# Service difficulty reports: N160US, cancelled Dec 14, 2001 A list on [N160US, cancelled Dec 14, 2001](https://openairdocs.org/deregistered/N160US-2001-12-14.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0002741160](https://openairdocs.org/sdr/0002741160.md): Line · leaking · Jul 28, 2000 · N160US · Doug DC1040 · Hydraulic System, Main > ABORTED TAKEOFF AT 80 KNOTS DUE TO COMPLETE LOSS OF NR 1 HYDRAULIC SYSTEM. REPAIRED LEAKING NR 1 SYSTEM BRAKE RETURN LINE. REPLACED BOTH NR 1 SYSTEM ENGINE DRIVEN PUMP. OPERATIONAL CHECK OK. - [SDR 9901061160](https://openairdocs.org/sdr/9901061160.md): Windshield · broken · Mar 13, 1999 · N160US · Doug DC1040 · Flight Compartment Windows > DURING CRUISE EN ROUTE TO AMS, THE CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED IN FLIGHT. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT INCIDENT. REPLACED WINDSHIELD AND HEAT CONTROLLER, OPERATIONAL CHECK GOOD. - [SDR 9810201160](https://openairdocs.org/sdr/9810201160.md): Frame · cracked · Sep 24, 1998 · N160US · Doug DC1040 · Fuselage Main, Frame > DURING M-CHECK, FOUND CRACK ON LOWER NOSE FUSELAGE FRAME AT FS 459. REPAIRED PER EA 11-157988. - [SDR 9810211160](https://openairdocs.org/sdr/9810211160.md): Floorbeam · cracked · Sep 21, 1998 · N160US · Doug DC1040 · Fuselage Main, Floor Beam > DURING M-CHECK, FOUND CRACK AT THE AFT CARGO FLOORBEAM UPPER CHORD UNDER THE LEFT SEAT TRACK AT FS 1821. REPAIRED PER EA 11-161103. - [SDR 9810221160](https://openairdocs.org/sdr/9810221160.md): Longeron · corroded · Sep 17, 1998 · N160US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING M-CHECK, FOUND CORROSION ON LONGERON INBOARD FLANGE UPPER SIDE AT FS 1159-1179, LONGERON 27L. REPAIRED PER EA 11-160045. - [SDR 9810051160](https://openairdocs.org/sdr/9810051160.md): Support · corroded · Sep 1, 1998 · N160US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND CORROSION ON THE FLOOR SUPPORT ON FRAME 999 ABOVE STR 44L. REPAIRED PER EA 11-160661. - [SDR 9810011160](https://openairdocs.org/sdr/9810011160.md): Skin · corroded · Aug 25, 1998 · N160US · Doug DC1040 · Fuselage Main, Plate/Skin > CENTER LANDING GEAR WHEEL WELL REAR SHELF AREA HAS EXPOSED METAL AND CORROSION AT FS 1509 TO 1521 FROM LEFT KEEL WEB TO RIGHT KEEL WEB. REPAIRED PER EA 11-158662. - [SDR 9808211160](https://openairdocs.org/sdr/9808211160.md): Compressor · stalled · May 2, 1998 · N160US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT REACHED 800C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER TAFI 71-00-00 WITH NO DEFECTS NOTED. THE THRUST REVERSER WAS PLACED ON MEL 78-1A U - [SDR 9807741160](https://openairdocs.org/sdr/9807741160.md): Engine · flamed out · Apr 29, 1998 · N160US · Doug DC1040 · Engine (Turbine/Turboprop) > AT TOP OF DESCENT FL330, THE NR 3 ENGINE FLAMED OUT. THE ENGINE WAS SUCCESSFULLY RESTARTED ON THE SECOND ATTEMPT. THE DESCENT AND LANDING WAS WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE ENGINE PER TAFI 71-00-00 AND PERFORMED A HIGH POWER ENGINE RUN, ALL W - [SDR 9802281160](https://openairdocs.org/sdr/9802281160.md): Tr Unit · malfunctioned · Feb 7, 1998 · N160US · Doug DC1040 · Engine Thrust Reverser > DURING LANDING ROLL AND WHILE COMING OUT OF REVERSE THRUST, THE NR 2 ENGINE THRUST REVERSER REMAINED DEPLOYED. THE CREW ATTEMPTED TO RECYCLE THE REVERSER AND A COMPRESSOR STALL OCCURRED. THE ENGINE WAS SHUT DOWN WITH A MAXIMUM EGT OF 800C. MAINTENANCE INSPE - [SDR 9724251160](https://openairdocs.org/sdr/9724251160.md): Compressor · stalled · Dec 22, 1997 · N160US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT, WHILE IN REVERSE THRUST THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 880C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER MM71-00-00 WITH NO DEFECTS NOTED. THE ENGINE WAS RUN WITH NORMAL INDICATIONS. THE - [SDR 9722411160](https://openairdocs.org/sdr/9722411160.md): Compressor · stalled · Dec 2, 1997 · N160US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT, THE NR 3 ENGINE COMPRESSOR STALLED, EGT REACHED 1000C FOR 1 TO 2 SECONDS BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE DEACTIVATED THE THRUST REVERSER PER MEL AND INSPECTED THE INLET AND EXHAUST WITH NO DAMAGE FOUND. THE BORESCOPE INSP - [SDR 9711121160](https://openairdocs.org/sdr/9711121160.md): Duct · loose · Jun 6, 1997 · N160US · Doug DC1040 · Pneumatic Distribution System > AT APPROXIMATELY V1 SPEED, THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED AND AT 800 FT AGL THE NR 1 REVERSER UNLOCK LIGHT ILLUMINATED. THE NR 1 ENGINE WAS SHUT DOWN PER IAW COM PROCEDURES AND FUEL WAS DUMPED. AIRCRAFT RETURNED TO MSP AND LANDED WITHO - [SDR 9708341160](https://openairdocs.org/sdr/9708341160.md): Tr Light · illuminated · Apr 27, 1997 · N160US · Doug DC1040 · Engine Thrust Reverser > DURING TAKEOFF ROLL, THE NR 2 ENGINE AMBER REVERSER UNLOCK LIGHT ILLUMINATED AND TAKEOFF WAS ABORTED. MAINTENANCE VERIFIED REVERSER WAS STOWED AND ALL LOCKPLATES INSTALLED. MEL 78-2A WAS ADDED. SPECIFIC PART CAUSING PROBLEM TO BE DETERMINED. - [SDR 9707431160](https://openairdocs.org/sdr/9707431160.md): Erp Indicator · malfunctioned · Apr 13, 1997 · N160US · Doug DC1040 · Engine Pressure Ratio (EPR) > DURING TAKEOFF, NR 1 ENGINE EPR LOW. TAKEOFF WAS ABORTED AT 100 KNOTS. MAINTENANCE REPLACED EPR INDICATOR. ENGINE GROUND RUN AND EPR INDICATION AT IDLE AND TAKEOFF POWER WAS NORMAL. - [SDR 9704011160](https://openairdocs.org/sdr/9704011160.md): Compressor · stalled · Feb 26, 1997 · N160US · Doug DC1040 · Turbine Engine Compressor Section > SHORTLY AFTER TAKEOFF, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AT 300 FEET. ENGINE EGT BRIEFLY REACHED 985 AND THEN ALL INDICATIONS RETURNED TO NORMAL. FLIGHT CREW DECIDED TO RETURN TO DEPARTURE AIRPORT. PRIOR TO AN UNEVENTFUL LANDING, 110,000 LBS OF - [SDR 9617741160](https://openairdocs.org/sdr/9617741160.md): Indicator · failed · Aug 15, 1996 · N160US · Doug DC1040 · Cabin Pressure Indicator > DURING CLIMB, CABIN WOULD NOT PRESSURIZE. FLIGHT RETURNED TO SEA. MAINTENANCE REPLACED THE CABIN DIFFERENTIAL PRESSURE INDICATOR, OPERATIONAL CHECK OK. - [SDR 9613741160](https://openairdocs.org/sdr/9613741160.md): Dnlock Switch · failed · Jun 24, 1996 · N160US · Doug DC1040 · Landing Gear Position and Warning > DURING CLIMB, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON WITH THE GEAR HANDLE UP. RECYCLED GEAR AND VERIFIED LEFT MAIN GEAR DOOR WAS UP AND LOCKED. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE DOWNLOCK PROXIMITY SWITCH. - [SDR 9608421160](https://openairdocs.org/sdr/9608421160.md): Skin · corroded · Apr 9, 1996 · N160US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING C-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 869, LONGERON 39R, UNDER THE PRIMARY STATIC PORT. REPAIRED SKIN (P/N ADA7030-1) PER EA 11-103927. - [SDR 9517531160](https://openairdocs.org/sdr/9517531160.md): Link · failed · Nov 4, 1995 · N160US · Doug DC1040 · Landing Gear Door Retract Section > DURING CLIMB, THE AIRCRAFT EXPERIENCED EXCESSIVE VIBRATION. AIRCRAFT DUMPED 120,000 LBS OF FUEL AND RETURNED TO DTW. REPLACED LEFT FORWARD CENTER GEAR DOOR DRIVE LINK AND OPERATIONAL CHECK OK. - [SDR 9515661160](https://openairdocs.org/sdr/9515661160.md): Tee · cracked · Oct 12, 1995 · N160US · Doug DC1040 · Aircraft Fuel Distribution System > DURING CRUISE, UNABLE TO TRANSFER FUEL FROM THE AUXILIARY TANK, DUMPED 35,000 LBS OF FUEL AND RETURNED TO BOS. REPLACED THE CENTER TANK FILL LINE TEE ASSEMBLY. - [SDR 9511151160](https://openairdocs.org/sdr/9511151160.md): Air Distr · fumes · Jul 23, 1995 · N160US · Doug DC1040 · Air Distribution System > DURING TAXI AND ENGINE START, SMOKE AND FUMES WERE DETECTED IN THE CABIN. THE AIRCRAFT RETURNED TO THE GATE. VISUALLY CHECKED THE NR 1 AND NR 3 OIL QUANTITIES. PERFORMED ENGINE RUN AND CHECKED AIR CONDITIONING PACK OPERATION. CHECKED OK, AIRCRAFT APPROVED ## 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 = 'N160US' AND deregistration_id = 'N160US-2001-12-14' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N160US-2001-12-14/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.