# Service difficulty reports: N514US, cancelled Jan 26, 2011 A list on [N514US, cancelled Jan 26, 2011](https://openairdocs.org/deregistered/N514US-2011-01-26.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR NWAA082605514](https://openairdocs.org/sdr/NWAA082605514.md): Skin · damaged · Jun 2, 2008 · N514US · Boeing 757251 · Vertical Stabilizer, Plate/Skin > DURING INSPECTION FOUND DAMAGE CAUSED TO VERTICAL STABILIZER RT LOWER LOWER SIDE SKIN PANEL. DAMAGE WAS CAUSED BY THE DEPARTURE OF RT WING TRAILING EDGE PANEL. REPAIRED PER EA 55-213280 SECT1 SECTION 2 REQUIRES REPETITIVE INSPECTIONS NOT TO EXCEED 24 MONTH I - [SDR NWAA082645514](https://openairdocs.org/sdr/NWAA082645514.md): Skin · damaged · May 23, 2008 · N514US · Boeing 757251 · Fuselage Main, Plate/Skin > DURING INSPECTION FOUND DAMAGE TO FUSELAGE SKIN AT BS 1310 S2R-S3R. REPAIRED PER EA 55-213052. (A) - [SDR NWAA082615514](https://openairdocs.org/sdr/NWAA082615514.md): Skin Panel · damaged · May 18, 2008 · N514US · Boeing 757251 · Vertical Stabilizer, Plate/Skin > DURING INSPECTION FOUND DAMAGE TO VERTICAL STABILIZER LT SIDE SKIN PANEL. REPAIRED PER EA 55-213388. (A) - [SDR NWAA082185514](https://openairdocs.org/sdr/NWAA082185514.md): Panel · inflt separation · May 12, 2008 · N514US · Boeing 757251 · Wing, Plate/Skin > CLIMBING THROUGH FL 230 PANEL 651, ON THE UPPER SURFACE OF THE RIGHT WING ABOVE THE RIGHT LANDING GEAR RETRACT CYLINDER, DEPARTED FROM THE AIRCRAFT. WHEN THE PANEL DEPARTED THE AIRCRAFT IT TORE TWO HYDRAULIC LINES FOR THE RETRACT CYLINDER AND DRAINED THE LEFT - [SDR NWAA072665514](https://openairdocs.org/sdr/NWAA072665514.md): Switch · shorted · Jul 27, 2007 · N514US · Boeing 757251 · Emergency Lighting > PILOT REPORTED WITH OVERRIDE SWITCH IN "ARMED" POSITION THE EMERGENCY AISLE LIGHTS FROM DOOR 3 AFT COME ON INTERMITTENTLY. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE FOUND A SHORTED SWITCH, WHICH THEY REPLACED, AND ALSO REMOVED AND REPLACED - [SDR NWAA072645514](https://openairdocs.org/sdr/NWAA072645514.md): Battery Pack · malfunctioned · Jul 26, 2007 · N514US · Boeing 757251 · Emergency Lighting > DURING FLIGHT EMERGENCY LIGHTS FROM DOOR 3 AFT, INCLUDING GALLEY'S AND AISLE CAME ON AND REMAINED ON. RE-CYCLED FLIGHT DECK AND FORWARD CABIN ATTENDANT'S EMERGENCY LIGHT SWITCHES AND NO CHANGE. LATER IN FLIGHT LIGHTS BEGAN FLASHING ON AND OFF. FLIGHT CONTIN - [SDR NWAA071835514](https://openairdocs.org/sdr/NWAA071835514.md): Connector · loose · May 12, 2007 · N514US · Boeing 757251 · Light System Wiring > DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS AT ROWS 23 TO 32 INOPERATIVE. RESET ELECTRICAL PLUG ON POWER SUPPLY. AIRCRAFT OK FOR SERVICE. - [SDR 0004595514](https://openairdocs.org/sdr/0004595514.md): Service difficulty · Dec 29, 2000 · N514US · Boeing 757251 · Aileron Control System > ON APPROACH, AILERON CONTROL DESCRIBED AS BINDING BADLY. ROLL CONTROL NOTED AS VERY UNRESPONSIVE WITH UNCOMMANDED ROLL OSCILLATIONS DURING LAST 200 FT OF LANDING. MAINTENANCE REPLACED BEARING IN THE AILERON FEEL AND TRIM MECHANISM. OPERATIONAL CHECK OK. - [SDR 0004225514](https://openairdocs.org/sdr/0004225514.md): Slide · ruptured · Mar 17, 2000 · N514US · Boeing 757251 · Escape Slide > DURING SLIDE SHOP TEST AT OPERATING PRESSURE, INFLATABLE SEAM RUPTURED AT DOG LEG. SLIDE WILL BE OVERHAULED AND RECEIVE A NEW INFLATABLE. - [SDR 9905245514](https://openairdocs.org/sdr/9905245514.md): Light · inoperative · Dec 7, 1999 · N514US · Boeing 757251 · Emergency Lighting > DURING INTERIOR CHECK, MAINTENANCE FOUND FORWARD SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE DUE TO BROKEN WIRE AT ELECTRICAL CONNECTOR. REPLACED THE ELECTRICAL CONNECTOR. OPERATIONAL CHECK OK. - [SDR 9714505514](https://openairdocs.org/sdr/9714505514.md): Longeron · corroded · Jul 9, 1997 · N514US · Boeing 757251 · Fuselage Main, Longeron/Stringer > DURING TRANSITION CHECK, FOUND CORROSION IN ATR 28R, FS 660 - 680. REPAIRED PER NEA 55-150836. - [SDR 9713335514](https://openairdocs.org/sdr/9713335514.md): Floorbeam · corroded · Jul 3, 1997 · N514US · Boeing 757251 · Fuselage Main, Floor Beam > DURING TRANSITION CHECK, FOUND CORROSION ON UPPER SURFACE OF FLOORBEAM AT FS 324, RBL 48-60. REPAIRED PER EA 55-150832. - [SDR 9701825514](https://openairdocs.org/sdr/9701825514.md): Power Supply · inoperative · Jan 22, 1997 · N514US · Boeing 757251 · Emergency Lighting > DURING PREFLIGHT, FOUND DOOR 1R EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK. - [SDR 9610335514](https://openairdocs.org/sdr/9610335514.md): Hyd Bypass Ind · malfunctioned · May 8, 1996 · N514US · Boeing 727251 · Hydraulic Indicating System > DURING CRUISE FLIGHT, AIRCRAFT INDICATED LOSS OF LEFT SYSTEM HYDRAULICS. AIRCRAFT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT HYDRAULIC FILTER BYPASS INDICATOR. PERFORMED PRESSURE AND LEAK CHECK, CHECKS WERE OK. - [SDR 9608535514](https://openairdocs.org/sdr/9608535514.md): Compressor · stalled · Apr 14, 1996 · N514US · Boeing 757251 · Turbine Engine Compressor Section > DURING CLIMB, THE NR 2 ENGINE EXPERIENCED A VIBRATION AND A COMPRESSOR STALL, THE ENGINE WAS SHUTDOWN. THE AIRCRAFT RETURNED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. THE NR 2 ENGINE WAS BORESCOPE INSPECTED AND FOUND TO HAVE DAMAGE TO THE 6TH THROUGH 10TH - [SDR 9603815514](https://openairdocs.org/sdr/9603815514.md): Chord · corroded · Jan 25, 1996 · N514US · Boeing 757251 · Fuselage Main, Floor Beam > DURING PERIODIC CHECK, FOUND CORROSION ON THE BS 345 FLOORBEAM UPPER CHORD FROM LBL 8 TO BL 0. REPAIRED CHORD PER EA 55-13905. - [SDR 9601035514](https://openairdocs.org/sdr/9601035514.md): Stator Vane Act · failed · Jan 17, 1996 · N514US · Boeing 757251 · Compressor Bleed Control > DURING TAXI OUT, EICAS MESSAGE ENGINE CONTROLS DISPLAYED. THIRTY SECONDS LATER, NR 1 ENGINE SHUT DOWN. AIRCRAFT RETURNED TO GATE. GROUND MAINTENANCE REPLACED NR 1 ENGINE STATOR VANE ACTUATOR. OPERATIONAL CHECK OK. - [SDR 9503735514](https://openairdocs.org/sdr/9503735514.md): Indicator Bulb · failed · Mar 10, 1995 · N514US · Boeing 757251 · Landing Gear Position and Warning > EXECUTED A GO-AROUND AT MSP DUE TO THE RIGHT MAIN GEAR GREEN LIGHT WOULD NOT COME ON. ACFT LANDED WITHOUT INCIDENT. REPLACED INDICATOR BULB, SYSTEM CHECKED NORMAL. ## 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 = 'N514US' AND deregistration_id = 'N514US-2011-01-26' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N514US-2011-01-26/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.