# N190SW: 1987 Embraer EMB-120, registration cancelled 2006-03-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 22, 2006 - Exported to: Nigeria - Status when cancelled: Triennial form not returned - Airframe: [Embraer EMB-120](https://openairdocs.org/model/embraer-emb-120) (registry code 3260201) - 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: 120.050 - Year built: 1987 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: October 1, 1987 - Certificate issued: October 1, 1987 - Last registry action: April 19, 2005 - Mode S code: A169D0 - 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/N190SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=190SW - Page: https://openairdocs.org/deregistered/N190SW-2006-03-22 From the FAA registry file of October 28, 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-120: https://openairdocs.org/model/embraer-emb-120.md ## Service difficulty reports (106, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWIA200515947](https://openairdocs.org/sdr/SWIA200515947), Dec 4, 2005: ACTUATOR. MALFUNCTIONED. RT RUDDER JAMMED AFTER TAKEOFF. REPLACED LOWER RUDDER ACTUATOR AND RIGGED IAW MM 27-22-02 AND 27-20-00. OPERATIONAL CHECK GOOD. - [SDR SWIA200515399](https://openairdocs.org/sdr/SWIA200515399), Aug 2, 2005: ACTUATOR. MALFUNCTIONED. AFTER ADDING FLAPS TO 25 DEGREES ON FINAL APPROACH, NOTICED RIGHT ROLLING TENDANCY. REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD IAW MM 27-50-0 - [SDR SWIA200514800](https://openairdocs.org/sdr/SWIA200514800), Mar 29, 2005: WIRE. BROKEN. EXIT SIGN ABOVE F/A JUMPSEAT WILL NOT ILLUMINATE. REPAIRED BROKEN WIRE AT FIXTURE, OPERATIONAL CHECK GOOD. - [SDR SWIA200514729](https://openairdocs.org/sdr/SWIA200514729), Mar 14, 2005: WIRE. BROKEN. EMERGENCY EXIT LIGHT AT ROW 9 OVERHEAD INOPERATIVE. REPAIRED BROKEN WIRE AT OVERHEAD BIN AT 9A FOR EMERGENCY EXIT LIGHT AS REQUIRED. OPERATIONAL CHECK GOOD. - [SDR SWIA200514669](https://openairdocs.org/sdr/SWIA200514669), Mar 3, 2005: LIGHT. INOPERATIVE. AFT SECTION OF EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED AFT OVERHEAD LIGHT SOCKET AS NECESSARY, OPERATIONAL CHECK GOOD. - [SDR SWIA200414310](https://openairdocs.org/sdr/SWIA200414310), Dec 24, 2004: SELECTOR. FAULTY. WHEN FLAP LEVER WAS MOVED, CONTROL FAULT MESSAGE. REMOVED AND REPLACED FLAP SELECTOR IAW EMB MM 22-50-01. OPERATIONAL CHECK GOOD. - [SDR SWIA200414305](https://openairdocs.org/sdr/SWIA200414305), Dec 21, 2004: ACTUATOR. MALFUNCTIONED. RECEIVED CONTROL FAULT ON APPROACH WHEN SELECTING FLAPS 25 DEGREES. REMOVED AND REPLACED RIGHT INBOARD, RIGHT NACELLE, AND RIGHT OUTBOARD FLAP ACTUATORS IAW EMB - [SDR SWIA200413862](https://openairdocs.org/sdr/SWIA200413862), Sep 28, 2004: LAMP. BURNED OUT. FRONT CABIN EXIT LIGHT NEAR MAIN CABIN DOOR IS INOPERATIVE. RELAMPED AS REQUIRED, OPERATIONAL CHECK GOOD. - [SDR SWIA200413707](https://openairdocs.org/sdr/SWIA200413707), Aug 13, 2004: DUCT. LOOSE. LEFT PACK MAKES A SQUEALING SOUND WITH LOW SELECTED. IN FLIGHT, PACK CREATES A HOT, SMOKEY SMELL UNTIL TURNED OFF. TIGHTENED CLAMPS AT LEFT PACK. COULD NOT DUPL - [SDR SWIA200413599](https://openairdocs.org/sdr/SWIA200413599), Jul 18, 2004: SIGNAL COND UNIT. MALFUNCTIONED. ON T/O ROLL, RIGHT ENGINE AUTO-FEATHERED DURING POWER LEVER ADVANCEMENT. REMOVED AND REPLACED RIGHT HAND ENGINE TORQUE SIGNAL CONDITIONER IAW MM 77-11-01. OPERA - [SDR SWIA200413555](https://openairdocs.org/sdr/SWIA200413555), Jul 3, 2004: WIRE. BROKEN. EMERGENCY LIGHT ON OVERHEAD BIN ROW 9 DOESN'T ILLUMINATE. REPAIRED WIRING TO EMERGENCY LIGHT ON OVERHEAD BIN. OPERATIONAL CHECK GOOD. - [SDR SWIA200413225](https://openairdocs.org/sdr/SWIA200413225), Apr 24, 2004: BATTERY PACK. INOPERATIVE. REAR SECTION EMERGENCY LIGHTS DOES NOT ILLUMINATE. REPLACED AFT ELBP WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 17366-04-001, S/N OFF 397. - [SDR SWIA200413144](https://openairdocs.org/sdr/SWIA200413144), Apr 1, 2004: ANNUNCIATOR. MALFUNCTIONED. ON THE GROUND WITH FLAP LEVER AT UP POSITION, CONTROL FAULT, FLAP AND ADVANCED SWS APPEAR INTERMITTENTLY. REPLACED FLAP ANNUNCIATOR IAW MM 20-21-00, MM 27-50-05 - [SDR SWIA200412959](https://openairdocs.org/sdr/SWIA200412959), Jan 21, 2004: FLOOR SUPPORT. CRACKED. UNDER FLOOR PANEL 243 DF BRACKET BUCKLED AND CRACKED. DISCOVERED DURING C-CHECK INSPECTION. FITTED AND INSTALLED NEW FLOOR SUPPORT BRACKET. P/N: 120-14243-001. - [SDR SWIA200412958](https://openairdocs.org/sdr/SWIA200412958), Jan 21, 2004: FRAME. CRACKED. CHANNEL CRACKED FORWARD OF FRAME NR 1 ON RIGHT ENGINE NACELLE AT TOP INBOARD SIDE AT UPPER NUT PLATE STRIP. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOA - [SDR SWIA200412957](https://openairdocs.org/sdr/SWIA200412957), Jan 21, 2004: FRAME. CRACKED. CRACK ON CENTER FRAME RIB BELOW E-BRAKE VALVE BOX INBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. PERFORMED REPAIR ON CENTER FRAME RIB BELOW E-BRAKE VALVE B - [SDR SWIA200412862](https://openairdocs.org/sdr/SWIA200412862), Jan 20, 2004: LIGHT. INOPERATIVE. ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB IN ENTRYWAY. OPS CHECKS GOOD. - [SDR SWIA200312702](https://openairdocs.org/sdr/SWIA200312702), Dec 9, 2003: SELECTOR. MALFUNCTIONED. ON DESCENT INTO SGU- LOW SPEED ALARM WENT OFF AND WOULD NOT STOP DESPITE NO ICING CONDITIONS AND ONLY STANDARD ICE ON. LANDED IN SGU WITHOUT INCIDENT AND WHEN T - [SDR SWIA200312531](https://openairdocs.org/sdr/SWIA200312531), Oct 22, 2003: WIRE HARNESS. FAULTY. WHEN SELECTING THE GEAR DOWN, ONLY THE RIGHT MAIN EXTENDED. RIGHT GREEN B-LIGHT AND ALL DISAGREEMENTS ILLUMINATED. THE ELECTRICAL OVER RIDE PROCEDURE IN THE QRH - [SDR SWIA200312427](https://openairdocs.org/sdr/SWIA200312427), Sep 17, 2003: APU. LEAKING. CAPT REPORTS SMOKE IN COCKPIT FROM AIR CONDITIONING SYSTEM. BOTH LT AND RT AIR CONDITIONING PACKS ARE COVERED IN OIL. APU BLEED SYSTEM IS PUTTING OIL INTO PACKS - [SDR SWIA200312307](https://openairdocs.org/sdr/SWIA200312307), Aug 24, 2003: SERVO. MALFUNCTIONED. WITH AUTOPILOT ENGAGED ON EITHER C/A OR F/O SIDE, AP MAKES UNCOMMANDED SLOW ROLL LEFT OR RIGHT. AUTOPILOT FAIL LIGHT ON MAP DOES NOT ILLUMINATE. REMOVED AND REP - [SDR SWIA200312114](https://openairdocs.org/sdr/SWIA200312114), Jun 18, 2003: WIRE. BROKEN. WHITE EMERGENCY TRACK LIGHTING A-BEAM GALLEY INOP, SINGLE LIGHT. INSPECTED AND FOUND BROKEN WIRE. REPAIRED BROKEN WIRE ON WHITE EMERGENCY LIGHT TRACK A-BEAM GAL - [SDR SWIA200311835](https://openairdocs.org/sdr/SWIA200311835), Mar 17, 2003: FCU. MALFUNCTIONED. FLAP CONTROL FAULT FOR INBOARD FLAPS UPON RETRACTING FLAPS AFTER LANDING. REMOVED AND REPLACED FLAP ANNUNCIATOR PANEL AND FCU FOR TROUBLESHOOTING. RAN FLAPS UP - [SDR SWIA200311833](https://openairdocs.org/sdr/SWIA200311833), Mar 15, 2003: CONNECTOR. DAMAGED. FLAP CONTROL FAULT INDICATED FOR INBOARD FLAPS. FLAPS WOULD NOT RETRACT ON THE GROUND. REMOVED AND REPLACED CONNECTOR FOR LEFT INBOARD FLAP ACTUATOR WITH A NEW - [SDR SWIA200311759](https://openairdocs.org/sdr/SWIA200311759), Jan 31, 2003: BUSHING. LACK OF LUBE. BOTH AIR CONDITIONING PACKS FAILED IN THE NORMAL POSITION. SMOKE FILLED THE CABIN AND COCKPIT. VERY LIMITED AIRFLOW IN LOW/LOW CONFIGURATION. LUBRICATED LEFT AN - [SDR SWIA200211597](https://openairdocs.org/sdr/SWIA200211597), Dec 17, 2002: WIRE HARNESS. MALFUNCTIONED. ON TAKEOFF COULDN'T GET THE LANDING GEAR TO GO UP. ALL THE LIGHTS WOULD BE ON BUT THE LEFT RED A. RETURNED TO FAT. REMOVED AND REPLACED LEFT MAIN GEAR A-PROXIMI - [SDR SWIA200211409](https://openairdocs.org/sdr/SWIA200211409), Oct 30, 2002: PUMP. FLUCTUATES. AUX FEATHER PUMP BROKEN, RT ENGINE TORQUE FLUCTUATES 3 PERCENT TO 4 PERCENT AT CRUISE. REMOVED AND REPLACED AUX FEATHER PUMP. - [SDR SWIA200211371](https://openairdocs.org/sdr/SWIA200211371), Oct 26, 2002: TERMINAL BLOCK. LOOSE. MULTIPLE FAILURES ASSOCIATED WITH THE AHAR: HSI ROTATES 60 DEGREES-BOTH SIDES THEN CENTERS ADI-COMPUTER FAILURE LT SIDE ASSOCIATED WITH A GYRO FLAG RIGHT SIDE C - [SDR SWIA200211372](https://openairdocs.org/sdr/SWIA200211372), Oct 17, 2002: CONTROL UNIT. MALFUNCTIONED. DURING CLIMB, RIGHT NP DROPPED TO 96 PERCENT. TURNED OFF EEC WITH POWER LEVER AT FLIGHT IDLE AND CL MAX T6 780, TORQUE 97 PERCENT AND NP 56 PERCENT. WE FEATHERE - [SDR SWIA200211115](https://openairdocs.org/sdr/SWIA200211115), Aug 2, 2002: RECEIVER. FAILED. WHILE HOLDING AT WYS, ADF FAILED IN FLIGHT. DIVERTED TO IDA. REPLACED ADF RECEIVER. OPS CHECKS GOOD IAW MM 34-53-00. - [SDR SWIA200211081](https://openairdocs.org/sdr/SWIA200211081), Jul 26, 2002: BRAKE. SEIZED. ON TAXI OUT THE OUTBOARD RIGHT MAIN TIRE POPPED. FOUND NR 4 BRAKE LOCKED UP. REMOVED AND REPLACED NR 4 BRAKE IAW MM 32-41-05. LEAK CHECKS GOOD. - [SDR SWIA200211004](https://openairdocs.org/sdr/SWIA200211004), Jun 30, 2002: SERVO. BINDING. RUDDER PEDALS FEEL LIKE RUDDERS ARE BINDING UP. INSTALLED SERVICEABLE SVO65 AUTOPILOT SERVO. OPS CHECKS GOOD. - [SDR SWIA200210916](https://openairdocs.org/sdr/SWIA200210916), Jun 8, 2002: COMPUTER. MALFUNCTIONED. AUTOPILOT/YAW FAILURE IN FLIGHT. INSTALLED SERVICEABLE AHC85 COMPUTER. OPS CHECKS GOOD. CAPTAIN'S COMPUTER AND GYRO FLAGS ARE INTERMITTENT IN FLIGHT. INSTALLED - [SDR SWIA200210826](https://openairdocs.org/sdr/SWIA200210826), May 2, 2002: ACTUATOR. FAILED. IN CRUISE FLIGHT, FLAP LIGHT ON MAP PANEL ILLUMINATED ALONG WITH ADVANCED SWS LIGHT. FLAP INBOARD LIGHTS WERE ILLUMINATED. COMPLIED WITH QRH PROCEDURES. FLAPS W - [SDR SWIA200210804](https://openairdocs.org/sdr/SWIA200210804), Apr 14, 2002: COMPUTER. FAULTY. FIRST OFFICER'S EHSI TURNED 30-40 DEGREES RIGHT WHILE CLIMBING STRAIGHT OUT. FIRST OFFICER'S RMI HEADING INFORMATION MATCHES CAPTAIN'S EHSI, RMI AND MAGNETIC CO - [SDR SWIA200210810](https://openairdocs.org/sdr/SWIA200210810), Apr 13, 2002: COMPUTER. MALFUNCTIONED. DURING CLIMBOUT, FIRST OFFICER'S HEADING INDICATOR STARTED STICKING WITH A 30 DEGREE DIFFERENCE BETWEEN HI'S WITH NO ASSOCIATED FLAGS OR ALARMS. AFTER TURNING B - [SDR SWIA200210726](https://openairdocs.org/sdr/SWIA200210726), Mar 13, 2002: WIRE. LOOSE. EMERGENCY LIGHTS IN FLOOR TRACK WILL NOT ILLUMINATE. SECURED LOOSE WIRE AT CONNECTION BELOW FLOOR AT ROW 3. EMERGENCY LIGHTS, OPS CHECK OK. - [SDR SWIA200210728](https://openairdocs.org/sdr/SWIA200210728), Feb 16, 2002: CONTROL CABLE. CORRODED. LEFT RUDDER AFT OUTBOARD AND INBOARD CABLES SHOW SIGNS OF CORROSION. REPLACED LEFT RUDDER AFT OUTBOARD AND INBOARD CABLES IAW EMB120 MM 27-00-01. - [SDR SWIA200210727](https://openairdocs.org/sdr/SWIA200210727), Feb 16, 2002: CONTROL CABLE. CORRODED. RIGHT OUTBOARD AFT ELEVATOR CABLE AND RIGHT AND LEFT AFT ELEVATOR TRIM CABLES SHOWING SIGNS OF WEAR AND CORROSION. REPLACED RIGHT OUTBOARD AFT ELEVATOR CABLE AN - [SDR SWIA200210667](https://openairdocs.org/sdr/SWIA200210667), Feb 12, 2002: ANNUNCIATOR. FAULTY. FLAPS INOP - ALL CONTROL FAULT, DISAGREEMENT AND ASYMMETRY LIGHTS ON. COULD NOT CLEAR ANY OF THE FAULT LIGHTS. FLAP CONTROL PANEL FLAP PORTION INDICATOR (ALL) I - [SDR SWIA200210577](https://openairdocs.org/sdr/SWIA200210577), Jan 19, 2002: TAIL CONE. OUT OF POSITION. CONTROL YOKE BINDS ABOUT HALFWAY THROUGH FORWARD AND AFT TRAVEL WITH ELEVATOR TRIM IN THE GREEN ARC. BIND IS LESS WITH ELEVATOR TRIM FULL FORWARD AND GOES AWAY - [SDR SWIA200110344](https://openairdocs.org/sdr/SWIA200110344), Nov 8, 2001: TIMER. MALFUNCTIONED. LEFT ENGINE AIR INLET FAILED 14 MINUTES INTO FLIGHT PASSING THROUGH FL180. TURNED OFF FOR A FEW MINUTES AND THEN ON FOR ANOTHER 14 MINUTES DURING RETURN TO SLC - [SDR SWIA200110317](https://openairdocs.org/sdr/SWIA200110317), Nov 3, 2001: HARNESS. FAULTY. AFTER GEAR RETRACTION, RIGHT MAIN GEAR B-GREEN LIGHT REMAINS ILLUMINATED WITH ALL OTHER LIGHTS OUT. RECYCLED GEAR WITH SAME RESULT. B-GREEN LIGHT DID FINALLY GO - [SDR SWIA200110305](https://openairdocs.org/sdr/SWIA200110305), Oct 29, 2001: ACTUATOR. FAILED. CONTROL FAULT WOULD NOT RESET PER QRH. INBOARD FLAPS SHOWED 10 DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR PER MM 27-50-00. OPS CHECK, LEAK CHECKS - [SDR SWIA200110311](https://openairdocs.org/sdr/SWIA200110311), Oct 24, 2001: DOOR. MISSING. LEFT HYDRAULIC DOOR MISSING. (DISCOVERED ON WALK AROUND INSPECTION.) FIT AND INSTALLED A NEW LEFT HYDRAULIC BAY DOOR IAW EMB SRM 51-00-00 AND 51-40-02. - [SDR SWIA200110266](https://openairdocs.org/sdr/SWIA200110266), Oct 24, 2001: ROLLER. WORN. CONTROL FAULT ON INBOARD FLAPS. FOUND CONTAMINATION IN INBOARD ACTUATOR CANNON PLUGS. ALSO FOUND WORN ROLLERS ON LEFT INBOARD FLAP. CLEANED CANNON PLUGS AND REM - [SDR SWIA200110236](https://openairdocs.org/sdr/SWIA200110236), Oct 9, 2001: ACTUATOR. FAILED. CONTROL FAULT ON FLAPS ON TAKEOFF. REPLACED INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPS AND LEAK CHECK GOOD. - [SDR SWIA200110235](https://openairdocs.org/sdr/SWIA200110235), Oct 8, 2001: SWITCH. INOPERATIVE. FIRST OFFICER'S PTT SWITCH INOP. RETURNED TO SLC. INSTALLED NEW SWITCH. FIRST OFFICER'S PTT OPS CHECK GOOD. - [SDR SWIA200110199](https://openairdocs.org/sdr/SWIA200110199), Sep 22, 2001: PROXIMITY SENSOR. FAILED. ABORTED TAKEOFF WHEN WE BROUGHT THE POWER UP DUE TO TAKEOFF TRIM WARNING. TRIM CONFIRMED SET AT 4 IN THE GREEN BAND.REMOVED AND REPLACED LEFT TRIM PROXIMITY SEN - [SDR SWIA200110193](https://openairdocs.org/sdr/SWIA200110193), Sep 20, 2001: EEC. MALFUNCTIONED. LEFT EEC WENT TO MANUAL ON TAKEOFF POWER UP. ABORTED TAKEOFF.RESET LEFT EEC. OPS CHECK GOOD. All 106: https://openairdocs.org/deregistered/N190SW-2006-03-22/reports.md ## FAA accident and incident reports (1) 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 19920925044899I](https://openairdocs.org/incident/19920925044899I), Sep 25, 1992: Emb EMB120 (N190SW), Billings, MT. Left main gear doors failed to close after departure. Returned. Landed safely. ## Other aircraft with N190SW - [Registered now](https://openairdocs.org/aircraft/N190SW): Hawker Beechcraft HAWKER 900XP, S/N HA-0079, built 2008 --- 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.