N514US, cancelled Jan 26, 2011

Service difficulty reports · 18

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR NWAA082605514Skin · damagedDURING 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 IJun 2, 2008 · N514US · Boeing 757251 · Vertical Stabilizer, Plate/SkinSDR NWAA082645514Skin · damagedDURING INSPECTION FOUND DAMAGE TO FUSELAGE SKIN AT BS 1310 S2R-S3R. REPAIRED PER EA 55-213052. (A)May 23, 2008 · N514US · Boeing 757251 · Fuselage Main, Plate/SkinSDR NWAA082615514Skin Panel · damagedDURING INSPECTION FOUND DAMAGE TO VERTICAL STABILIZER LT SIDE SKIN PANEL. REPAIRED PER EA 55-213388. (A)May 18, 2008 · N514US · Boeing 757251 · Vertical Stabilizer, Plate/SkinSDR NWAA082185514Panel · inflt separationCLIMBING 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 LEFTMay 12, 2008 · N514US · Boeing 757251 · Wing, Plate/SkinSDR NWAA072665514Switch · shortedPILOT 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 Jul 27, 2007 · N514US · Boeing 757251 · Emergency LightingSDR NWAA072645514Battery Pack · malfunctionedDURING 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 CONTINJul 26, 2007 · N514US · Boeing 757251 · Emergency LightingSDR NWAA071835514Connector · looseDURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTS AT ROWS 23 TO 32 INOPERATIVE. RESET ELECTRICAL PLUG ON POWER SUPPLY. AIRCRAFT OK FOR SERVICE.May 12, 2007 · N514US · Boeing 757251 · Light System WiringSDR 0004595514Service difficultyON 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.Dec 29, 2000 · N514US · Boeing 757251 · Aileron Control SystemSDR 0004225514Slide · rupturedDURING SLIDE SHOP TEST AT OPERATING PRESSURE, INFLATABLE SEAM RUPTURED AT DOG LEG. SLIDE WILL BE OVERHAULED AND RECEIVE A NEW INFLATABLE.Mar 17, 2000 · N514US · Boeing 757251 · Escape SlideSDR 9905245514Light · inoperativeDURING 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.Dec 7, 1999 · N514US · Boeing 757251 · Emergency LightingSDR 9714505514Longeron · corrodedDURING TRANSITION CHECK, FOUND CORROSION IN ATR 28R, FS 660 - 680. REPAIRED PER NEA 55-150836.Jul 9, 1997 · N514US · Boeing 757251 · Fuselage Main, Longeron/StringerSDR 9713335514Floorbeam · corrodedDURING TRANSITION CHECK, FOUND CORROSION ON UPPER SURFACE OF FLOORBEAM AT FS 324, RBL 48-60. REPAIRED PER EA 55-150832.Jul 3, 1997 · N514US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9701825514Power Supply · inoperativeDURING PREFLIGHT, FOUND DOOR 1R EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK.Jan 22, 1997 · N514US · Boeing 757251 · Emergency LightingSDR 9610335514Hyd Bypass Ind · malfunctionedDURING 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.May 8, 1996 · N514US · Boeing 727251 · Hydraulic Indicating SystemSDR 9608535514Compressor · stalledDURING 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 Apr 14, 1996 · N514US · Boeing 757251 · Turbine Engine Compressor SectionSDR 9603815514Chord · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON THE BS 345 FLOORBEAM UPPER CHORD FROM LBL 8 TO BL 0. REPAIRED CHORD PER EA 55-13905.Jan 25, 1996 · N514US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9601035514Stator Vane Act · failedDURING 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.Jan 17, 1996 · N514US · Boeing 757251 · Compressor Bleed ControlSDR 9503735514Indicator Bulb · failedEXECUTED 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.Mar 10, 1995 · N514US · Boeing 757251 · Landing Gear Position and Warning
Back to N514US, cancelled Jan 26, 2011