# Service difficulty reports: N157US, cancelled Oct 30, 2002 A list on [N157US, cancelled Oct 30, 2002](https://openairdocs.org/deregistered/N157US-2002-10-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [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 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 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 9803171157](https://openairdocs.org/sdr/9803171157.md): Tr Unit · malfunctioned · Feb 22, 1998 · N157US · Doug DC1040 · Engine Thrust Reverser > DURING LANDING ROLLOUT, THE NR 3 ENGINE THRUST REVERSER DID NOT STOW AND THE ENGINE COMPRESSOR STALLED. THE EGT REACHED 1000C AND THE ENGNE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE AND DEFERRED THE REVERSER PER MEL 78-1A. THE REVERSER WAS STOWED AND - [SDR 9720781157](https://openairdocs.org/sdr/9720781157.md): Compressor · stalled · Nov 5, 1997 · N157US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT WHILE COMING OUT OF REVERSER THRUST, THE NBR 1 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 850C AND THE ENGINE WAS SHUT DOWN. THE CREW STATED THERE WAS A TAIL CROSSWING DURING LANDING. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS N - [SDR 9718791157](https://openairdocs.org/sdr/9718791157.md): Bleed Duct · damaged · Oct 5, 1997 · N157US · Doug DC1040 · Pneumatic Distribution System > AT ROTATION, THE NR 1 ENGINE FIRE LIGHT ILLUMINATED FOLLOWED BY THE REVERSER UNLOCK LIGHT. WITH POWER REDUCED TO IDLE ON THE NR 1 ENGINE, THE FIRE LIGHT WENT OUT. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED WITHOUT INCIDENT. MAINTENANCE FOUND AN ENGINE BLEED - [SDR 9720411157](https://openairdocs.org/sdr/9720411157.md): Longeron · corroded · Oct 4, 1997 · N157US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING M-CHECK, FOUND CORROSION ON LONGERON 51R AT FS 1119. REPAIRED PER EA 11-152790. - [SDR 9720421157](https://openairdocs.org/sdr/9720421157.md): Skin · corroded · Oct 1, 1997 · N157US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING M-CHECK, FOUND CORROSION ON FUSELAGE SKIN FS 1509 TO 1531 AND LONGERON 49L TO 49R. REPAIRED PER EA 11-150758. - [SDR 9718641157](https://openairdocs.org/sdr/9718641157.md): Skin · corroded · Sep 30, 1997 · N157US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING M CHECK, FOUND CORROSION ON SKIN DOUBLER AT FS 1157 BETWEEN LONGERON 51L AND 50L. REPAIRED PER EA 11-152199. - [SDR 9718631157](https://openairdocs.org/sdr/9718631157.md): Skin · corroded · Sep 30, 1997 · N157US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING M CHECK, FOUND CORROSION ON FUSELAGE SKIN AT FS 1148 BETWEEN LONGERONS 51R AND 52. REPAIRED PER EA 11-152199. - [SDR 9718981157](https://openairdocs.org/sdr/9718981157.md): Seat Track · corroded · Sep 25, 1997 · N157US · Doug DC1040 · Fuselage, Seat/Cargo Attach Fittings > DURING M-CHECK, FOUND CORROSION ON SEAT TRACK (P/N AEA7325-11) BETWEEN FS 1288 AND 1301 AT DOOR 3L. REPAIRED PER EA 11-152198. - [SDR 9718421157](https://openairdocs.org/sdr/9718421157.md): Floorbeam · cracked · Sep 24, 1997 · N157US · Doug DC1040 · Fuselage Main, Floor Beam > DURING M CHECK, FOUND CRACK ON FLOORBEAM UPPER CAP AT RBL 5, FS 791. REPAIRED PER EA 11-150759. - [SDR 9720431157](https://openairdocs.org/sdr/9720431157.md): Skin · corroded · Sep 11, 1997 · N157US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING M-CHECK, FOUND CORROSION ON FUSELAGE SKIN AT LOWER BEACON MOUNTING AREA. REPAIRED PER EA 11-150583. - [SDR 9713421157](https://openairdocs.org/sdr/9713421157.md): Compressor · stalled · Jul 9, 1997 · N157US · Doug DC1040 · Turbine Engine Compressor Section > WHEN NR 2 ENGINE POWER ADVANCED TO 1.2 EPR AND STABLE FOR A CROSSBLEED START, THE NR 2 ENGINE COMPRESSOR STALLED. EGT WAS RISING THROUGH 680 CELSIUS WHEN THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED ENGINE PER MM 71-00-00 FOR STALL WITH NO DEFECTS NOTED. - [SDR 9711981157](https://openairdocs.org/sdr/9711981157.md): Egt Indication · rising · Jun 19, 1997 · N157US · Doug DC1040 · Engine EGT/TIT Indicating System > ON LANDING ROLLOUT WHILE COMING OUT OF REVERSE THRUST, THE NR 3 ENGINE EGT STARTED RISING RAPIDLY. THE ENGINE WAS SHUT DOWN WITH A MAX EGT OF 650C. MAINTENANCE CHECKED REVERSER OPERATION PER MM 78-30-00, WITH NO DEFECTS NOTED. EGT WAS WITHIN LIMITS PER MM 7 - [SDR 9704791157](https://openairdocs.org/sdr/9704791157.md): Switch · malfunctioned · Mar 6, 1997 · N157US · Doug DC1040 · Landing Gear Position and Warning > DURING TAKEOFF, RECEIVED THE GEAR WARNING AND 3 RED LIGHTS. RECYCLED GEAR AND RECEIVED 3 RED LIGHTS. REPLACED MAIN LANDING GEAR PROXIMITY CONTROL WITH NO HELP. NEXT FLIGHT DURING TAKEOFF, RED UNSAFE LIGHTS REMAINED ILLUMINATED. FOLLOWED COM AND VERIFIED LA - [SDR 9616011157](https://openairdocs.org/sdr/9616011157.md): Oil Press Transm · failed · Jul 25, 1996 · N157US · Doug DC1040 · Engine Oil Pressure > DURING TAKEOFF, THE NR 3 ENGINE OIL PRESSURE DROPPED TO 20 PSI. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 3 ENGINE OIL PRESSURE TRANSMITTER AND OIL PRESSURE INDICATOR. PERFORMED LEAK AND - [SDR 9603551157](https://openairdocs.org/sdr/9603551157.md): Computer · failed · Feb 12, 1996 · N157US · Doug DC1040 · Air Data Computer > DURING TAKEOFF, CAPTAIN'S AIRSPEED INDICATOR FROZE AT 100 KNOTS WHILE THE FIRST OFFICER'S INDICATOR READ 60 KNOTS. TAKEOFF WAS ABORTED. THE CAPTAIN'S AIR DATA COMPUTER WAS SWAPPED WITH THE NR 3 COMPUTER AND AIRCRAFT RETURNED TO SERVICE. - [SDR 9605301157](https://openairdocs.org/sdr/9605301157.md): Compressor · stalled · Feb 4, 1996 · N157US · Doug DC1040 · Turbine Engine Compressor Section > DURING TAKEOFF, THE NR 3 ENGINE STALLED AND TAKEOFF WAS ABORTED. AIRCRAFT RETURNED TO GATE AND BORESCOPE OF NR 3 ENGINE REVEALED NO TROUBLE. REPLACED THE NR 3 EVC AND PRECISION TRIMMED. OPERATIONAL CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE. - [SDR 9601661157](https://openairdocs.org/sdr/9601661157.md): Longeron · corroded · Jan 18, 1996 · N157US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING L-CHECK, FOUND CORROSION ON THE RBL 7 LONGERON FITTING FROM FS 1509 TO 1521 IN THE CENTER GEAR WHEEL WELL. REPLACED THE FITTING PER SRM 51-00-00 FIG 2. - [SDR 9502651157](https://openairdocs.org/sdr/9502651157.md): Air Duct · ruptured · Feb 16, 1995 · N157US · Doug DC1040 · Engine Thrust Reverser > DURING INITIAL CLIMB, THE NR 1 ENGINE EXPERIENCED THE REVERSER UNLOCK LIGHT ILLUMINATE THEN GO OUT FOLLOWED BY THE FIRE LIGHT AND BELL COMING ON. POWER WAS REDUCED TO IDLE AND THE LIGHTS EXTINGUISHED. THE ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO SEA W ## 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 = 'N157US' AND deregistration_id = 'N157US-2002-10-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N157US-2002-10-30/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.