# N593SW: 1990 Embraer EMB-120, registration cancelled 2004-08-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 27, 2004 - Exported to: South Africa - Status when cancelled: Valid registration - 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: 120.191 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: July 21, 1990 - Certificate issued: August 19, 2004 - Last registry action: August 19, 2004 - Mode S code: A7AA31 - Owner when cancelled: [International Aviation Support](https://openairdocs.org/faa-owner/INTERNATIONAL%20AVIATION%20SUPPORT) - Location: [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas) - Owner type: Corporation - Owner's area on the map: 32.9619° N, 96.8993° W: Placed by OpenAirDocs at the center of ZIP code 75006, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N593SW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=593SW - Page: https://openairdocs.org/deregistered/N593SW-2004-08-27 From the FAA registry file of November 4, 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 (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SWIA200312073](https://openairdocs.org/sdr/SWIA200312073), Jun 4, 2003: SWITCH. MALFUNCTIONED. WHEN FLAPS 15 WERE SELECTED FCU INDICATES CONTROL FAULT WITH FLAP AND ASWS LIGHTS ON MAP. REMOVED AND REPLACED FLAP HANDLE WITH A SERVICEABLE UNIT. OPS CHECK GO - [SDR SWIA200311895](https://openairdocs.org/sdr/SWIA200311895), Apr 3, 2003: SWITCH. MALFUNCTIONED. WITH FLAPS SELSECTED TO 15 DEGREES FLAP CONTROL FAULT. REMOVED AND REPLACED FLAP SELECTOR HANDLE WITH SERVICEABLE UNIT. RAN FLAPS FULL SCALE MULTIPLE TIMES. OPS - [SDR SWIA200311775](https://openairdocs.org/sdr/SWIA200311775), Feb 7, 2003: CONTROL UNIT. MALFUNCTIONED. ON TAKEOFF THE ANALOG FLAP INDICATOR BOUNCED BACK AND FORTH BETWEEN 0-15 DEGREES, SETTING OFF THE TAKEOFF AURAL WARNING SYSTEM. ALSO, EACH TIME IT WENT TO 0 DEG - [SDR SWIA200311705](https://openairdocs.org/sdr/SWIA200311705), Jan 9, 2003: ENGINE. MALFUNCTIONED. ON CLIMBOUT HEARD AND FELT A LOUD THUMP AND SLIGHT LOSS OF POWER ON THE LEFT ENGINE. ABOUT 30 SECONDS LATER RECEIVED AN 'OIL' MAP AND AURAL WARNING. OIL PRESSUR - [SDR SWIA200211314](https://openairdocs.org/sdr/SWIA200211314), Oct 10, 2002: LOCKWASHER. BROKEN. AFTER DEPARTURE, LEFT MAIN GEAR WOULD NOT RETRACT. RETURNED TO RDM. FOUND TANG BROKEN ON LOCKING WASHER FOR LEFT MAIN LANDING GEAR ACTUATOR. REPLACED TANG WASHE - [SDR SWIA200210961](https://openairdocs.org/sdr/SWIA200210961), Jun 15, 2002: CONTROL PANEL. MALFUNCTIONED. WITH AUTOPILOT SELECTED TO EITHER SIDE AND AUTOPILOT ENGAGED, RECEIVED AN AURAL TRIM FAIL WITH ASSOCIATED MAP LIGHT ON AP PANEL, RED AP & E LIGHTS ILLUMINATED. - [SDR SWIA200210960](https://openairdocs.org/sdr/SWIA200210960), Jun 15, 2002: BATTERY PACK. DISCHARGED. FLOOR LEVEL EMERGENCY LIGHTS AND EXIT LIGHT IN ROW 9 WILL NOT ILLUMINATE. REMOVED AND REPLACED AFT ELBP WITH A SERVICEABLE UNIT. OPS CHECK GOOD. - [SDR SWIA200210754](https://openairdocs.org/sdr/SWIA200210754), Mar 22, 2002: ACTUATOR. MALFUNCTIONED. FLAP CONTROL FAULT ILLUMINATED DURING CRUISE WITH FLAP SELECTOR IN UP POSITION. ANNUNCIATOR PANEL SHOWED SECOND SEGMENTS ONLY OF INBOARD LEFT AND RIGHT FLAPS IL - [SDR SWIA200210744](https://openairdocs.org/sdr/SWIA200210744), Mar 20, 2002: WIRE. CHAFED. AFTER ENGINE START, CONTROL FAULT FLAP AND ADV SWS ILLUMINATED AND WOULD NOT RESET. INSPECTED RIGHT INBOARD WIRE BUNDLE FROM P1756 TO P0366 AND FOUND WIRES CHAF - [SDR SWIA200210722](https://openairdocs.org/sdr/SWIA200210722), Mar 15, 2002: SWITCH. FAILED. LEFT MIDDLE WING DEICE BOOT FAILS DURING CLIMBOUT AT HIGH POWER SETTINGS. RETURNED TO PDX. REPLACED 16 PSI SWITCH FOR LEFT MID WING BOOT PER MM 30-00-00. OPS CH - [SDR SWIA200110397](https://openairdocs.org/sdr/SWIA200110397), Nov 24, 2001: PRESSURE SWITCH. FAILED. LEFT ENGINE INLET DEICE BOOT FAILS IN FLIGHT. REPLACED AND SECURED LEFT INLET DEICE BOOT PRESSURE SWITCH. COMPLIED WITH ENGINE RUN OPS CHECK GOOD. - [SDR SWIA972590](https://openairdocs.org/sdr/SWIA972590), May 24, 2001: PROXIMITY SENSOR. OUT OF ADJ. ON APPROACH TO YUM, LEFT MAIN LANDING GEAR A-SYSTEM RED LIGHT WOULD NOT EXTINGUISH. A-SYSTEM GREEN LIGHT WOULD NOT ILLUMINATE. INSTALLED GEAR PINS AND SECURED. - [SDR SWIA972397](https://openairdocs.org/sdr/SWIA972397), Feb 26, 2001: WINDOW FRAME. CRACKED. WINDOW FRAME CRACKED ON PILOTS SIDE. DISCOVERED DURING LINE INSPECTION. INSTALLED WINDOW FRAME REPAIR ON PILOTS SIDE PER SB 120-053-0010. - [SDR SWIA972052](https://openairdocs.org/sdr/SWIA972052), Oct 19, 2000: FCU. INOPERATIVE. FLAP CONTROL FAULT INBOARD PAIR WILL NOT RESET. REMOVED AND REPLACED FCU IAW MM 27-50-06. S/N: 0013, S/N OFF: 0178. - [SDR SWIA971876](https://openairdocs.org/sdr/SWIA971876), Jul 12, 2000: BULB. FAILED. ENTRANCE EMERGENCY BOARDING LIGHT INOP. INSTALLED NEW MAIN ENTRANCE EMERGENCY BOARDING LIGHT BULB, OPS CHECK GOOD. - [SDR SWIA971736](https://openairdocs.org/sdr/SWIA971736), Mar 13, 2000: ANNUNCIATOR. MALFUNCTIONED. DURING FLIGHT WITH FLAPS UP AT 9000 ADVANCE STALL WARNING SYSTEM AND FLAP LIGHT CAME ON, MAP AND FLAP WARNING INDICATION OVERHEAD DISAGREEMENT, CONTROL FAULT AS - [SDR SWIA971719](https://openairdocs.org/sdr/SWIA971719), Mar 3, 2000: HARNESS. FAILED. RIGHT MAIN FORWARD GEAR DOORS WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO RDM REMOVED AND REPLACED THE A SYSTEM UPLOCK HARNESS (RIGHT MAIN). - [SDR SWIA971585](https://openairdocs.org/sdr/SWIA971585), Oct 15, 1999: RETRACT MECH. DIRTY. FLAP DISAGREEMENT ON TAKEOFF WOULD NOT CLEAR. RETURNED TO RDM. CYCLED FLAPS MULTIPLE TIMES, COULD NOT DUPLICATE PROBLEM. INSPECTED AND CLEANED FLAP TRACKS AND R --- 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.