# Service difficulty reports: N153US, cancelled Nov 26, 2002 A list on [N153US, cancelled Nov 26, 2002](https://openairdocs.org/deregistered/N153US-2002-11-26.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 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 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 9905631153](https://openairdocs.org/sdr/9905631153.md): Stiffener · cracked · Nov 9, 1999 · N153US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M CHECK, FOUND CRACK ON HORIZONTAL T STIFFENER AT FS1521 BULKHEAD AT X=40, Z=97.350. REPAIRED PER EA 12-171336. - [SDR 9809551153](https://openairdocs.org/sdr/9809551153.md): Engine · failed · Jun 12, 1998 · N153US · Doug DC1040 · Engine (Turbine/Turboprop) > DURING CLIMB-OUT, THE NR 2 ENGINE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED AND THE INDICATED OIL TEMPERATURE WAS INCREASING. THE ENGINE WAS SHUT DOWN. 50,000 LBS OF FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO LAX WITHOUT FURTHER DIFFICULTY. THE AIRCRAFT - [SDR 9707031153](https://openairdocs.org/sdr/9707031153.md): Engine · malfunctioned · Apr 2, 1997 · N153US · Doug DC1040 · Engine (Turbine/Turboprop) > AFTER LANDING WHILE COMING OUT OF ENGINE REVERSER, THE NR 1 ENGINE EGT EXCEEDED LIMITS. THE NR 1 ENGINE WAS SHUT DOWN. MAINTENANCE BORESCOPE INSPECTED ENGINE AND PERFORMED RAB'S SYSTEM CHECK IN ACCORDANCE WITH MM 75-30-00, PG 201-203. NO DISCREPANCIES WERE - [SDR 9707051153](https://openairdocs.org/sdr/9707051153.md): Engine · malfunctioned · Mar 24, 1997 · N153US · Doug DC1040 · Engine (Turbine/Turboprop) > AFTER LANDING WHILE COMING OUT OF ENGINE REVERSE THRUST, THE NR 3 ENGINE EGT BEGAN TO EXCEED LIMITS. ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED ENGINE PER MM 72-00-00, PG 227. NO DISCREPANCIES WERE NOTED. - [SDR 9627201153](https://openairdocs.org/sdr/9627201153.md): Reverser System · malfunctioned · Dec 28, 1996 · N153US · Doug DC1040 · Engine Thrust Reverser > DURING TAKEOFF ROLL, ENGINE NR 2 AMBER REVERSE UNLOCK LIGHT ANNUNCIATED. TAKEOFF ABORTED AT 120 KNOTS. MAINTENANCE PERFORMED REJECTED TAKEOFF INSPECTION, NO DAMAGE FOUND. REVERSER ON MEL. - [SDR 9627631153](https://openairdocs.org/sdr/9627631153.md): Skin · corroded · Dec 23, 1996 · N153US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING TRANSITION CHECK, CORROSION WAS FOUND ON THE UNDERWING BARREL SKIN AT FS 1509 TO 1531, LBL 49 TO RBL 49. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLERS PER EA 11-120126 (P/N AYB7065-1). - [SDR 9627621153](https://openairdocs.org/sdr/9627621153.md): Skin · delaminated · Dec 23, 1996 · N153US · Doug DC1040 · Vertical Stabilizer, Plate/Skin > DURING PERIODIC CHECK, DELAMINATION OF THE VERTICAL STABILIZER SKIN AT STR 375 TO 405 RIGHT SIDE. REPAIRED PER EA 11-120122 (P/N ANC7047-2). - [SDR 9627641153](https://openairdocs.org/sdr/9627641153.md): Support · cracked · Dec 20, 1996 · N153US · Doug DC1040 · Horizontal Stabilizer Structure > DURING PERIODIC CHECK, A CRACK WAS FOUND ON THE LEFT HORIZONTAL STABILIZER SECONDARY PIVOT SUPPORT. REMOVED AND REPLACED PIVOT SUPPORT PER EA 11-120135 (P/N AJC7230-1). - [SDR 9627551153](https://openairdocs.org/sdr/9627551153.md): Doubler · gouged · Dec 19, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, GOUGES WERE FOUND ON THE FORWARD CARGO LOWER JAMB SKIN DOUBLER AT FS 911.97. BLENDED OUT GOUGES AND INSTALLED REPAIR DOUBLER PER EA 11-120623. - [SDR 9627561153](https://openairdocs.org/sdr/9627561153.md): Angle · corroded · Dec 18, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FORWARD CARGO JAMB ANGLE AT FS 1002, LONGERON 43R. REMOVED CORROSION AND INSTALLED REPAIR ANGLE PER EA 11-120622 (P/N ADA0233-7). - [SDR 9627611153](https://openairdocs.org/sdr/9627611153.md): Longeron · corroded · Dec 16, 1996 · N153US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FUSELAGE OVERWING EXTERNAL LONGERONS AT FS 1404 TO 1515. BLENDED OUT CORROSION AND INSTALLED DOUBLERS PER EA 11-120121. - [SDR 9627571153](https://openairdocs.org/sdr/9627571153.md): Doorframe · corroded · Dec 16, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE CENTER CARGO DOOR JAMB FRAME AT FS 1787, LONGERON 43R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS AND SHIMS PER EA 11-120612(PN AFA3876-3). - [SDR 9627581153](https://openairdocs.org/sdr/9627581153.md): Mounting Rings · corroded · Dec 12, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE RADIO ALTIMETER ANTENNA MOUNTING RINGS. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER EA 11-120609 (P/N AYB7053-1). - [SDR 9627601153](https://openairdocs.org/sdr/9627601153.md): Support · cracked · Dec 4, 1996 · N153US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, THE FLOOR PANEL ATTACH TAB WAS FOUND CRACKED AT FS 475, LBL 36 FLOOR SUPPORT RAIL. REMOVED DAMAGED AREA AND INSTALLED REPAIR CHANNEL AND FILLERS PER EA 11-105163 (P/N NCA6042-33). - [SDR 9619781153](https://openairdocs.org/sdr/9619781153.md): Fire Wire · chafed · Sep 12, 1996 · N153US · Doug DC1040 · Fire Detection > DURING INITIAL CLIMB, THE NR 3 ENGINE B-LOOP LIGHT ILLUMINATED. CREW FOLLOWED COM PROCEDURE AND CONTINUED FLIGHT AS SCHEDULED. ON FINAL APPROACH, THE NR 3 ENGINE FIRE WARNING INDICATION ILLUMINATED AGAIN. CREW SHUT THE ENGINE DOWN AND MADE A TWO ENGINE LAND - [SDR 9609281153](https://openairdocs.org/sdr/9609281153.md): Wire · failed · Apr 25, 1996 · N153US · Doug DC1040 · Light System Wiring > DURING LINE INSPECTION, FOUND THE FLOOR TRACK LIGHT INOPERATIVE ON THE RIGHT SIDE OF THE FIRST CLASS CABIN. REPAIRED TRACK WIRING AT DOOR 2R. - [SDR 9514971153](https://openairdocs.org/sdr/9514971153.md): Pneu Ind Loop · failed · Oct 1, 1995 · N153US · Doug DC1040 · Pneumatic Indicating System > DURING CRUISE, THE NR 2 PNEUMATIC MANIFOLD FAIL LIGHT ILLUMINATED. FLIGHT RETURNED TO HNL. FOUND THE NR 2 LOOP BAD, DEFERRED PER MEL 36-10A. - [SDR 9505871153](https://openairdocs.org/sdr/9505871153.md): Nr 3 Bearing · failed · Apr 16, 1995 · N153US · Doug DC1040 · Turbine Engine Compressor Section > DURING CLIMB AT ABOUT 7000 FEET, SMOKE AND FUMES APPEARED IN THE CABIN AND THE AIRCRAFT RETURNED TO MSP WHERE AN UNEVENTFUL LANDING WAS MADE. NO FUEL WAS DUMPED. THE NR 3 ENGINE NR 3 BEARING COMPARTMENT SHOWED EVIDENCE OF DISTRESS AND BLACK OIL WAS FOUND. T - [SDR 9505731153](https://openairdocs.org/sdr/9505731153.md): Bracket · corroded · Apr 13, 1995 · N153US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE SHEAR TIE AT FS 1761 TO 1782, STR 45R AND 46R. REMOVED CORROSION AND INSTALLED REPAIR STRAP PER EA 11-97995. - [SDR 9505721153](https://openairdocs.org/sdr/9505721153.md): Angle · cracked · Apr 13, 1995 · N153US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE 'TEE' ANGLE AT FS 1162, RBL 47 ABOVE ACCESS 142AZ. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER EA 11-97997. - [SDR 9504961153](https://openairdocs.org/sdr/9504961153.md): Engine · flame out · Mar 26, 1995 · N153US · Doug DC1040 · Engine (Turbine/Turboprop) > DURING TAXI OUT, THE NR 2 ENGINE EXPERIENCED A SURGE AND FLAMED OUT WITH THE EGT GOING TO MAX FOR THREE SECONDS. TAIL WIND GUSTS TO 25 KTS WERE BEING EXPERIENCED. THE ENGINE WAS INSPECTED AND BOROSCOPE WAS ACCOMPLISHED. AN ENGINE CHANGE HAS BEEN SCHEDULED. - [SDR 9503551153](https://openairdocs.org/sdr/9503551153.md): Compressor · stalled · Mar 6, 1995 · N153US · Doug DC1040 · Turbine Engine Compressor Section > DURING TAKEOFF, THE NR 2 ENGINE COMPRESSOR STALLED AND SHUT DOWN. DUMPED 43,000 LBS OF FUEL AND RETURNED TO LAX. FERRIED AIRCRAFT TO MSP AND REPLACED THE NR 2 ENGINE. - [SDR 9500571153](https://openairdocs.org/sdr/9500571153.md): Compressor · stalled · Jan 11, 1995 · N153US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT IN REVERSE THRUST, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH RISING EGT AND WAS SHUT DOWN. THE ENGINE WAS INSPECTED AND THE RABS SOLENOID WAS REPLACED. A GROUND RUN-UP CONFIRMED PROPER ENGINE OPERATION. A BOROSCOPE IS SCHEDU ## 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 = 'N153US' AND deregistration_id = 'N153US-2002-11-26' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N153US-2002-11-26/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.