N250YV, cancelled Aug 27, 2008

Service difficulty reports · 70

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 = 'N250YV' AND deregistration_id = 'N250YV-2008-08-27'
  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 SWIA200819349Seat Track · corrodedLEFT SIDE FLOOR SEAT TRACK FRONT SECTION IS CORRODED, FOUND AT C-CHECK. REPLACED LEFT SEAT TRACK IAW APPROVED REPAIR 55-12-345-1235.Jan 15, 2008 · N250YV · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200819348Seat Track · corrodedLEFT FORWARD CABIN SEAT TRACK ALONG WALL IS CORRODED, FOUND AT C-CHECK. REPLACED SEAT TRACK IAW MM 55-12-345-12.Jan 15, 2008 · N250YV · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200819347Seat Track · corrodedFOUND AT C-CHECK, LEFT FORWARD CABIN SEAT TRACK IS CORRODED. REPLACED LEFT FORWARD SEAT TRACK IAW EMB-120 MM 53-01-05.Jan 15, 2008 · N250YV · Emb EMB120ER · Fuselage, Seat/Cargo Attach FittingsSDR SWIA200819346Stringer · crackedFOUND AT C-CHECK, LEFT WING INBOARD UNDERWING NR 2 FUEL PANEL HAS LEAKING RIVETS. REPLACED RIVETS AND REPAIRED CRACKED STRINGER IAW SRM 57-20-03.Jan 15, 2008 · N250YV · Emb EMB120ER · Wing, Longeron/StringerSDR SWIA200718999Sign · crackedFLT 5787 - EMERGENCY EXIT LIGHT AT SEAT 6C IS CRACKED. REPLACED SIGN ASSEMBLY PER MM 33-61-02. OPS CHECK GOOD. Dec 26, 2007 · N250YV · Emb EMB120ER · Emergency LightingSDR SWIA200718824Cap · leakingFLT 5781 - ON TAXI OUT, RECEIVED A TRIPLE CHIME WITH AURAL "OIL PRESSURE" MESSAGE. FOUND OIL LEAKING PAST THE FILLER CAP. ADJUSTED CAP TENSION WITH NO FURTHER LEAKS NOTED. Oct 29, 2007 · N250YV · Emb EMB120ER · Engine Oil Storage (Airframe Furnished)SDR SWIA200718539Skin · crackedRIGHT NACELLE FLAP HAS A CRACK ON THE UPPER SURFACE SKIN. REPLACED RIGHT NACELLE FLAP WITH SERVICEABLE UNIT IAW MM 27-50-03.Jul 28, 2007 · N250YV · Emb EMB120ER · Trailing Edge FlapsSDR SWIA200718333Roller · bindingCOULD NOT OPEN THE CABIN DOOR FROM THE OUTSIDE. ADJUSTED THE FORWARD AND AFT PAX DOOR UPPER ROLLERS ON FUSELAGE CUT OUT. OPS CHECK GOOD.Jun 12, 2007 · N250YV · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200717981Unknown · odorWITH APU RUNNING AND PACKS SET TO APU, FIRE DETECTOR GOES OFF IN LAV WITH AN OVERHEATED ODOR. UNABLE TO DUPLICATE.Mar 7, 2007 · N250YV · Emb EMB120 · Air Distribution SystemSDR SWIA200617498Unknown · smokeAPU BLEED GENERATED SMOKE IN CABIN. UNABLE TO DUPLICATE SMOKE OR SMELL AFTER OPERATING BOTH PACKS WITH APU BLEED. OPERATIONAL CHECKS GOOD.Dec 27, 2006 · N250YV · Emb EMB120ER · APU Bleed Air SystemSDR SWIA200617373Tab · corrodedRT ELEVATOR TRIM TAB SHOWING SIGNS OF CORROSION, DISCOVERED DURING ROUTINE SERVICE INSPECTION. REPLACED RT ELEVATOR TRIM TAB IAW EMB 120 MM 27-32-01 AND TASK CARD RII 27-900-1001.Nov 1, 2006 · N250YV · Emb EMB120ER · Elevator, Tab StructureSDR SWIA200616813Pump · malfunctionedTAKEOFF AURAL WARNING "AUTO FEATHER" DURING TAKEOFF ROLL WHEN AUTO FEATHER SWITCH WAS ON AND GREEN ARMED LIGHT ILLUMINATED. REPLACED RIGHT PROP AUX FEATHER PUMP. OPERATIONAL CHECKS GOOD, S/N OFF - 505.Jun 27, 2006 · N250YV · Emb EMB120ER · Propeller Feathering/ReversingSDR SWIA200616546Servo · malfunctionedDURING CRUISE FLIGHT AT 11,000 A/P AND YAW DAMP ENGAGED. AIRCRAFT UNCOMMAND RT YAW. REPLACED RUDDER SERVO. OPERATIONAL CHECK GOOD IAW EMB MM 22-10-05. P/N: 622-5734-002, S/N ON: 5155, S/N OFF: 8045.Apr 8, 2006 · N250YV · Emb EMB120ER · Autopilot Trim ServoSDR SWIA200616495Actuator · malfunctionedELEVATOR TRIM ACTUATOR BINDING (FREEZING UP) AT ALTITUDE CLIMBED THROUGH RAIN AND BELOW FREEZING TEMPERATURES. REPLACED LT AND RT ELEVATOR TRIM ACTUATORS IAW CH 27-32-02 EMB 120 MM. OPERATIONAL CHECK GOOD. P/N ON 5299-1, OFF 302283, P/N ON 5299 -1 OFF 768.Apr 4, 2006 · N250YV · Emb EMB120ER · Elevator Tab Control SystemSDR SWIA200616343Control Panel · intermittentINTERMITTENT AURAL "STALL WARNING" WITH QUICK FLASH ON MAP. REPLACED STALL WARN TEST PANEL IAW 120 MM 27-34-08. OPERATIONAL CHECK GOOD.Feb 21, 2006 · N250YV · Emb EMB120ER · Stall Warning SystemSDR SWIA200616132Fan · smokeWHEN CHANGING L PACK TO APU, SMOKE SMELL ON GROUND ON "LOW." REMOVED AND REPLACED LEFT A/C GROUND COOLING FAN. OPERATIONAL CHECK GOOD IAW MM 21-51-03.Jan 16, 2006 · N250YV · Emb EMB120ER · Air Distribution FanSDR SWIA200515361Battery Pack · malfunctionedEMERGENCY LIGHTS EXIT SIGN INOP AT ROW 6. REPLACED MIDDLE ELBP. OPERATIONAL CHECK GOOD.Jul 29, 2005 · N250YV · Emb EMB120ER · Emergency LightingSDR SWIA200515247Wire · brokenONE FLOOR EMERGENCY LIGHT INOP AT ROW 9. REPAIRED WIRE TO FLOOR LIGHT AT ROW 9. OPERATIONAL CHECK GOOD.Jul 5, 2005 · N250YV · Emb EMB120ER · Light System WiringSDR SWIA200515030Control Unit · malfunctionedLEFT OUTBOARD FLAP SHOWED DISAGREEMENT AFTER TAKEOFF AFTER SELECTING FLAPS UP. REPLACED FCU IAW MM 27-50-06. OPERATIONAL CHECK GOOD.May 22, 2005 · N250YV · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA200414292Roller · bindingMAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. REPLACED FORWARD AND AFT TRANSLATION BELL CRANK ROLLERS AND TORQUED AFT TRANSLATION CAM MOUNT BASE BOLT. LUBED CAM'S AND ROLLERS. OPERATIONAL CHECK GOOD.Dec 20, 2004 · N250YV · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200414002Door · obstructedMAIN CABIN DOOR WOULD NOT OPEN DUE TO F/A SEAT BLOCKING HANDLE. INSPECTED OPERATION OF FLIGHT ATTENDANT SEAT AND EMERGENCY EXIT DOORS IAW 52-21-03. OPERATIONAL CHECKS GOOD.Oct 22, 2004 · N250YV · Emb EMB120ER · Passenger/Crew DoorsSDR SWIA200413878Computer · malfunctionedSTALL SYSTEM NR 1 WILL NOT TEST. REPLACED NR 1 AOA TRANSDUCER, NR 1 STALL WARNING COMPUTER AND STALL WARNING PANEL ASSY. CLEANED MPU CONNECTOR. OPERATIONAL CHECK GOOD. P/N 120-34428-505, S/N OFF 14882-304, P/N C-81817-1, S/N ON 955, S/N OFF 1101, P/N C-818Sep 26, 2004 · N250YV · Emb EMB120ER · Stall Warning SystemSDR SWIA200413671Cooling Fan · failedON FIRST FLIGHT AFTER SAFETY CHECK, NOTICED A FAINT SMOKE ODOR. REPLACED LT GROUND COOLING FAN WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.Aug 8, 2004 · N250YV · Emb EMB120ER · Air Distribution FanSDR SWIA200413502Computer · malfunctionedRIGHT STALL WARNING ACTIVATES ON MAP AND AURAL WARNING INTERMITTENTLY IN FLIGHT. REPLACED STALL WARN COMPUTER WITH SERVICEABLE UNIT. ALSO REPLACED STALL WARN PANEL WITH SERVICEABLE UNIT. ALL CHECKS GOOD. PANEL P/N: 120-34428-505, S/N OFF 120127.Jun 13, 2004 · N250YV · Emb EMB120ER · Stall Warning SystemSDR SWIA200413124Computer · failedBOTH STALL WARNING SYSTEMS WILL NOT TEST. THE RED STALL WARNING TEST LIGHTS STAY ILLUMINATED AFTER TESTING. REPLACED STALL WARNING COMPUTER WITH SERVICEABLE UNIT. OPS CHECKS GOOD.Apr 3, 2004 · N250YV · Emb EMB120ER · Stall Warning SystemSDR SWIA200412930Power Supply · dischargedMERGENCY FLOOR LIGHTING, FRONT SECTION INOP. REPLACED FORWARD SECTION EMERGENCY LIGHT POWER SUPPLY. OPS CHECKED GOOD.Feb 20, 2004 · N250YV · Emb EMB120ER · Emergency LightingSDR SWIA200412873Wire · damagedCAPTAIN'S STALL WARNING SHAKER INOP ON TEST (PUSHER WORKS). REPAIRED WIRING AT NR 1 STALL SHAKER CONNECTOR. OPS CHECK GOOD.Feb 3, 2004 · N250YV · Emb EMB120ER · Navigation System WiringSDR SWIA200312568Computer · malfunctionedRED AP LIGHT ON AFCP KEPT FLASHING WITH ASSOCIATED TRIPLE CHIME IN FLIGHT. REPLACED CAPTAIN'S SIDE AUTOPILOT COMPUTER. OPS CHECK GOOD ON GROUND CHECK.Oct 28, 2003 · N250YV · Emb EMB120ER · Autopilot SystemSDR SWIA200312552Control Panel · malfunctionedAUTOPILOT FAILED AND DISCONNECTED, INTERMITTENT CAPT F/D FLAG AND ERRATIC FD MOVEMENT ON BOTH SIDES. REMOVED AND REPLACED APP-65A IAW EMB 120 MM 22-10-04. OPS CHECK GOOD.Oct 24, 2003 · N250YV · Emb EMB120ER · Autopilot SystemSDR SWIA200312524Computer · malfunctionedDURING FLIGHT, THE CAPTAIN'S FLIGHT DIRECTOR COMMAND BARS DEVIATED FROM LEVEL TO +/- 5 DEGREES. NOSE DOWN PITCH, FOLLOWED BY AN AUTOPILOT FAILURE MAP INDICATION. REMOVED AND REPLACED NR 1 AUTOPILOT COMPUTER IAW EMB-120 MM 22-10-02. OPS CHECK NORMAL.Oct 17, 2003 · N250YV · Emb EMB120ER · Autopilot ComputerSDR SWIA200312481Computer · malfunctionedFO'S FLIGHT DIRECTOR ERRATIC. REPLACED FO'S APC-65B AUTOPILOT COMPTUER. OPS CHECK GOOD IAW MM 22-10-00.Sep 30, 2003 · N250YV · Emb EMB120ER · Autopilot SystemSDR SWIA200312242Battery Pack · dischargedEMERGENCY LIGHTS FROM ROW 6 FORWARD INOP. REMOVED AND REPLACED THE NR 1 ELBP WITH SERVICEABLE UNIT IAW 33-51-01. OPS CHECKS GOOD. S/N OFF: 1210/04-96Aug 3, 2003 · N250YV · Emb EMB120ER · Emergency LightingSDR SWIA200312142Pin · damagedDURING LANDING GEAR RETRACTION, LEFT MAIN FORWARD GEAR DOORS WOULD NOT CLOSE AFTER GEAR RETRACTED. CLOSED AFTER GEAR WAS DOWN. REPAIRED AND REPLACED PIN ON P1067 LANDING GEAR CONTROL. PERFORMED SEVERAL GEAR SWINGS. OPS CHECK GOOD.Jun 19, 2003 · N250YV · Emb EMB120ER · Landing Gear Retraction/Extension SystemSDR SWIA200311931Sequence Valve · malfunctionedGEAR RETRACTION NORMAL. IN FLIGHT THE B-DISAGREEMENT LIGHTS ILLUMINATED FOR ABOUT 15 SECONDS. UPON GEAR EXTENSION, THE LEFT AND NOSE GEAR EXTENDED NORMALLY, THE RIGHT GEAR REQUIRED ABOUT 7 SECONDS BEFORE THE DISAGREEMENT LIGHT EXTINGUISHED. REPLACED RIGHT MApr 29, 2003 · N250YV · Emb EMB120ER · Landing Gear Retraction/Extension SystemSDR SWIA200211481Warning Light · illuminatedA/B NOSE GEAR LIGHTS DISAGREE, COULD NOT PUT LANDING GEAR DOWN. HAD TO EXTEND LANDING GEAR USING MANUAL OVERRIDE. FOUND NOSE GEAR A SYSTEM DOWN SENSOR HARNESS FAILS. INSPECTED NLG A & B SYSTEM HARNESS. CHECKED PROXIMITY SENSOR CLEARANCES. FOUND NO DEFECTSNov 12, 2002 · N250YV · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA200210978Fuse · corrodedTHE REAR TWO THIRDS OF THE EMERGENCY FLOOR LIGHTING ILLUMINATED. EMERGENCY LIGHT IN ROW 9 ILLUMINATED. ALL EMERGENCY LIGHT SWITCHES IN NORMAL POSITION. AT TIMES, THE LIGHTS WILL EXTINGUISH THEN COME BACK ON. INSPECTED E-LIGHTS SYSTEM. FOUND FUSE X0017 TO Jun 24, 2002 · N250YV · Emb EMB120ER · Emergency LightingSDR SWIA200210630Uplock Switch · looseRIGHT MAIN GEAR INTRANSIT LIGHT ON AND DOOR VIBRATION ON RIGHT MAIN GEAR. RETURNED TO FIELD. INSPECTED, FOUND LOOSE JAM-NUT ON RIGHT GEAR UPLOCK PLUNGER. ADJUSTED AND SECURED NUT. SWUNG GEAR NUMEROUS TIMES. ALL GEAR SWINGS SATISFACTORY.Feb 4, 2002 · N250YV · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA200210579Actuator · failedRIGHT INBOARD FLAP DROOPS. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. OPS CHECKED GOOD. NO LEAKS FOUND.Jan 18, 2002 · N250YV · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200210576Actuator · failedRIGHT INBOARD FLAP WILL NOT RETRACT. INSPECTED RIGHT INBOARD FLAP. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. REMOVED AND REPLACED FCU. CYCLED FLAPS SEVERAL TIMES. OPS CHECKED GOOD.Jan 18, 2002 · N250YV · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200110269Pcu · malfunctionedUNCOMMANDED YAW INFLIGHT WITH FLUTTER MOTION IN TRIM AND ON RUDDER PEDALS. USED QRH PROCEDURE AND TURNED RUDDERS OFF. REMOVED AND REPLACED RUDDER POWER CONTROL UNIT PER AMM 27-22-01. SYSTEM OPS CHECK GOOD.Oct 24, 2001 · N250YV · Emb EMB120ER · Rudder Control SystemSDR SWIA200110257Actuator · failedUPON INITIAL POWER-UP, INBOARD FLAPS SHOWED 1 LIGHT BAR W/DISAGREEMENT ALARM. AFTER FOLLOWING MX PROCEDURES, INBOARD FLAPS SHOW ONLY 2 BARS W/45 DEGREES FLAPS SELECTED AND DISAGREEMENT. RESET OF FLAPS THEN GO TO 45 DEGREES, INBOARD FLAPS DON'T EXTEND AT ALL.Oct 19, 2001 · N250YV · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200110224Actuator · failedFLAP DISAGREEMENT DURING FLAP RETRACTION AFTER LANDING. REPLACED LEFT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-50-00. NO LEAKS NOTED. NO FLAP DISAGREEMENTS NOTED. FLAPS FUNCTIONAL CHECK GOOD.Oct 5, 2001 · N250YV · Emb EMB120ER · Trailing Edge Flap ActuatorSDR SWIA200110171Landing Gear · malfunctionedLANDING GEAR WOULD NOT EXTEND UNTIL THE FOURTH CYCLE OF THE HANDLE, AT WHICH POINT THE GEAR EXTENDED NORMALLY, WITH THREE GREEN A & B LIGHTS ILLUMINATED. AIRCRAFT WAS FERRIED FROM RDD TO SFO. PERFORMED GEAR SWING. OPS CHECK GOOD THROUGH CYCLING OF THE LANDINSep 16, 2001 · N250YV · Emb EMB120ER · Landing Gear Retraction/Extension SystemSDR SWIA200110133Sequence Valve · out of adjUPON GEAR RETRACTION, LEFT MAIN GEAR REMAINED DOWN WITH BOTH A AND B RED AND GREEN LIGHTS ILLUMINATED. RECYCLED GEAR DOWN WITH NORMAL INDICATIONS. CYCLED GEAR UP AND LEFT MAIN AGAIN REMAINED DOWN, THIS TIME WITH RIGHT RED A AND B LIGHTS ILLUMINATED AND THEN Aug 18, 2001 · N250YV · Emb EMB120ER · Landing Gear Door Retract SectionSDR SWIA200110104Connector · looseAFTER TAKEOFF RIGHT GEAR A & B RED LIGHTS REMAINED ON AND IT FELT LIKE GEAR WAS STILL DOWN. WHILE READING QRH, LEFT MAIN A & B RED LIGHTS CAME ON AND AIRPLANE YAWED TO THE LEFT, THEN TO THE RIGHT, FOLLOWED BY ALL LIGHTS OUT.TIGHTENED CONNECTOR AT LEFT AND RIGAug 15, 2001 · N250YV · Emb EMB120ER · Landing Gear Position and WarningSDR SWIA200110103Control Unit · malfunctionedON TAXI OUT FLAP ASYMMETRY RIGHT INBOARD FLAP. FLAP BARS ILLUMINATED.INSPECTED FLAPS. PULLED MX CODES AND CLEARED FAULTS. REPLACED FLAP CONTROL UNIT. GROUND CHECK NORMAL. ALL PANELS CLOSED.Aug 14, 2001 · N250YV · Emb EMB120ER · Trailing Edge Flap Control SystemSDR SWIA972074Pressure Switch · malfunctionedAUTO PRESSURIZATION WOULD NOT PRESSURIZE NORMALLY. RETURNED TO PDX. AUTO PRESSURIZATION CHECKS COMPLIED WITH ON GROUND. OPS CHECKS OK AT THIS TIME.Nov 2, 2000 · N250YV · Emb EMB120ER · Cabin Pressure Control SystemSDR SWIA972012Controller · failedCAPTAIN''S FLIGHT DIRECTOR INOPERABLE. FOUND NUMBER ONE ADS 65 FAULTY. REPLACED NUMBER ONE ADS 65. TESTED AUTOPILOT IAW EMB120 MM 22-10-00. TESTED PITOT STATIC SYSTEM FOR LEAKS IAW FAR 91.411. ALL TESTS GOOD. (P/N: 622-5797-001) (S/N ON: 1678) (S/N OFFSep 24, 2000 · N250YV · Emb EMB120ER · Flight ControllerSDR SWIA971865Rccb · failedWHEN WINDSHIELD HEAT WAS TURNED ON CLIMBING THROUGH 18,000 FT, RECIEVED SINGLE CHIME AND DEICE LIGHT ON MAP LEFT WINDSHIELD HEAT INOP LIGHT ILLUMINATED. AFTER ADDRESSING QRH AND TURNING OFF LEFT WINDSHIELD HEAT, THE SINGLE CHIME WOULD SOUND CONTINUOUSLY FOR AJul 4, 2000 · N250YV · Emb EMB120ER · DC Generating SystemSDR SWIA971847Actuator · malfunctionedON DEPARTURE, RIGHT MAIN GEAR WOULD NOT RETRACT. CYCLED GEAR ONCE, RETURNED TO PDX. REPLACED RIGHT GEAR ACTUATOR AND RIGHT GEAR CONTROL SHUT OFF VALVE IAW MM 323011. ADJUSTED GEAR DOORS SEQUENCE VALVES RIGHT GEAR. GEAR RETRACTION TESTS COMPLIED WITH, LEAKJun 28, 2000 · N250YV · Emb EMB120ER · Landing Gear Actuator
Back to N250YV, cancelled Aug 27, 2008