# N207SW: 1992 Embraer EMB-120ER, registration cancelled 2005-01-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 10, 2005 - Exported to: Australia - 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: 120.266 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: February 11, 1994 - Certificate issued: August 3, 1998 - Last registry action: August 17, 2004 - Mode S code: A1ADA9 - Owner when cancelled: [First Union Commercial Corporation](https://openairdocs.org/faa-owner/FIRST%20UNION%20COMMERCIAL%20CORPORATION) - Location: [Charlotte, NC](https://openairdocs.org/faa-place/NC/Charlotte) - Owner type: Corporation - Owner's area on the map: 35.2273° N, 80.8442° W: Placed by OpenAirDocs at the center of ZIP code 28202, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N207SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=207SW - Page: https://openairdocs.org/deregistered/N207SW-2005-01-10 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 (38) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWIA200312698](https://openairdocs.org/sdr/SWIA200312698), Dec 12, 2003: STRINGER. CRACKED. STRINGER NR 8 AT RIB 5 CRACKED. DISCOVERED DURING A CHECK INSPECTION. REPAIRED STRINGER IAW EMB SRM 57-20-03 AND GST 3176/02. - [SDR SWIA200312627](https://openairdocs.org/sdr/SWIA200312627), Nov 21, 2003: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ROW 1-4 INOP. REPLACED BATTERY PACK. OP CHECK OK. - [SDR SWIA200312514](https://openairdocs.org/sdr/SWIA200312514), Oct 11, 2003: PEDAL. RESTRICTED. AFTER ROTATION, RT RUDDER PEDAL RESTRICTED, WITH ABOUT 1 INCH OF MOVEMENT. RAN QRH JAMMED RUDDER PROCEDURE, TURNED OFF BLUE SYSTEM AND NORMAL RUDDER TRAVEL RETU - [SDR SWIA200311784](https://openairdocs.org/sdr/SWIA200311784), Feb 12, 2003: PROXIMITY SENSOR. MALFUNCTIONED. ABORTED TAKEOFF WITH AURAL WARNING. REPOWERED AIRCRAFT AND DID A COMPLETE AURAL WARNING SYSTEM RESET. NOW IT WILL NOT PASS A STATIC TEST. REPLACED LEFT PROXIMIT - [SDR SWIA200311665](https://openairdocs.org/sdr/SWIA200311665), Jan 1, 2003: WARNING SYSTEM. FALSE ACTIVATION. HIGH SPEED WARNING ON TAKEOFF AT 60 KIAS. ABORTED TAKEOFF. THIS HAPPENED TWICE. PERFORMED TEST PROCEDURES FOR BOTH AIRSPEED INDICATORS AND OVERSPEED WARNINGS. A - [SDR SWIA200211405](https://openairdocs.org/sdr/SWIA200211405), Oct 30, 2002: BOOT. TORN. RIGHT AND LEFT OUTBOARD STAB AND VERT FIN BOOTS INOP AFTER 28 SECONDS ON TIMERS 1 & 2. RETURNED TO DEN. REPLACED LEFT HORIZONTAL STAB DEICE BOOT IAW MM CHAPTER - [SDR SWIA200211226](https://openairdocs.org/sdr/SWIA200211226), Aug 13, 2002: RIB. DAMAGED. RIB IN RUDDER 1 DAMAGED JUST BELOW GREEN RUDDER ACTUATOR ATTACH POINT. DISCOVERED DURING C-CHECK. REPLACED DAMAGED RIB IAW 120 SRM 51-10-02. - [SDR SWIA200210940](https://openairdocs.org/sdr/SWIA200210940), Jun 2, 2002: SENSOR. MALFUNCTIONED. TAKEOFF TRIM AURAL WARNING FAILURE. ABORTED TAKEOFF. REPLACED BOTH LEFT AND RIGHT ELEVATOR TRIM SENSORS. RAN BOTH ENGINES TO TAKEOFF POWER SETTINGS AND ALL TRIM - [SDR SWIA200210525](https://openairdocs.org/sdr/SWIA200210525), Jan 4, 2002: SKIN. CRACKED. CRACK IN SKIN AROUND FWD CORNER OF RT SIDE COCKPIT SIDE WINDOW. DISCOVERED DURING ROUTINE LINE INSPECTION. INSTALLED REPAIR DOUBLER PER SB 120-053-0010. - [SDR SWIA200110431](https://openairdocs.org/sdr/SWIA200110431), Dec 11, 2001: ACTUATOR. FAILED. AFTER TAKEOFF A FLAP DISAGREEMENT OCCURRED. TWO SEGMENTS OF THE INBOARD PAIR WERE ILLUMINATED AND 1 BAR OF THE NACELLE AND OUTBOARD PAIR FLASHED. DISAGREEMENT C - [SDR SWIA200110174](https://openairdocs.org/sdr/SWIA200110174), Sep 15, 2001: SELECTOR SWITCH. MALFUNCTIONED. FLAPS WILL NOT MOVE WHEN 45 DEGREES IS SELECTED.REMOVED AND REPLACED FLAP SELECTOR LEVER IAW MM 27-50-01. OPS CHECK GOOD IAW 27-50-00. - [SDR SWIA972484](https://openairdocs.org/sdr/SWIA972484), Apr 5, 2001: SWITCH. OUT OF ADJ. ON TAKEOFF FORWARD DOOR LIGHT BLINKED ON WITH WARNING. ADJUSTED THE MICROSWITCH FOR THE FORWARD DOOR LIGHT. OPS CHECK GOOD. - [SDR SWIA972471](https://openairdocs.org/sdr/SWIA972471), Mar 29, 2001: PROXIMITY SENSOR. FAILED. ELEVATOR TRIM AURAL WARNING CONTINUOUS IN OR OUT OF TRIM. REMOVED AND REPLACED LEFT ELEVATOR TRIM PROXIMITY SENSOR WITH NEW IAW EMB MM 27-32-00. P/N 922AA2Y-A6P - [SDR SWIA972304](https://openairdocs.org/sdr/SWIA972304), Jan 21, 2001: SPRING. LACK OF LUBE. ELEVATOR MOVEMENT PRODUCES ABNORMAL SOUNDS, SOUNDS LIKE CABLES PRANGING. LUBED ELEVATOR RETURN SPRING FWD ATTACH POINT. SYSTEM CHECK OK. - [SDR SWIA972154](https://openairdocs.org/sdr/SWIA972154), Dec 7, 2000: CONTROLLER. FAILED. DESCENDING FROM FLIGHT LEVEL 260 CABIN ALTITUDE LIGHT ILLUMINATED ON THE MAP. LOST CONTROL OF CABIN ALTITUDE IN BOTH AUTO AND MANUAL MODES. MASKS DROPPED. PRESS - [SDR SWIA972120](https://openairdocs.org/sdr/SWIA972120), Nov 11, 2000: WARNING SYSTEM. ACTIVATED. TAKEOFF TRIM ALARMED, ABORTED TAKEOFF. RAN BOTH ENGINES TO TEST TAKEOFF TRIM ALARM. TAKEOFF TRIM OPS CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY. - [SDR SWIA972119](https://openairdocs.org/sdr/SWIA972119), Nov 11, 2000: SEQUENCE VALVE. FAILED. LEFT LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LEFT MAIN GEAR OUTBOARD SEQUENCE VALVE IAW MM 32-32-07. CYCLED GEAR SEVERAL TIMES. OPS CHECK GOOD. P/N - [SDR SWIA972090](https://openairdocs.org/sdr/SWIA972090), Nov 10, 2000: LANDING GEAR. CONTAMINATED. LEFT LANDING GEAR WOULD NOT RETRACT. RETURNED TO COD. INSPECTED LEFT LANDING GEAR. CLEANED OFF SNOW AND ICE. SWUNG LANDING GEAR OVER 10 TIMES IAW 32-30-00. LAND - [SDR SWIA972040](https://openairdocs.org/sdr/SWIA972040), Oct 17, 2000: COMPUTER. MALFUNCTIONED. ON CLIMBOUT CLACKER WARNING ACTIVATED FOR DURATION OF FLIGHT. RETURNED TO SLC. REPLACED STALL WARNING COMPUTER AND TESTED IAW MM 27-34-02. REPLACED STALL PANEL - [SDR SWIA972038](https://openairdocs.org/sdr/SWIA972038), Oct 14, 2000: REGULATOR. FAILED. RIGHT DUCT LEAK LIGHT ON INFLIGHT. FOLLOWED QRH AND LIGHT DID NOT GO OUT AFTER 3 MINUTES. SHUT DOWN RIGHT ENGINE AND RETURNED TO SLC. TROUBLESHOOT RIGHT BLEED A - [SDR SWIA971919](https://openairdocs.org/sdr/SWIA971919), Aug 6, 2000: ENGINE. MALFUNCTIONED. DURING TAKEOFF ROLL, RECEIVED T6 WARNING BEFORE V1. ABORTED TAKEOFF. PERFORMED STATIC RUN UP AND RECEIVED T6 WARNING ON RIGHT ENGINE AT 90 PERCENT TORQUE WITH B - [SDR SWIA971892](https://openairdocs.org/sdr/SWIA971892), Jul 22, 2000: CONTROL BOX. FAILED. RED A SYSTEM GEAR LIGHTS ILLUMINATED DURING FLIGHT WITH GEAR UP. RETURNED TO SLC. REPLACED GEAR CONTROL BOX WITH SERVICEABLE ASSY, OPS CHECK GOOD IAW 32-60-00. - [SDR SWIA971717](https://openairdocs.org/sdr/SWIA971717), Feb 29, 2000: SWITCH. FAILED. SERVICE DOOR LIGHT ILLUMINATED IN FLIGHT. RETURNED TO PSP. INSPECTED FUEL DOOR SWITCH, AVIONICS BAY SWITCH AND RIGGING DOOR SWITCH. ALL SWITCHES CHECK GOOD. COU - [SDR SWIA971633](https://openairdocs.org/sdr/SWIA971633), Dec 20, 1999: SWITCH. DAMAGED. GREEN SYSTEM MAIN PUMP LOW PRESSURE LIGHT AND LOW LEVEL LIGHT ILLUMINATED WITHIN A FEW SECONDS OF EACH OTHER. QUANTITY INDICATOR FOR GREEN SYSTEM INDICATED EMPT - [SDR SWIA971512](https://openairdocs.org/sdr/SWIA971512), Jul 9, 1999: FILTER. DIRTY. RIGHT HYDRAULIC FILTER LIGHT ILLUMINATED. RETURNED TO SLC. REPLACED HIGH AND LOW PRESSURE FILTERS ON RIGHT PACK. OPS AND LEAKS CHECK GOOD. - [SDR SWIA971463](https://openairdocs.org/sdr/SWIA971463), Apr 5, 1999: HYD SYST. REQD SERVICE. SHORTLY AFTER TAKEOFF REACHING CRUISE ALTITUDE THE LEFT HYDRAULIC RESERVOIR LOW PRESSURE LIGHT CAME ON AND WAS ACCOMPANIED BY A FLUID QUANTITY INDICATION IN MID - [SDR SWIA971342](https://openairdocs.org/sdr/SWIA971342), Dec 21, 1998: ACTUATOR. FAILED. NACELLE FLAP DISAGREEMENT AT 2 BARS ON DEPARTURE. RETURNED TO SLC. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-08 AND OPS CHECKS GOOD. - [SDR SWIA971289](https://openairdocs.org/sdr/SWIA971289), Oct 15, 1998: ACTUATOR. MALFUNCTIONED. UNABLE TO RETRACT FLAPS, DISAGREEMENT. RETURNED TO SLC. REMOVED AND REPLACED RIGHT WING INBOARD FLAP ACTUATOR, OPS CHECKS GOOD. - [SDR SWIA971271](https://openairdocs.org/sdr/SWIA971271), Sep 7, 1998: TQ SENSOR. MALFUNCTIONED. AFTER TAKEOFF RIGHT TORQUE GAUGE OSCILLATED BETWEEN 40 PERCENT AND 100 PERCENT AND THEN FEATHERED INADVERTENTLY. RETURNED TO FIELD, REMOVED AND REPLACED TORQUE - [SDR SWIA971031](https://openairdocs.org/sdr/SWIA971031), Nov 15, 1997: AHRS COMPUTER. MALFUNCTIONED. CAPTAINS ATTITUDE DISPLAY FAILED. RETURNED TO FIELD. REPLACED NR 1 AHRS COMPUTER. OPS CHECKS GOOD. - [SDR SWIA97824](https://openairdocs.org/sdr/SWIA97824), Jan 12, 1997: CLAMP. LOOSE. RIGHT ENGINE AIR INLET DE-ICE INOP. RETURNED TO FIELD AFTER TAKEOFF. TIGHTENED CLAMP ON RIGHT ENGINE INLET DE-ICE BOOT SUPPLY LINE, OPS CHECKS GOOD. - [SDR SWIA95767](https://openairdocs.org/sdr/SWIA95767), Sep 30, 1996: HOSE. CHAFED. AT CRUISE ALTITUDE, RIGHT OIL PRESSURE DROPPED TO 40 PSI. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN ON RIGHT ENGINE. REMOVED AND REPLACED UPPER HOSE ASSY ON RIGH - [SDR SWIA95701](https://openairdocs.org/sdr/SWIA95701), Dec 25, 1995: SEAL. LOOSE. CLIMBING THROUGH 24,000 FEET, CABIN ALTITUDE LIGHT CAME ON. TESTED ALTITUDE WARNING SWITCH SYSTEM IAW MM 21-30-08. SYSTEM OPERATION CHECKS GOOD. FOUND CARGO DOO - [SDR SWIA95698](https://openairdocs.org/sdr/SWIA95698), Dec 17, 1995: BLADE TIP. DAMAGED. VIBRATION ON CLIMB-OUT FROM SLC, FOUND RT PROPELLER DAMAGED, ALL ENGINE PARAMETERS WERE NORMAL FOR TAKEOFF AND CLIMB. FOUND DAMAGED TO NR TWO BLADE TIP. PROPELL - [SDR SWIA95620](https://openairdocs.org/sdr/SWIA95620), Aug 28, 1995: OIL SYST. REQD SERVICE. AFTER ROTATION, RT OIL PRESSURE FLUCTUATED TO AROUND 40 PSI AND OIL AURAL WARNING SOUNDED. OIL PRESSURE IMMEDIATELY RETURNED AND MAINTAINED NORMAL PSI. SERVICED - [SDR SWIA95597](https://openairdocs.org/sdr/SWIA95597), Jul 13, 1995: REG VLV GASKET. FAILED. FIVE MINUTES AFTER TAKEOFF USING ONLY APU BLEED X FEED TO BOTH PACS, RT DUCT LEAK LIGHT, ILLUMINATED, TURNED OFF X FEED AND RT PAC, STARTED TIME AS PER CHECK LI - [SDR SWIA95580](https://openairdocs.org/sdr/SWIA95580), May 13, 1995: HYD PUMP. FAILED. LOST ALL HYDRAULIC PRESSURE IN FLIGHT, LOW PRESSURE ELECTRICAL STANDBY FAILED TO OPERATE. REPLACED A BROKEN RETURN LINE AT ENGINE PUMP IN THE LEFT HYDRAULICS BA - [SDR SWIA95522](https://openairdocs.org/sdr/SWIA95522), Feb 8, 1995: WHEEL. CRACKED. NR 1 MAIN WHEEL CRACKED. REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY. SEE FL 73942 FOR MECH SIGN OFF. ## 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 19980812027189I](https://openairdocs.org/incident/19980812027189I), Aug 12, 1998: Emb EMB120ER (N207SW), Salt Lake City, UT. After takeoff the right rudder pedal jammed, no travel past neutral. Pilot in command attempted to use rudder trim wheel and yaw to no avial. Aircrafat… - [Incident 19951217046249I](https://openairdocs.org/incident/19951217046249I), Dec 17, 1995: Emb EMB120ER (N207SW), Salt Lake City, UT, Minor damage. Narrative: aircraft returned to slc due to abnormal vibrations. Aircraft landed without incident. It appeared that a propeller blade, on number two engine, hit… ## Other aircraft with N207SW - [Registered now](https://openairdocs.org/aircraft/N207SW): Jonathan D Ross W-10 TAILWIND, S/N 429 --- 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.