# Service difficulty reports: N159US, cancelled Nov 12, 2002 A list on [N159US, cancelled Nov 12, 2002](https://openairdocs.org/deregistered/N159US-2002-11-12.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [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 9811101159](https://openairdocs.org/sdr/9811101159.md): Skin · corroded · Nov 20, 1998 · N159US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING M CHECK, FOUND CORROSION ON INTERIOR SURFACE SKIN AT CENTER WHEEL WELL, LONGERON 48L TO 48R, FS 1509 TO 1521. REPAIRED PER EA 11-161113, MFG PART NUMBER AYB7065-. - [SDR 9811451159](https://openairdocs.org/sdr/9811451159.md): Frame · cracked · Oct 2, 1998 · N159US · Doug DC1040 · Fuselage Main, Frame > DURING M-CHECK, FOUND FRAME CRACKED AT FS 454, RBL 64. REPAIRED PER EA 11-161107. - [SDR 9706071159](https://openairdocs.org/sdr/9706071159.md): Switch · bent · Mar 18, 1997 · N159US · Doug DC1040 · Landing Gear Position and Warning > DURING TAKEOFF, ALL THE GEAR RED UNSAFE LIGHTS ILLUMINATED. FOLLOWED COM PROCEDURE AND VERIFIED GEAR UP AND LOCKED. FLIGHT PROCEEDED TO PHX. MAINTENANCE REPLACED THE THROTTLE SWITCHES S1-342. - [SDR 9615461159](https://openairdocs.org/sdr/9615461159.md): Power Supply · inoperative · Jul 16, 1996 · N159US · Doug DC1040 · Emergency Lighting > DURING LINE INSPECTION, FOUND THE ESCAPE EMERGENCY FLOOR LIGHT AT DOOR 3L AND 3R INTERMITTENT. REPLACED BATTERY POWER SUPPLY. - [SDR 9615001159](https://openairdocs.org/sdr/9615001159.md): Engine · malfunctioned · Jul 9, 1996 · N159US · Doug DC1040 · Engine (Turbine/Turboprop) > DURING LANDING ROLLOUT, THE NR 3 ENGINE EXPERIENCED REVERSE STALL. WITH EGT INCREASING TO 1,000 DEGREES, CREW FOLLOWED COM PROCEDURE AND SHUT DOWN THE ENGINE WHILE STILL IN REVERSE. AIRCRAFT WAS TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. BORESCOPE INSPECT - [SDR 9614121159](https://openairdocs.org/sdr/9614121159.md): Power Supply · inoperative · Jun 24, 1996 · N159US · Doug DC1040 · Emergency Lighting > DURING LINE CHECK, FOUND THE FORWARD 'B' ZONE AND AFT ZONE EMERGENCY FLOOR LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND POWER SUPPLY. - [SDR 9611881159](https://openairdocs.org/sdr/9611881159.md): Throttle Switch · broken arm · May 30, 1996 · N159US · Doug DC1040 · Landing Gear Position and Warning > DURING CLIMB, PLACED THE GEAR HANDLE IN THE UP POSITION, THE WARNING HORN SOUNDED AND ALL FOUR GEAR LIGHTS STAYED RED. GEAR WAS RECYCLED AND VISUALLY CHECKED IN THE UP POSITION WITH THE RED GEAR UNSAFE LIGHT STILL ILLUMINATED. FLIGHT CONTINUED TO MSP AND LAND - [SDR 9610651159](https://openairdocs.org/sdr/9610651159.md): Wire · failed · May 15, 1996 · N159US · Doug DC1040 · Entertainment System > DURING CRUISE, MULTIPLEX SYSTEM POWER CABLE SHORTED AND SPARKED BETWEEN SEATS 33DE. MECHANIC ON BOARD DISCONNECTED THE POWER SOURCE FROM THE MUX BOX. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. REPLACED SEATS, CABLES, AND SEAT BOXES. - [SDR 96104311596](https://openairdocs.org/sdr/96104311596.md): Battery Pack · discharged · May 13, 1996 · N159US · Doug DC1040 · Emergency Lighting > DURING LINE INSPECTION, FOUND THE EMERGENCY ESCAPE PATH LIGHT FROM DOOR 3L TO ROW 28 DIM. REPLACED EMERGENCY LIGHT BATTERY PACK. - [SDR 9602921159](https://openairdocs.org/sdr/9602921159.md): Battery · discharged · Feb 4, 1996 · N159US · Doug DC1040 · Emergency Lighting > DURING LINE CHECK, FOUND THE FORWARD SECTION OF THE EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED THE FORWARD BATTERY PACK. - [SDR 9517961159](https://openairdocs.org/sdr/9517961159.md): Fuel Control · failed · Nov 10, 1995 · N159US · Doug DC1040 · Fuel Control/Turbine Engines > DURING TAXI OUT, THE NR 2 ENGINE EGT WENT TO 1,000 DEGREES FOR 30 SECONDS AND THE ENGINE WAS SHUTDOWN. THE ENGINE WAS INSPECTED AND THE EPR INDICATOR WAS REPLACED. DURING THE SECOND TAXI OUT THE FUEL FLOW PEGGED AND THE EGT AGAIN ROSE. THE FUEL CONTROL AND - [SDR 9516881159](https://openairdocs.org/sdr/9516881159.md): Longeron · cracked · Oct 25, 1995 · N159US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING T-CHECK, FOUND A THREE INCH CRACK IN LONGERON 45L AT FS 2160. REPAIRED LONGERON (P/N AJC 7208-1) PER EA 11-103208. - [SDR 9516861159](https://openairdocs.org/sdr/9516861159.md): Door Jamb · corroded · Oct 24, 1995 · N159US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR JAMB INNER BEAM FS 882 AT LONGERON 43L. REPAIRED BEAM (P/N ADA 0251-1) PER EA 11-99322. - [SDR 9516851159](https://openairdocs.org/sdr/9516851159.md): Frame · corroded · Oct 24, 1995 · N159US · Doug DC1040 · Fuselage Main, Frame > DURING T-CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR JAMB FRAMES AT LONGERON 41R, FS 895 AND 1002. REPAIRED FRAMES (P/N ADA 0233-3, -4) PER EA 11-99323. - [SDR 9516831159](https://openairdocs.org/sdr/9516831159.md): Mounting Plates · corroded · Oct 19, 1995 · N159US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION ON BOTH FORWARD RADIO ALTIMETER MOUNTING PLATES. REPAIRED RINGS (P/N AYB 7022, 7053) PER EA 11-103171. - [SDR 9516821159](https://openairdocs.org/sdr/9516821159.md): Frame · cracked · Oct 19, 1995 · N159US · Doug DC1040 · Fuselage Main, Frame > DURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR FRAME AT FS 879, LBL 33. REPAIRED FRAME (P/N ADA 7034) PER EA 11-99361. - [SDR 9516801159](https://openairdocs.org/sdr/9516801159.md): Web · corroded · Oct 17, 1995 · N159US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION IN THE LEFT OUTBOARD FLOOR WEB AND DOUBLER AT FS 1900 - 1928, LBL 90. - [SDR 9516791159](https://openairdocs.org/sdr/9516791159.md): Floor Beam · cracked · Oct 12, 1995 · N159US · Doug DC1040 · Fuselage Main, Floor Beam > DURING T-CHECK, FOUND 0.5 INCH CRACKS IN THE FS 791 FLOOR BEAM UPPER CAP, LBL 20 - RBL 20. REPAIRED CAP (P/N ADA 7226-13) PER EA 11-99329. ## 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 = 'N159US' AND deregistration_id = 'N159US-2002-11-12' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N159US-2002-11-12/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.