# Service difficulty reports: N250YV, cancelled Aug 27, 2008

A list on [N250YV, cancelled Aug 27, 2008](https://openairdocs.org/deregistered/N250YV-2008-08-27.md).

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

Page 1 of 2 · 70 reports

- [SDR SWIA200819349](https://openairdocs.org/sdr/SWIA200819349.md): Seat Track · corroded · Jan 15, 2008 · N250YV · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE FLOOR SEAT TRACK FRONT SECTION IS CORRODED, FOUND AT C-CHECK. REPLACED LEFT SEAT TRACK IAW APPROVED REPAIR 55-12-345-1235.
- [SDR SWIA200819348](https://openairdocs.org/sdr/SWIA200819348.md): Seat Track · corroded · Jan 15, 2008 · N250YV · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FORWARD CABIN SEAT TRACK ALONG WALL IS CORRODED, FOUND AT C-CHECK. REPLACED SEAT TRACK IAW MM 55-12-345-12.
- [SDR SWIA200819347](https://openairdocs.org/sdr/SWIA200819347.md): Seat Track · corroded · Jan 15, 2008 · N250YV · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > FOUND AT C-CHECK, LEFT FORWARD CABIN SEAT TRACK IS CORRODED. REPLACED LEFT FORWARD SEAT TRACK IAW EMB-120 MM 53-01-05.
- [SDR SWIA200819346](https://openairdocs.org/sdr/SWIA200819346.md): Stringer · cracked · Jan 15, 2008 · N250YV · Emb EMB120ER · Wing, Longeron/Stringer
  > FOUND 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.
- [SDR SWIA200718999](https://openairdocs.org/sdr/SWIA200718999.md): Sign · cracked · Dec 26, 2007 · N250YV · Emb EMB120ER · Emergency Lighting
  > FLT 5787 - EMERGENCY EXIT LIGHT AT SEAT 6C IS CRACKED. REPLACED SIGN ASSEMBLY PER MM 33-61-02. OPS CHECK GOOD.
- [SDR SWIA200718824](https://openairdocs.org/sdr/SWIA200718824.md): Cap · leaking · Oct 29, 2007 · N250YV · Emb EMB120ER · Engine Oil Storage (Airframe Furnished)
  > FLT 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.
- [SDR SWIA200718539](https://openairdocs.org/sdr/SWIA200718539.md): Skin · cracked · Jul 28, 2007 · N250YV · Emb EMB120ER · Trailing Edge Flaps
  > RIGHT NACELLE FLAP HAS A CRACK ON THE UPPER SURFACE SKIN. REPLACED RIGHT NACELLE FLAP WITH SERVICEABLE UNIT IAW MM 27-50-03.
- [SDR SWIA200718333](https://openairdocs.org/sdr/SWIA200718333.md): Roller · binding · Jun 12, 2007 · N250YV · Emb EMB120ER · Passenger/Crew Doors
  > COULD NOT OPEN THE CABIN DOOR FROM THE OUTSIDE. ADJUSTED THE FORWARD AND AFT PAX DOOR UPPER ROLLERS ON FUSELAGE CUT OUT. OPS CHECK GOOD.
- [SDR SWIA200717981](https://openairdocs.org/sdr/SWIA200717981.md): Unknown · odor · Mar 7, 2007 · N250YV · Emb EMB120 · Air Distribution System
  > WITH APU RUNNING AND PACKS SET TO APU, FIRE DETECTOR GOES OFF IN LAV WITH AN OVERHEATED ODOR. UNABLE TO DUPLICATE.
- [SDR SWIA200617498](https://openairdocs.org/sdr/SWIA200617498.md): Unknown · smoke · Dec 27, 2006 · N250YV · Emb EMB120ER · APU Bleed Air System
  > APU BLEED GENERATED SMOKE IN CABIN. UNABLE TO DUPLICATE SMOKE OR SMELL AFTER OPERATING BOTH PACKS WITH APU BLEED. OPERATIONAL CHECKS GOOD.
- [SDR SWIA200617373](https://openairdocs.org/sdr/SWIA200617373.md): Tab · corroded · Nov 1, 2006 · N250YV · Emb EMB120ER · Elevator, Tab Structure
  > RT 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.
- [SDR SWIA200616813](https://openairdocs.org/sdr/SWIA200616813.md): Pump · malfunctioned · Jun 27, 2006 · N250YV · Emb EMB120ER · Propeller Feathering/Reversing
  > TAKEOFF 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.
- [SDR SWIA200616546](https://openairdocs.org/sdr/SWIA200616546.md): Servo · malfunctioned · Apr 8, 2006 · N250YV · Emb EMB120ER · Autopilot Trim Servo
  > DURING 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.
- [SDR SWIA200616495](https://openairdocs.org/sdr/SWIA200616495.md): Actuator · malfunctioned · Apr 4, 2006 · N250YV · Emb EMB120ER · Elevator Tab Control System
  > ELEVATOR 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.
- [SDR SWIA200616343](https://openairdocs.org/sdr/SWIA200616343.md): Control Panel · intermittent · Feb 21, 2006 · N250YV · Emb EMB120ER · Stall Warning System
  > INTERMITTENT AURAL "STALL WARNING" WITH QUICK FLASH ON MAP. REPLACED STALL WARN TEST PANEL IAW 120 MM 27-34-08. OPERATIONAL CHECK GOOD.
- [SDR SWIA200616132](https://openairdocs.org/sdr/SWIA200616132.md): Fan · smoke · Jan 16, 2006 · N250YV · Emb EMB120ER · Air Distribution Fan
  > WHEN 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.
- [SDR SWIA200515361](https://openairdocs.org/sdr/SWIA200515361.md): Battery Pack · malfunctioned · Jul 29, 2005 · N250YV · Emb EMB120ER · Emergency Lighting
  > EMERGENCY LIGHTS EXIT SIGN INOP AT ROW 6. REPLACED MIDDLE ELBP. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515247](https://openairdocs.org/sdr/SWIA200515247.md): Wire · broken · Jul 5, 2005 · N250YV · Emb EMB120ER · Light System Wiring
  > ONE FLOOR EMERGENCY LIGHT INOP AT ROW 9. REPAIRED WIRE TO FLOOR LIGHT AT ROW 9. OPERATIONAL CHECK GOOD.
- [SDR SWIA200515030](https://openairdocs.org/sdr/SWIA200515030.md): Control Unit · malfunctioned · May 22, 2005 · N250YV · Emb EMB120ER · Trailing Edge Flap Control System
  > LEFT OUTBOARD FLAP SHOWED DISAGREEMENT AFTER TAKEOFF AFTER SELECTING FLAPS UP. REPLACED FCU IAW MM 27-50-06. OPERATIONAL CHECK GOOD.
- [SDR SWIA200414292](https://openairdocs.org/sdr/SWIA200414292.md): Roller · binding · Dec 20, 2004 · N250YV · Emb EMB120ER · Passenger/Crew Doors
  > MAIN 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.
- [SDR SWIA200414002](https://openairdocs.org/sdr/SWIA200414002.md): Door · obstructed · Oct 22, 2004 · N250YV · Emb EMB120ER · Passenger/Crew Doors
  > MAIN 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.
- [SDR SWIA200413878](https://openairdocs.org/sdr/SWIA200413878.md): Computer · malfunctioned · Sep 26, 2004 · N250YV · Emb EMB120ER · Stall Warning System
  > STALL 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-818
- [SDR SWIA200413671](https://openairdocs.org/sdr/SWIA200413671.md): Cooling Fan · failed · Aug 8, 2004 · N250YV · Emb EMB120ER · Air Distribution Fan
  > ON FIRST FLIGHT AFTER SAFETY CHECK, NOTICED A FAINT SMOKE ODOR. REPLACED LT GROUND COOLING FAN WITH A SERVICEABLE UNIT. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413502](https://openairdocs.org/sdr/SWIA200413502.md): Computer · malfunctioned · Jun 13, 2004 · N250YV · Emb EMB120ER · Stall Warning System
  > RIGHT 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.
- [SDR SWIA200413124](https://openairdocs.org/sdr/SWIA200413124.md): Computer · failed · Apr 3, 2004 · N250YV · Emb EMB120ER · Stall Warning System
  > BOTH 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.
- [SDR SWIA200412930](https://openairdocs.org/sdr/SWIA200412930.md): Power Supply · discharged · Feb 20, 2004 · N250YV · Emb EMB120ER · Emergency Lighting
  > MERGENCY FLOOR LIGHTING, FRONT SECTION INOP. REPLACED FORWARD SECTION EMERGENCY LIGHT POWER SUPPLY. OPS CHECKED GOOD.
- [SDR SWIA200412873](https://openairdocs.org/sdr/SWIA200412873.md): Wire · damaged · Feb 3, 2004 · N250YV · Emb EMB120ER · Navigation System Wiring
  > CAPTAIN'S STALL WARNING SHAKER INOP ON TEST (PUSHER WORKS). REPAIRED WIRING AT NR 1 STALL SHAKER CONNECTOR. OPS CHECK GOOD.
- [SDR SWIA200312568](https://openairdocs.org/sdr/SWIA200312568.md): Computer · malfunctioned · Oct 28, 2003 · N250YV · Emb EMB120ER · Autopilot System
  > RED AP LIGHT ON AFCP KEPT FLASHING WITH ASSOCIATED TRIPLE CHIME IN FLIGHT. REPLACED CAPTAIN'S SIDE AUTOPILOT COMPUTER. OPS CHECK GOOD ON GROUND CHECK.
- [SDR SWIA200312552](https://openairdocs.org/sdr/SWIA200312552.md): Control Panel · malfunctioned · Oct 24, 2003 · N250YV · Emb EMB120ER · Autopilot System
  > AUTOPILOT 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.
- [SDR SWIA200312524](https://openairdocs.org/sdr/SWIA200312524.md): Computer · malfunctioned · Oct 17, 2003 · N250YV · Emb EMB120ER · Autopilot Computer
  > DURING 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.
- [SDR SWIA200312481](https://openairdocs.org/sdr/SWIA200312481.md): Computer · malfunctioned · Sep 30, 2003 · N250YV · Emb EMB120ER · Autopilot System
  > FO'S FLIGHT DIRECTOR ERRATIC. REPLACED FO'S APC-65B AUTOPILOT COMPTUER. OPS CHECK GOOD IAW MM 22-10-00.
- [SDR SWIA200312242](https://openairdocs.org/sdr/SWIA200312242.md): Battery Pack · discharged · Aug 3, 2003 · N250YV · Emb EMB120ER · Emergency Lighting
  > EMERGENCY 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: 1210/04-96
- [SDR SWIA200312142](https://openairdocs.org/sdr/SWIA200312142.md): Pin · damaged · Jun 19, 2003 · N250YV · Emb EMB120ER · Landing Gear Retraction/Extension System
  > DURING 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.
- [SDR SWIA200311931](https://openairdocs.org/sdr/SWIA200311931.md): Sequence Valve · malfunctioned · Apr 29, 2003 · N250YV · Emb EMB120ER · Landing Gear Retraction/Extension System
  > GEAR 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 M
- [SDR SWIA200211481](https://openairdocs.org/sdr/SWIA200211481.md): Warning Light · illuminated · Nov 12, 2002 · N250YV · Emb EMB120ER · Landing Gear Position and Warning
  > A/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 DEFECTS
- [SDR SWIA200210978](https://openairdocs.org/sdr/SWIA200210978.md): Fuse · corroded · Jun 24, 2002 · N250YV · Emb EMB120ER · Emergency Lighting
  > THE 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
- [SDR SWIA200210630](https://openairdocs.org/sdr/SWIA200210630.md): Uplock Switch · loose · Feb 4, 2002 · N250YV · Emb EMB120ER · Landing Gear Position and Warning
  > RIGHT 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.
- [SDR SWIA200210579](https://openairdocs.org/sdr/SWIA200210579.md): Actuator · failed · Jan 18, 2002 · N250YV · Emb EMB120ER · Trailing Edge Flap Actuator
  > RIGHT INBOARD FLAP DROOPS. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. OPS CHECKED GOOD. NO LEAKS FOUND.
- [SDR SWIA200210576](https://openairdocs.org/sdr/SWIA200210576.md): Actuator · failed · Jan 18, 2002 · N250YV · Emb EMB120ER · Trailing Edge Flap Actuator
  > RIGHT 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.
- [SDR SWIA200110269](https://openairdocs.org/sdr/SWIA200110269.md): Pcu · malfunctioned · Oct 24, 2001 · N250YV · Emb EMB120ER · Rudder Control System
  > UNCOMMANDED 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.
- [SDR SWIA200110257](https://openairdocs.org/sdr/SWIA200110257.md): Actuator · failed · Oct 19, 2001 · N250YV · Emb EMB120ER · Trailing Edge Flap Actuator
  > UPON 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.
- [SDR SWIA200110224](https://openairdocs.org/sdr/SWIA200110224.md): Actuator · failed · Oct 5, 2001 · N250YV · Emb EMB120ER · Trailing Edge Flap Actuator
  > FLAP 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.
- [SDR SWIA200110171](https://openairdocs.org/sdr/SWIA200110171.md): Landing Gear · malfunctioned · Sep 16, 2001 · N250YV · Emb EMB120ER · Landing Gear Retraction/Extension System
  > LANDING 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 LANDIN
- [SDR SWIA200110133](https://openairdocs.org/sdr/SWIA200110133.md): Sequence Valve · out of adj · Aug 18, 2001 · N250YV · Emb EMB120ER · Landing Gear Door Retract Section
  > UPON 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
- [SDR SWIA200110104](https://openairdocs.org/sdr/SWIA200110104.md): Connector · loose · Aug 15, 2001 · N250YV · Emb EMB120ER · Landing Gear Position and Warning
  > AFTER 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 RIG
- [SDR SWIA200110103](https://openairdocs.org/sdr/SWIA200110103.md): Control Unit · malfunctioned · Aug 14, 2001 · N250YV · Emb EMB120ER · Trailing Edge Flap Control System
  > ON 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.
- [SDR SWIA972074](https://openairdocs.org/sdr/SWIA972074.md): Pressure Switch · malfunctioned · Nov 2, 2000 · N250YV · Emb EMB120ER · Cabin Pressure Control System
  > AUTO PRESSURIZATION WOULD NOT PRESSURIZE NORMALLY. RETURNED TO PDX. AUTO PRESSURIZATION CHECKS COMPLIED WITH ON GROUND. OPS CHECKS OK AT THIS TIME.
- [SDR SWIA972012](https://openairdocs.org/sdr/SWIA972012.md): Controller · failed · Sep 24, 2000 · N250YV · Emb EMB120ER · Flight Controller
  > CAPTAIN''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 OFF
- [SDR SWIA971865](https://openairdocs.org/sdr/SWIA971865.md): Rccb · failed · Jul 4, 2000 · N250YV · Emb EMB120ER · DC Generating System
  > WHEN 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 A
- [SDR SWIA971847](https://openairdocs.org/sdr/SWIA971847.md): Actuator · malfunctioned · Jun 28, 2000 · N250YV · Emb EMB120ER · Landing Gear Actuator
  > ON 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, LEAK

Next page: https://openairdocs.org/deregistered/N250YV-2008-08-27/reports.md?page=2

## 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 = 'N250YV' AND deregistration_id = 'N250YV-2008-08-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N250YV-2008-08-27/reports

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