# Service difficulty reports: N145US, cancelled Nov 1, 2002 A list on [N145US, cancelled Nov 1, 2002](https://openairdocs.org/deregistered/N145US-2002-11-01.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 9903021145](https://openairdocs.org/sdr/9903021145.md): Doubler · cracked · Jun 30, 1999 · N145US · Doug DC1040 · Wing Miscellaneous Structure > DURING M CHECK, FOUND CRACK ON RIGHT WING FIXED LEADING EDGE AT XORS 593 TO 629.3. REPAIRED PER EA 11-168615. - [SDR 9902561145](https://openairdocs.org/sdr/9902561145.md): Longeron · corroded · Jun 28, 1999 · N145US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING M CHECK, FOUND CORROSION ON LONGERON 48R AT FS 1125. REPAIRED PER EA 168621. - [SDR 9902571145](https://openairdocs.org/sdr/9902571145.md): Frame · cracked · Jun 24, 1999 · N145US · Doug DC1040 · Fuselage Main, Frame > DURING M CHECK, FOUND CRACK IN FORWARD CARGO FLOOR FRAME AT FS 1099, RBL 58. REPAIRED PER EA 11-167242. - [SDR 9903031145](https://openairdocs.org/sdr/9903031145.md): Skin · cracked · Jun 13, 1999 · N145US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING M CHECK, FOUND CRACK AND CORROSION ON FUSELAGE SKIN AT FS 1509 - 1531, LONGERON 47L TO 48R. REPAIRED PER EA 11-168288. - [SDR 9902591145](https://openairdocs.org/sdr/9902591145.md): Skin · corroded · May 23, 1999 · N145US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING M CHECK, FOUND CORROSION IN CENTER GEAR WHEEL WELL ON LOWER SHELF SKIN AT FS 1512-1518, LBL 11 - LBL 27. REPAIRED PER EA 11-168288. - [SDR 9902581145](https://openairdocs.org/sdr/9902581145.md): Support · corroded · May 23, 1999 · N145US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M CHECK, FOUND CORROSION IN CENTER GEAR WHEEL WELL ON LOWER LEG SUPPORT AT FS 1510 BETWEEN BL 0 AND LBL 5. REPAIRED PER EA 168288. - [SDR 9902551145](https://openairdocs.org/sdr/9902551145.md): Fitting · corroded · May 23, 1999 · N145US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M CHECK, FOUND CORROSION IN CENTER GEAR WHEEL WELL ON LOWER SHELF SUPPORT FITTING OUTBOARD LEG AT FS 1512-1518 AT RBL 12. REPAIRED PER EA 11-168288. - [SDR 9902541145](https://openairdocs.org/sdr/9902541145.md): Fitting · corroded · May 23, 1999 · N145US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M CHECK, FOUND CORROSION IN CENTER GEAR WHEEL WELL ON LOWER SHELF SUPPORT FITTING OUTBOARD LEG AT FS 1512 - 1517 AT LBL 12. REPAIRED PER EA 11-168288. - [SDR 9902531145](https://openairdocs.org/sdr/9902531145.md): Skin · cracked · May 23, 1999 · N145US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING M CHECK, FOUND CRACK ON SKIN AT FS 1510 BETWEEN LONGERON 50R AND 51R. REPAIRED PER EA 168288. - [SDR 9801091145](https://openairdocs.org/sdr/9801091145.md): Engine · over temp · Jan 15, 1998 · N145US · Doug DC1040 · Engine (Turbine/Turboprop) > DURING THE LANDING ROLLOUT WHILE COMING OUT OF REVERSE THRUST, THE NR 3 ENGINE REACHED AN EGT OF 940C FOR ONE SECOND. THE ENGINE WAS SHUT DOWN. MAINTENANCE PERFORMED AN OVERTEMP INSPECTION PER MM 72-00-00, PG 233 WITH NO DEFECTS. THE BORESCOPE WAS DEFERRED - [SDR 9707021145](https://openairdocs.org/sdr/9707021145.md): Compressor · stalled · Apr 2, 1997 · N145US · Doug DC1040 · Turbine Engine Compressor Section > AFTER AIRCRAFT PUSHBACK FROM GATE, NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL WHILE AT IDLE POWER. FLIGHT CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO THE GATE. MAINTENANCE INSPECTED ENGINE AND FOUND NO DISCREPANCIES. ENGINE WAS GROUND RUN AND ALL PARAMETERS - [SDR 9619931145](https://openairdocs.org/sdr/9619931145.md): Sensor · failed · Sep 14, 1996 · N145US · Doug DC1040 · Fuel Controlling System > DURING LANDING ROLLOUT, THE NR 1 AND NR 3 ENGINES EXPERIENCED REVERSE STALL SIMULTANEOUSLY. BOTH ENGINES WERE SHUT DOWN DUE TO INCREASING EGT AND AIRCRAFT TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BORESCOPE INSPECTION OF THE NR 3 ENGINE - [SDR 9618921145](https://openairdocs.org/sdr/9618921145.md): Tt2 Sensor · failed · Sep 1, 1996 · N145US · Doug DC1040 · Engine BMEP/Torque Indicating > DURING TAXING OUT, THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AND VIBRATION. AS THE NR 1 ENGINE EGT CLIMBED TO 750 DEGREES, THE CREW FOLLOWED COM PROCEDURE, SHUT DOWN THE ENGINE, AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. REPLACED TT2 SENSOR, LEAK - [SDR 9611061145](https://openairdocs.org/sdr/9611061145.md): Web · cracked · May 14, 1996 · N145US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND A CRACK IN THE RIGHT NOSE LANDING GEAR WHEELWELL WEB FS 481 - FS 496, WATER LINE -60 TO -70. REPAIRED WEB (P/N NCA 6246-28) PER EA 11-104263. - [SDR 9612691145](https://openairdocs.org/sdr/9612691145.md): Jamb Doubler · corroded · May 13, 1996 · N145US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION IN THE AFT CARGO DOOR JAMB LOWER AFT CORNER DOUBLERS AND RAIL. REPAIRED DOUBLERS (P/N AFA7052-1, AFA7083-501) AND THE RAIL (P/N AFA7029-1) PER EA 11-104264. - [SDR 9611611145](https://openairdocs.org/sdr/9611611145.md): Seat Track · corroded · May 13, 1996 · N145US · Doug DC1040 · Fuselage, Seat/Cargo Attach Fittings > DURING T-CHECK, FOUND CORROSION ON THE RIGHT OUTBOARD SEAT TRACK FROM FS 1990 - FS 2005, RBL 67. REPAIRED TRACK (P/N NFA 6222-9) PER EA 11-104266. - [SDR 9611031145](https://openairdocs.org/sdr/9611031145.md): Longeron · corroded · May 13, 1996 · N145US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING T-CHECK, FOUND CORROSION ON LONGERON 45R AT FS 1690. REPAIRED LONGERON (P/N AFA 7097-1) PER EA 11-104262. - [SDR 9611591145](https://openairdocs.org/sdr/9611591145.md): Track · corroded · May 11, 1996 · N145US · Doug DC1040 · Fuselage, Seat/Cargo Attach Fittings > DURING T-CHECK, FOUND CORROSION ON THE LEFT OUTBOARD SEAT TRACK FROM FS 1521 - FS 1541, LBL 107. REPAIRED TRACK PER EA 11-099327. - [SDR 9611001145](https://openairdocs.org/sdr/9611001145.md): Longeron · corroded · May 11, 1996 · N145US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING T-CHECK, FOUND CORROSION ON LONGERON 52 AT FS 1652. REPAIRED LONGERON (P/N AFA 7078-1) PER EA 11-104261. - [SDR 9611581145](https://openairdocs.org/sdr/9611581145.md): Longeron · corroded · May 9, 1996 · N145US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING T-CHECK, FOUND CORROSION ON EXTERNAL LONGERON 31R AT FS 1504. REPAIRED LONGERON (P/N AEA 7136-2) PER EA 11-105391. - [SDR 9612681145](https://openairdocs.org/sdr/9612681145.md): Jamb Web · cracked · May 8, 1996 · N145US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND TWO CRACKS 2.5 AND 1.75 LONG 3L IN THE DOOR 3L AFT LOWER DOOR JAMB WEB. REPAIRED WEB (P/N AEA0112-1) PER EA 11-105390. - [SDR 9611571145](https://openairdocs.org/sdr/9611571145.md): Skin · corroded · May 8, 1996 · N145US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING T-CHECK, FOUND CORROSION ON THE EXTERIOR SKIN FS 1343 - FS 1368, LBL 51 - RBL 51, AT THE POPPET DRAIN PLUGS. REPAIRED SKIN (P/N AYB 7065/NYB 6208) PER EA 11-105372. - [SDR 9611561145](https://openairdocs.org/sdr/9611561145.md): Jamb · cracked · May 8, 1996 · N145US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND A CRACK IN THE 3R LOWER FORWARD DOOR JAMB WEB. REPAIRED WEB (P/N AEA 0115-2) PER EA 11-105389. - [SDR 9611541145](https://openairdocs.org/sdr/9611541145.md): Skin · cracked · May 7, 1996 · N145US · Doug DC1040 · Wing, Plate/Skin > DURING T-CHECK, FOUND A CRACK IN THE LEFT WING LEADING EDGE SKIN AT THE FUELING ACCESS CUT-OUT XOS 611. REPAIRED SKIN (P/N ARB 2887-501) PER EA 11-105388. - [SDR 9518341145](https://openairdocs.org/sdr/9518341145.md): Eel Power Supply · failed · Nov 17, 1995 · N145US · Doug DC1040 · Emergency Lighting > DURING LINE CHECK, MID CABIN EMERGENCY FLOOR LIGHTS FAILED TEST. REPLACED THE POWER SUPPLY AND BATTERY. - [SDR 9506631145](https://openairdocs.org/sdr/9506631145.md): Roll Computer · malfunctioned · Apr 23, 1995 · N145US · Doug DC1040 · Autopilot Computer > DURING DESCENT WHEN DEPLOYING SPEEDBRAKES, AIRCRAFT ROLLED TO THE LEFT. VISUAL AND OPERATIONAL CHECK WAS NORMAL, NO FAULTS FOUND AND AUTO-PILOT BITE CHECK WAS NORMAL. RIGGED SPOILER CABLES AND REPLACED THE ROLL COMPUTER. - [SDR 9505681145](https://openairdocs.org/sdr/9505681145.md): Engine · malfunctioned · Apr 13, 1995 · N145US · Doug DC1040 · Engine (Turbine/Turboprop) > DURING CLIMB, THE NR 1 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO LAX WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS MADE. NO FUEL WAS DUMPED. BLACK OIL WAS FOUND AND THE AIRCRAFT WAS FERRIED TO MSP WHERE THE - [SDR 9505491145](https://openairdocs.org/sdr/9505491145.md): Computer · malfunctioned · Apr 9, 1995 · N145US · Doug DC1040 · Autopilot Computer > DURING CRUISE WITH A BANK ANGLE OF 10 DEGREES, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL TO 30 DEGREES. ADDITIONALLY, DURING APPROACH WITH 20 DEGREES SELECTED, THE AIRCRAFT EXPERIENCED ANOTHER UNCOMMANDED ROLL TO 35 DEGREES. REPLACED THE AUTO-PILOT CONTRO ## 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 = 'N145US' AND deregistration_id = 'N145US-2002-11-01' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N145US-2002-11-01/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.