# N214SW: 1993 Embraer EMB-120ER, registration cancelled 2007-02-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 8, 2007
- Exported to: France
- Status when cancelled: Triennial form not returned
- Airframe: [Embraer EMB-120ER](https://openairdocs.org/model/embraer-emb-120er) (registry code 3260203)
- Engine: [Pratt & Whitney Canada PW118](https://openairdocs.org/engine/pratt-whitney-canada-pw118) (registry code 52116)
- Data sheets: [TCDS A31SO](https://openairdocs.org/tcds/A31SO), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 120.280
- Year built: 1993
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: May 13, 1993
- Certificate issued: May 10, 1993
- Last registry action: May 17, 2005
- Mode S code: A1CA03
- Owner when cancelled: [Skywest Airlines Inc](https://openairdocs.org/faa-owner/SKYWEST%20AIRLINES%20INC)
- Location: [St George, UT](https://openairdocs.org/faa-place/UT/St%20George)
- Owner type: Corporation
- Owner's area on the map: 37.1384° N, 113.6296° W: Placed by OpenAirDocs at the center of ZIP code 84770, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N214SW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=214SW
- Page: https://openairdocs.org/deregistered/N214SW-2007-02-08

From the FAA registry file of October 27, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Embraer EMB-120ER: https://openairdocs.org/model/embraer-emb-120er.md

## Service difficulty reports (70, newest 50)

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

- [SDR SWIA200616291](https://openairdocs.org/sdr/SWIA200616291), Feb 17, 2006: LEVER. MALFUNCTIONED. RECEIVED "TOO LOW FLAPS" AURAL WARNINGS ON APPROACH. REPLACED FLAP SELECTOR LEVER ASSY IAW 27-50-01, OPERATIONAL CHECK GOOD.
- [SDR SWIA200516032](https://openairdocs.org/sdr/SWIA200516032), Dec 26, 2005: ACTUATOR. MALFUNCTIONED. RT RUDDER JAMMED AFTER TAKEOFF. REPLACED BOTH RUDDER ACTUATORS IAW MM 27-22-02. OPERATIONAL CHECK GOOD, PN 308140-1003, SN/OFF 0165 SN/OFF 0671.
- [SDR SWIA200515460](https://openairdocs.org/sdr/SWIA200515460), Aug 23, 2005: CONTROL UNIT. MALFUNCTIONED. ABOVE 160 KTS DURING FLAP RETRACTION OUTBOARD FLAPS DISAGREE (FLAP ON MAP, DISAGREEMENT ON OVERHEAD). REPLACED FLAP CONTROL UNIT IAW A/C MM 27-50-06, OPERATIONA
- [SDR SWIA200515433](https://openairdocs.org/sdr/SWIA200515433), Aug 17, 2005: CONTROL UNIT. MALFUNCTIONED. FLAP CONTROL FAULT ON CLIMB-OUT. REPLACED THE FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW MM 27-50-00.
- [SDR SWIA200515325](https://openairdocs.org/sdr/SWIA200515325), Jul 30, 2005: ANNUNCIATOR. MALFUNCTIONED. ON CLIMB-OUT, GOT A FLAP DISAGREEMENT INDICATION. REPLACED FLAP ANNUNCIATOR PANEL IAW EMB 120 MM 27-50-00. OPERATIONAL CHECK GOOD, PN ON 306900-1017; PN OFF 347
- [SDR SWIA200514932](https://openairdocs.org/sdr/SWIA200514932), Apr 26, 2005: SIGN. INOPERATIVE. RED EMERGENCY FLOOR LIGHTS IN GALLEY INOPERATIVE. REPLACED RED EMERGENCY SIGN AT THE GALLEY FLOOR. OPERATIONAL CHECK GOOD.
- [SDR SWIA200514696](https://openairdocs.org/sdr/SWIA200514696), Mar 11, 2005: DOOR. BINDING. MAIN CABIN DOOR VERY HARD TO OPEN AND CLOSE. ADJUSTED AND RIGGED PAX DOOR BACKSTOP SHIMS IAW EMB 120 MM 52-11-00.
- [SDR SWIA200514697](https://openairdocs.org/sdr/SWIA200514697), Mar 8, 2005: BATTERY PACK. DISCHARGED. AFT SECTION EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED LIGHT BATTERY PACK FOR AFT SECTION. OPERATIONAL CHECK GOOD.
- [SDR SWIA200514992](https://openairdocs.org/sdr/SWIA200514992), Feb 15, 2005: BUTTSTRAP. CORRODED. THERE IS CORROSION ON BUTT STRAP JUST AFT OF PAX DOOR ENTRANCE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED AFFECTED BUTT STRAP AND SECURED SAME IAW EMB 120 MM 5
- [SDR SWIA200414035](https://openairdocs.org/sdr/SWIA200414035), Oct 25, 2004: LAMP. BURNED OUT. PASSENGER ENTRY OVERHEAD EMERGENCY LIGHT DOES NOT ILLUMINATE. RELAMPED PASSENGER ENTRY OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413731](https://openairdocs.org/sdr/SWIA200413731), Aug 20, 2004: COMPUTER. MALFUNCTIONED. LT STALL WARNING LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED LT NR 1 STALL WARNING COMPUTER. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413550](https://openairdocs.org/sdr/SWIA200413550), Jul 6, 2004: ACTUATOR. MALFUNCTIONED. AFTER LANDING SELECTED FLAPS UP, RECEIVED A CONTROL FAULT ON OUTBOARD FLAPS. REMOVED AND REPLACED FLAP ACTUATOR IAW AMM 27-50-00. REPAIRED PIN 4 AT CONNECTOR P1
- [SDR SWIA200413440](https://openairdocs.org/sdr/SWIA200413440), Jun 13, 2004: LIGHT. INOPERATIVE. FORWARD EMERGENCY RED LIGHT STRIP ON FLOOR INOP. REPLACED FORWARD EMERGENCY LIGHT STRIP ON FLOOR WITH SERVICEABLE UNIT. OPS CHECK GOOD.
- [SDR SWIA200413430](https://openairdocs.org/sdr/SWIA200413430), Jun 10, 2004: WINDOW. CRACKED. LEFT CAPTIANS SIDE WINDOW CRACKED ON GROUND. REMOVED AND REPLACED LEFT SIDE WINDSHIELD IAW MM 56-10-01. PN: NP151311-1, S/N OFF: 00108.
- [SDR SWIA200413305](https://openairdocs.org/sdr/SWIA200413305), May 5, 2004: LAMP. INOPERATIVE. EMERGENCY LIGHT AT PAX DOOR CEILING IS INOP. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. P/N: 209.
- [SDR SWIA200413103](https://openairdocs.org/sdr/SWIA200413103), Mar 26, 2004: CONTROL PANEL. MALFUNCTIONED. STALL WARNING LIGHT ILLUMINATES ON THE MAP. REMOVED AND REPLACED STALL PANEL. OPS CHECKS GOOD.
- [SDR SWIA200412858](https://openairdocs.org/sdr/SWIA200412858), Feb 4, 2004: SWITCH. FAILED. DURING CRUISE FLIGHT AT 27,000 FT, HAD A PRESSURE POP AND THEN A CABIN ALT WITH TRIPLE CHIME. PERFORMED PRECAUTIONARY EMERGENCY DESCENT TO 10,000 FT AT THAT POI
- [SDR SWIA200312412](https://openairdocs.org/sdr/SWIA200312412), Sep 13, 2003: WIRE. DISCONNECTED. FORWARD EMERGENCY LIGHT (INOPERATIVE). RECONNECTED BOTH POWER LEADS AT FORWARD (EXIT) SIGN. OPS CHECK GOOD.
- [SDR SWIA200312411](https://openairdocs.org/sdr/SWIA200312411), Aug 25, 2003: CHANNEL. CRACKED. LT MLG INSIDE WELL FORWARD OUTBOARD CRACK ON NACELLE. (DISCOVERED DURING C-CHECK INSPECTION) LT MLG OUTBOARD CHANNEL REPLACED SRM120 51-10-02.
- [SDR SWIA200312206](https://openairdocs.org/sdr/SWIA200312206), Jul 16, 2003: BATTERY PACK. MALFUNCTIONED. EMERGENCY LIGHTS IN ROW 9 COME ON MOMENTARILY AND THEN GO OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 4 IAW MM 33-50-02. OPS CHECK GOOD.
- [SDR SWIA200312112](https://openairdocs.org/sdr/SWIA200312112), Jun 14, 2003: CHANNEL. CRACKED. AFTER DEPARTURE THE FLAPS WOULD NOT RETRACT PAST APPROXIMATELY 10 DEGREES. RECEIVED FLAP DISAGREEMENT WITH THE OUTBOARD FLAPS INDICATING APPROXIMATELY 10 DEGREE
- [SDR SWIA200312094](https://openairdocs.org/sdr/SWIA200312094), Jun 9, 2003: PANEL. MALFUNCTIONED. AFTER TAKEOFF, OUTBOARD FLAPS WOULD NOT COMPLETELY RETRACT AND FLAP DISAGREEMENT INDICATED. QRH, RECYCLED AND WOULD NOT CORRECT. FLAPS CAME DOWN FINE BUT WILL N
- [SDR SWIA200312069](https://openairdocs.org/sdr/SWIA200312069), Jun 3, 2003: FLAP TRACK. DAMAGED. AFTER DEPARTURE FLAPS WOULD NOT RETRACT PAST 10 DEGREES. FLAP DISAGREEMENT WITH THE OUTBOARD FLAPS INDICATING 10 DEGREES. RETURNED TO FIELD. REPLACED RIGHT OUTB
- [SDR SWIA200312058](https://openairdocs.org/sdr/SWIA200312058), Jun 2, 2003: SWITCH. STUCK. PILOT REPORTS THAT RIGHT ENGINE AUTO FEATHERED ON TAKEOFF ROLL WITH LT ENGINE TQ FLUCTUATION, BUT ENGINE DID NOT FOLLOW FLUCTUATION. FOUND LEFT ENGINE AUTO FEAT
- [SDR SWIA200312031](https://openairdocs.org/sdr/SWIA200312031), May 27, 2003: ACTUATOR. MALFUNCTIONED. FLAPS WILL NOT RETRACT FULLY. OUTBOARD FLAPS REMAIN AT ABOUT 10 DEGREES. RETURNED TO SLC. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE PAR
- [SDR SWIA200312009](https://openairdocs.org/sdr/SWIA200312009), May 22, 2003: STRINGER. CRACKED. CRACKED STRINGER LEFT INBOARD WING LOWER SURFACE AFT OF INBOARD FUEL CELL ACCESS PANEL. FOUND DURING A CHECK INSPECTION. COMPLIED WITH WING STRINGER REPAIR AT L
- [SDR SWIA200311919](https://openairdocs.org/sdr/SWIA200311919), Apr 28, 2003: FLAP TRACK. WORN. FLAP DISAGREEMENT AFTER TAKEOFF. OUTBOARD PAIR WOULD NOT RETRACT TO LESS THAN 10 DEGREES, OTHER PAIRS RETRACTED PROPERLY. APPLIED QRH PROCEDURE 3 TIMES, FAILED 
- [SDR SWIA200311915](https://openairdocs.org/sdr/SWIA200311915), Apr 25, 2003: WARNING LIGHT. ILLUMINATED. IN FLIGHT CLIMBING THROUGH 7,000 FEET, THE FLAP DISAGREEMENT LIGHT ILLUMINATED. COULD NOT CLEAR VIA QRH. RETURNED TO SLC. INSPECTED FLAPS. NO DEFECTS FOUND. PER
- [SDR SWIA200311790](https://openairdocs.org/sdr/SWIA200311790), Feb 16, 2003: CONNECTOR. CONTAMINATED. FLAP DISAGREEMENT ON FLAP RETRACTION ON TAKEOFF, OUTBOARD FLAPS. RETURNED TO SLC. INSPECTED OUTBOARD FLAPS CONNECTORS, FOUND GLYCOL IN LEFT OUTBOARD CONNECTOR. 
- [SDR SWIA200311675](https://openairdocs.org/sdr/SWIA200311675), Jan 3, 2003: CONNECTOR. WORN. FLAPS WOULD NOT RETRACT, DISAGREEMENT WITH THE OUTBOARD PAIRS, WOULD NOT CORRECT. FOUND LEFT OUTBOARD FLAP CONNECTOR TO HAVE FLUID INSIDE AND WORN BACKSHELL. RE
- [SDR SWIA200211502](https://openairdocs.org/sdr/SWIA200211502), Nov 22, 2002: SIGNAL COND UNIT. MALFUNCTIONED. NR 2 PROPELLER FEATHERED WHEN TAKEOFF POWER APPLIED. TORQUE REACHED 125 PERCENT INSTANTANEOUSLY. NP 18.9 PERCENT WHEN POWER BROUGHT BACK TO IDLE. REPLACED RIGHT
- [SDR SWIA200211501](https://openairdocs.org/sdr/SWIA200211501), Nov 18, 2002: CONNECTOR. CONTAMINATED. AFTER TAKEOFF, RECEIVED A FLAP DISAGREEMENT WITH 2 BARS ON OUTBOARD FLAPS, AND ALL LIGHTS ON THE 10 DEGREE LINE FLASHING. RESET AS PER QRH. RESET NOT SUCCESSFUL
- [SDR SWIA200211414](https://openairdocs.org/sdr/SWIA200211414), Oct 31, 2002: CONNECTOR. CONTAMINATED. FLAP DISAGREEMENT THAT WOULD NOT CLEAR AFTER TAKEOFF. RETURNED TO SLC. DEICE FLUID FOUND IN OUTBOARD FLAP ACTUATOR CONNECTOR PLUGS. CLEANED CONNECTOR PLUGS. OPS
- [SDR SWIA200211391](https://openairdocs.org/sdr/SWIA200211391), Oct 23, 2002: ANNUNCIATOR. MALFUNCTIONED. FLAP DISAGREEMENT ON TAKEOFF. RECYCLED 3 TIMES - UNSUCCESSFULLY. FLAP DISAGREEMENT ON OUTBOARD PAIR DURING RETRACTION. RETURNED TO DEN. CLEANED AND INSPECTED FL
- [SDR SWIA200211272](https://openairdocs.org/sdr/SWIA200211272), Sep 29, 2002: COMPUTER. MALFUNCTIONED. FO'S EHSI FAILED DURING TAXI AND IN FLIGHT. EHSI SHOWS YELLOW FAIL FLAG AND HEADING FLAG. SUCCESSFULLY RESET BOTH TIMES. REPLACED FO'S HDG74. OPERATIONAL CHECK 
- [SDR SWIA200211271](https://openairdocs.org/sdr/SWIA200211271), Sep 29, 2002: GCU. MALFUNCTIONED. CAPTAIN'S EHSI WENT BLANK ON TAXI OUT. REPLACED GCU NR 1 (AUX GEN NR 1) IAW MM 24-30-02. CHECKED OPERATION OF POWER TRANSFER AT NP 70 PERCENT WITHOUT OBSERVING 
- [SDR SWIA200211229](https://openairdocs.org/sdr/SWIA200211229), Sep 7, 2002: COMPUTER. MALFUNCTIONED. CAPT'S EHIS FAILED AFTER TAKEOFF. RETURNED TO FIELD. REMOVED AND REPLACED THE NR 1 HPU WITH A SERVICEABLE UNIT. OPS CHECK GOOD.
- [SDR SWIA200211067](https://openairdocs.org/sdr/SWIA200211067), Jul 25, 2002: ENGINE. MALFUNCTIONED. RIGHT ENGINE AUTO FEATHERED ON THE TAKEOFF ROLL. ABORTED THE TAKEOFF. PERFORMED TWO TAKEOFF POWER RUNS, ALL CHECKS NORMAL.
- [SDR SWIA200210957](https://openairdocs.org/sdr/SWIA200210957), Jun 8, 2002: CONNECTOR. LOOSE. FIRST OFFICER'S STICK SHAKER NOT WORKING ON FIRST FLIGHT OF THE DAY CHECK. FOUND CONNECTOR LOOSE ON SHAKER UNIT. TIGHTENED CONNECTOR. OPS CHECK PER 27-60-00 GOO
- [SDR SWIA200210905](https://openairdocs.org/sdr/SWIA200210905), Jun 7, 2002: FLAP. MALFUNCTIONED. FLAP DISAGREEMENT IN FLIGHT. RETURNED TO SLC. PERFORMED OPS CHECKS IAW 27-50-00. COULD NOT DUPLICATE DISCREPANCY.
- [SDR SWIA200210913](https://openairdocs.org/sdr/SWIA200210913), Jun 5, 2002: RELAY. FAILED. UPON ADDING POWER ON TAKEOFF, LEFT TORQUE GAUGE WOULD NOT GO ABOVE 75PERCENT, THEN AURAL AUTO FEATHER WARNING SOUNDED AND THE RIGHT ENGINE FEATHERED. UPON PULLI
- [SDR SWIA200210906](https://openairdocs.org/sdr/SWIA200210906), Jun 1, 2002: INDICATOR. ERRATIC. LEFT ENGINE T6 GAUGE ERRATIC. RETURNED TO DEN. REPLACED LEFT T6 GAUGE. OPS CHECK GOOD.
- [SDR SWIA200210815](https://openairdocs.org/sdr/SWIA200210815), Apr 23, 2002: FASTENER. LOOSE. ABORTED TAKEOFF AT 60 KIAS DUE TO A MAP RED DOOR LIGHT ILLUMINATING. FOUND CAMLOCK ON FUEL SERVICE DOOR UNSECURED. SECURED CAMLOCK ON FUEL DOOR. OPS CHECK GOOD.
- [SDR SWIA200210713](https://openairdocs.org/sdr/SWIA200210713), Mar 13, 2002: ACTUATOR. LEAKING. AT 1000 FT AGL AND 10 DEGREES BANK TO THE RIGHT (AFTER TAKEOFF), THE GREEN SYSTEM RESERVOIR LOW LEVEL LIGHT ILLUMINATED WITH HYD ON MAP. THE FLUID QUANTITY NEED
- [SDR SWIA200210714](https://openairdocs.org/sdr/SWIA200210714), Mar 12, 2002: DETECTOR. MALFUNCTIONED. ICE MONITOR FAILED INFLIGHT. RETURNED TO DEN. CYCLED CIRCUIT BREAKER. OPS CHECKED GOOD.
- [SDR SWIA200210615](https://openairdocs.org/sdr/SWIA200210615), Feb 1, 2002: WIRE HARNESS. DEFECTIVE. RT MAIN LANDING GEAR -A- DISAGREEMENT LIGHT ILLUMINATED DURING FLIGHT. ALL -B- LIGHTS FUNCTION NORMAL. REMOVED AND REPLACED -A- UPLOCK HARNESS WITH SERVICEABLE 
- [SDR SWIA200210604](https://openairdocs.org/sdr/SWIA200210604), Jan 29, 2002: TARGET. OUT OF ADJUST. RIGHT GEAR LIGHTS RED A & B WOULD NOT EXTINGUISH WHEN GEAR RETRACTED. CYCLED 3 TIMES. INSPECTED RT MAIN GEAR. FOUND UPLOCK HOOK ADJUSTED OUT, PLUS ICE BUILD UP 
- [SDR SWIA200210590](https://openairdocs.org/sdr/SWIA200210590), Jan 26, 2002: CONNECTOR. CONTAMINATED. ON TAKEOFF, DURING FLAP RETRACTION, RECEIVED A FLAP DISAGREEMENT. FOLLOWED QRH AND FLAPS RETRACTED NORMALLY. COULD NOT DUPLICATE ON GROUND. INSPECTED FLAPS, TRA
- [SDR SWIA200110239](https://openairdocs.org/sdr/SWIA200110239), Sep 21, 2001: FRAME. CRACKED. RIGHT AND LEFT NACELLE NR 1 FRAMES CRACKED. REPLACED BOTH NACELLE NR 1 FRAMES IAW EMB120 SRM 51-10-02 AND SB 120-54-0036.
- [SDR SWIA200110212](https://openairdocs.org/sdr/SWIA200110212), Sep 20, 2001: FCU. MALFUNCTIONED. ON CLIMBOUT RECEIVED A FLAP DISAGREEMENT AND FLAPS WOULD NOT FULLY RETRACT. RETURNED TO FAT. AIRCRAFT IN FOR C CHECK INSPECTION. DETAILS FORTHCOMING. UPDATE: PU

All 70: https://openairdocs.org/deregistered/N214SW-2007-02-08/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DEN03IA054](https://openairdocs.org/ntsb/DEN03IA054), Mar 17, 2003: Embraer EMB-120ER (N214SW), Cedar City, UT, incident, minor damage. Probable cause: the captain's failure to maintain directional control during takeoff. Factors contributing to the accident were the crew's diverted attention, the snow and slush-covered runway, the fog, and the…

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20030316003669I](https://openairdocs.org/incident/20030316003669I), Mar 16, 2003: Emb EMB120ER (N214SW), Cedar City, UT, Minor damage. (-23) Skw 3622 taxied out for takeoff at approximately 22:00 MST. The aircraft was de-iced prior to takeoff with type 1 fluid. Type 1 fluid was the only type…
- [Incident 19980809028999I](https://openairdocs.org/incident/19980809028999I), Aug 9, 1998: Emb EMB120ER (N214SW), Billings, MT. Skywest 736, bil-slc, returned to bil at 1603 MDT after shutting down the left engine. Aircraft landed without incident. Crew reported left bleed air duct…

## Other aircraft with N214SW

- [Registered now](https://openairdocs.org/aircraft/N214SW): John Stone Ware IV RV-14, S/N 140087, built 2016

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