805731154](https://openairdocs.org/sdr/9805731154.md): Compressor · stalled · Mar 30, 1998 · N154US · Doug DC1040 · Turbine Engine Compressor Section > DURING THE LANDING ROLLOUT AT APPROXIMATELY 80 KNOTS WHILE IN REVERSE THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUT DOWN AT APPROXIMATELY 40 KNOTS WITH THE EGT AT MAXIMUM FOR 10 SECONDS. THE ENGINE WAS BOROSCOPED WITH NO DEFECTS NOTED. THE - [SDR 9805721154](https://openairdocs.org/sdr/9805721154.md): Compressor · stalled · Mar 30, 1998 · N154US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT AT APPROXIMATELY 80 KNOTS WHILE IN REVERSE THRUST, THE NR 2 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUT DOWN AT APPROXIMATELY 40 KNOTS. THE EGT WAS AT MAXIMUM INDICATION FOR 10 SECONDS. THE ENGINE WAS BOROSCOPED WITH NO TROUBLE FOU - [SDR 9803401154](https://openairdocs.org/sdr/9803401154.md): Compressor · stalled · Feb 24, 1998 · N154US · Doug DC1040 · Turbine Engine Compressor Section > AT TOP OF DESCENT FL330, THE NR 3 ENGINE COMPRESSOR STALLED. ENGINE ANTI-ICE AND FUEL HEAT WERE ON. THE EGT REACHED 870C BEFORE THE ENGINE WAS SHUT DOWN. THE ENGINE RESTARTED NORMALLY AND OPERATED WITHOUT FURTHER DIFFICULTY FOR THE REMAINDER OF THE FLIGHT. - [SDR 9802331154](https://openairdocs.org/sdr/9802331154.md): Tat Wiring · out of position · Feb 8, 1998 · N154US · Doug DC1040 · Outside Air Temperature Indicator/Sensor > ON APPROACH INTO MSP UPON GEAR EXTENSION, ALL FOUR GEAR LIGHTS REMAINED RED. EXECUTED GO-AROUND AND RECYCLED GEAR HANDLE. RECEIVED ALL FOUR GREEN LIGHTS, FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND WIRING FROM TAT INDICATOR INTERFERING WITH GEAR HAND - [SDR 9800421154](https://openairdocs.org/sdr/9800421154.md): Bypass Switch · failed · Jan 7, 1998 · N154US · Doug DC1040 · Engine Oil Indicating System > DURING CLIMBOUT, THE NR 1 ENGINE OIL FILTER BYPASS WARNING LIGHT ILLUMINATED FOR ONE MINUTE. ALL OTHER INDICATIONS WERE NORMAL AND THE LIGHT EXTINGUISHED WITH NO ACTION. DURING DESCENT INTO MSP, THE LIGHT ILLUMINATED AGAIN AND THE CREW SHUT DOWN THE NR 1 ENG - [SDR 9717821154](https://openairdocs.org/sdr/9717821154.md): Engine · failed · Sep 20, 1997 · N154US · Doug DC1040 · Engine (Turbine/Turboprop) > DURING CRUISE, THE NR 1 ENGINE EGT CLIMBED AT LEAST 100 CELSIUS ABOVE THE OTHER ENGINES. ALL OTHER INDICATIONS WERE NORMAL. THE FLIGHT DIVERTED TO MSP AS A PRECAUTION. THE ENGINE FAILED A BORESCOPE INSPECTION AND WAS REPLACED. - [SDR 9711911154](https://openairdocs.org/sdr/9711911154.md): Fire Detector · malfunctioned · Jun 14, 1997 · N154US · Doug DC1040 · Fire Detection > DURING TAXI WHILE TRYING TO START APU, FIRE INDICATION LIGHT ANNUNCIATED. CREW DISCHARGED FIRE BOTTLE. MAINTENANCE FOUND NO EVIDENCE OF FIRE. REPLACED APU FIRE BOTTLE AND APU FIRE DETECTOR CONTROL UNIT (P/N 11-2611-9-0001, 90004). - [SDR 9710951154](https://openairdocs.org/sdr/9710951154.md): Skin · corroded · May 24, 1997 · N154US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING L-CHECK, FOUND CORROSION ON FUSELAGE SKIN FS 1853 TO 1871 AT LONGERON 43L. REPAIRED PER EA 11-124093. - [SDR 9710941154](https://openairdocs.org/sdr/9710941154.md): Spar · corroded · May 23, 1997 · N154US · Doug DC1040 · Wing Spar > DURING L-CHECK, FOUND CORROSION ON UPPER T-CHORD OF AFT SPAR FROM XORS 1077 TO 1086. REPAIRED PER EA 11-150360. - [SDR 9707731154](https://openairdocs.org/sdr/9707731154.md): Bleed Solenoid · malfunctioned · Apr 18, 1997 · N154US · Doug DC1040 · Compressor Bleed Control > AFTER LANDING, WHILE COMING OUT OF REVERSE THRUST, NR 2 ENGINE EGT ROSE RAPIDLY. NR 2 ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED ENGINE PER MM 72-00-00, PG 227 AND REPLACED BLEED OVERRIDE SOLENOID. THE NR 2 ENGINE WAS GROUND RUN AND CHECKED OK. - [SDR 9707741154](https://openairdocs.org/sdr/9707741154.md): Compressor · stalled · Apr 17, 1997 · N154US · Doug DC1040 · Turbine Engine Compressor Section > DURING TOP OF DESCENT, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL. THE NR 3 ENGINE WAS SHUT DOWN. THE NR 3 ENGINE WAS RESTARTED AT 25,000 FEET AND OPERATED NORMALLY FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE BOROSCOPE INSPECTED NR 3 ENGINE, NO TROUBLE - [SDR 9706711154](https://openairdocs.org/sdr/9706711154.md): Compressor · stalled · Mar 31, 1997 · N154US · Doug DC1040 · Turbine Engine Compressor Section > AT TOP OF DESCENT, NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL. ENGINE WAS SHUT DOWN AT 31,000 FEET DUE TO RISING EGT. ENGINE WAS RESTARTED AT 29,000 FEET. AN UNEVENTFUL LANDING WAS PERFORMED AT DESTINATION AIRPORT. MAINTENANCE INSPECTED ENGINE PER MM 71-00- - [SDR 9702381154](https://openairdocs.org/sdr/9702381154.md): Engine · malfunctioned · Feb 1, 1997 · N154US · Doug DC1040 · Engine (Turbine/Turboprop) > DURING LANDING ROLLOUT IN REVERSE THRUST, THE NR 3 ENGINE EGT BEGAN TO CLIMB. THE NR 3 ENGINE WAS SHUT DOWN AT 915 CELSIUS. MAINTENANCE PERFORMED VISUAL INSPECTION OF ENGINE, NO DISCREPANCIES NOTED. IN ACCORDANCE WITH MM 72-00-00, PG 227, NO ACTION IS REQUI - [SDR 9624641154](https://openairdocs.org/sdr/9624641154.md): N 1 Transmitter · failed · Nov 15, 1996 · N154US · Doug DC1040 · Engine RPM Indicating System > DURING TAKEOFF ROLLOUT, THE NR 3 ENGINE N1 WOULD NOT REACH TAKEOFF POWER WITH ENGINE FAIL LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 N1 TRANSMITTER. - [SDR 9618901154](https://openairdocs.org/sdr/9618901154.md): Engine · failed · Aug 31, 1996 · N154US · Doug DC1040 · Engine (Turbine/Turboprop) > EN ROUTE, THE NR 1 ENGINE EXPERIENCED LOSS OF OIL QUANTITY AND PRESSURE. CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGINE, AND RETURNED TO SEA WITHOUT FURTHER INCIDENT. AT THE TIME OF SHUTDOWN, RESIDUAL PRESSURE WAS 28 PSI WITH 30 PERCENT N1 AND 20 PERCENT - [SDR 9614511154](https://openairdocs.org/sdr/9614511154.md): Battery · discharged · Jul 1, 1996 · N154US · Doug DC1040 · Emergency Lighting > DURING LINE INSPECTION, FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED FOUR BATTERIES. - [SDR 9611391154](https://openairdocs.org/sdr/9611391154.md): Hyd Pump · broken plug · May 26, 1996 · N154US · Doug DC1040 · Hydraulic Pump (Electric/Engine), Main > DURING CLIMBOUT, LOST THE NR 1 HYDRAULIC SYSTEM FLUID. FLIGHT DUMPED 40,000 LBS OF FUEL AND RETURNED TO HNL. MAINTENANCE REPLACED THE RIGHT HYDRAULIC PUMP AND THE AIRCRAFT RETURNED TO SERVICE. - [SDR 9602151154](https://openairdocs.org/sdr/9602151154.md): Handle · lack of lube · Jan 28, 1996 · N154US · Doug DC1040 · Landing Gear Selector > DURING GEAR EXTENSION, THE GEAR HANDLE BUTTON STUCK IN PLACE IN DOWN POSITION WITH AN UNSAFE GEAR INDICATION. RECYCLED GEAR AND MANUALLY PUSHED HANDLE IN AND GOT NORMAL GEAR INDICATIONS. LUBED GEAR HANDLE RELEASE BUTTON AND GEAR HANDLE PIVOTS. - [SDR 9600771154](https://openairdocs.org/sdr/9600771154.md): Fitting · cracked · Jan 12, 1996 · N154US · Doug DC1040 · Vertical Stabilizer > DURING T-CHECK, FOUND A CRACK IN THE NR 4 BANJO FITTING, FORWARD RIGHT FLANGE IN THE RADIUS. REPAIRED PER SRM 55-20-00, SHEETS 1-17. - [SDR 9600721154](https://openairdocs.org/sdr/9600721154.md): Longeron · corroded · Jan 10, 1996 · N154US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING T-CHECK, FOUND CORROSION ON LONGERONS 29R TO 31R BETWEEN FS 1401 TO 1521. REPAIRED LONGERONS PER EA 11-104451. - [SDR 9600711154](https://openairdocs.org/sdr/9600711154.md): Skin · corroded · Jan 10, 1996 · N154US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 1661 TO 1681, LONGERONS 51L AND 51R BENEATH THE ANTI-COLLISION BEACON. REPAIRED SKIN (P/N NFA 6214) PER EA 11-99375. - [SDR 9600651154](https://openairdocs.org/sdr/9600651154.md): Bulkhead · cracked · Jan 5, 1996 · N154US · Doug DC1040 · Fuselage Main, Bulkhead > DURING T-CHECK, FOUND VERTICAL CRACKS IN A FS 1787 BULKHEAD STANCHION AT LBL 9, 10 INCHES ABOVE THE CARGO FLOOR LINE. REPAIRED STANCHION PER EA 11-104463. - [SDR 9600371154](https://openairdocs.org/sdr/9600371154.md): Splice Fitting · corroded · Jan 4, 1996 · N154US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION ON THE STR 52 SPLICE FITTING AT FS 1718. FABRICATED AND INSTALLED PER AFA 7102-1 AND SRM 53-10-00. - [SDR 9600621154](https://openairdocs.org/sdr/9600621154.md): Seat Track · corroded · Jan 2, 1996 · N154US · Doug DC1040 · Fuselage, Seat/Cargo Attach Fittings > DURING T-CHECK, FOUND CORROSION IN THE MAIN CABIN SEAT TRACK FS 1878 TO 1908 AT LBL 100. REPAIRED TRACK (P/N AFA 7789-503) PER EA 11-104452. - [SDR 9600611154](https://openairdocs.org/sdr/9600611154.md): Web · corroded · Jan 2, 1996 · N154US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION IN THE FLOOR WEB AND DOUBLER AT FS 1908 TO 1921 LBL 88. REPAIRED WEB (P/N AGA 3807-5) PER EA 11-104450. - [SDR 9522231154](https://openairdocs.org/sdr/9522231154.md): Doubler · corroded · Dec 29, 1995 · N154US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION ON THE NR 1 RADIO ALTIMETER DOUBLERS AT FS 1177. REPAIRED THE DOUBLERS PER EA 11-104443. - [SDR 9522221154](https://openairdocs.org/sdr/9522221154.md): Beam · cracked · Dec 28, 1995 · N154US · Doug DC1040 · Fuselage Main, Floor Beam > DURING T-CHECK, FOUND A CRACK IN THE FS 761 FLOORBEAM AT LBL 8, SEAT TRACK ATTACH HOLE. REPAIRED BEAM (P/N ADA 7226-505) PER EA 11-99295. - [SDR 9521751154](https://openairdocs.org/sdr/9521751154.md): Fitting · cracked · Dec 28, 1995 · N154US · Doug DC1040 · Cargo/Baggage Doors > DURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR LIFT ACTUATOR FITTING, FORWARD LOWER LUG. REPLACED FITTING. - [SDR 9522201154](https://openairdocs.org/sdr/9522201154.md): Door Jamb · corroded · Dec 27, 1995 · N154US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB LOWER OUTBOARD SILL BEAM BELOW LONGERON 43R FROM FS 1035 TO 1039. REPAIRED THE BEAM (P/N ADA 0250-1) PER EA 11-104446. ## 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 n_number = 'N154US' AND deregistration_id = 'N154US-2001-11-26' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N154US-2001-11-26/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.