# N205CA: 1990 Embraer EMB-120ER, registration cancelled 2009-02-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 11, 2009 - Exported to: Bermuda - Status when cancelled: Valid registration - 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: 120.205 - Year built: 1990 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: February 16, 2000 - Certificate issued: August 19, 2008 - Last registry action: August 19, 2008 - Mode S code: A1A4C9 - Owner when cancelled: [Bank Of Utah](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N205CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=205CA - Page: https://openairdocs.org/deregistered/N205CA-2009-02-11 From the FAA registry file of November 5, 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 (42) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COMA9810180](https://openairdocs.org/sdr/COMA9810180), Aug 18, 1998: BATTERY. DISCHARGED. AFT SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY. - [SDR COMA9810171](https://openairdocs.org/sdr/COMA9810171), Aug 6, 1998: DOOR. NOT LATCHED. SERVICE DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR UNLATCHED. SECURED DOOR CLOSED AND AIRCRAFT RETURNED TO SERVICE. - [SDR COMA9810150](https://openairdocs.org/sdr/COMA9810150), Jul 1, 1998: SWITCH. DIRTY. AUTOFEATHER SYSTEM INOPERABLE DURING TAKEOFF. CLEANED THE AUTOFEATHER ARMING SWITCHES IN POWER LEVER QUADRANT. - [SDR COMA9810120](https://openairdocs.org/sdr/COMA9810120), May 13, 1998: SIGN. LOOSE. EXIT SIGN LOOSE AT ROW 5A. REPLACED EXIT SIGN. - [SDR COMA9810108](https://openairdocs.org/sdr/COMA9810108), Apr 22, 1998: T/O WARNING. MALFUNCTION. 'TRIM' AURAL WARNING DURING TAKEOFF. REPLACED THE AUDIO WARNING UNIT. - [SDR COMA9810078](https://openairdocs.org/sdr/COMA9810078), Mar 25, 1998: ACTUATOR. MALFUNCTUATING. OUTBOARD FLAP INDICATION IS FLUCTUATING BETWEEN 2 AND 7 UNITS. COULD NOT DUPLICATE DISCREPANCY. REPLACED RIGHT HAND OUTBOARD FLAP ACTUATOR FOR TROUBLESHOOTING. - [SDR COMA9810015](https://openairdocs.org/sdr/COMA9810015), Jan 7, 1998: CROSSBEAM. CORRODED. 2C TASK 532D-147-03I REVEALED RIGHT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICEABLE PART USING EMB 120 STANDARD PRACT - [SDR COMA9810014](https://openairdocs.org/sdr/COMA9810014), Jan 7, 1998: CROSSBEAM. CORRODED. 2C TASK 151-01Z REVEALED LEFT CROSSBEAM TO BE CORRODED AT FRAME 33. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 STANDARD PRACTICES. - [SDR COMA9810009](https://openairdocs.org/sdr/COMA9810009), Jan 7, 1998: CROSSBEAM. CORRODED. 2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 23 TO BE CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 STANDARD - [SDR COMA9810008](https://openairdocs.org/sdr/COMA9810008), Jan 7, 1998: CROSSBEAM. CORRODED. DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING - [SDR COMA9810007](https://openairdocs.org/sdr/COMA9810007), Jan 7, 1998: CROSSBEAM. CORRODED. DURING 2C INSPECTION TASK 5310-131-01I REVEALED CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICABLE CROSSBEAM USING EMB 120 - [SDR COMA9810006](https://openairdocs.org/sdr/COMA9810006), Jan 7, 1998: SILL. CORRODED. DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CABIN SILL RIGHT TO BE HEAVILY CORRODED. REMOVED CORRODED SILL AND INSTALLED SERVICABLE SILL USING EMB 120 - [SDR COMA9810005](https://openairdocs.org/sdr/COMA9810005), Jan 7, 1998: BUTTSTRAP. CORRODED. DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRAP AND INSTALLED SERVICABLE BUTTSTRAP USING EMB 1 - [SDR COMA9810004](https://openairdocs.org/sdr/COMA9810004), Jan 7, 1998: BUTTSTRAP. CORRODED. DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CENTER BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRAP AND INSTALLED SERVICABLE BUTTSTRAP USIN - [SDR COMA9810013](https://openairdocs.org/sdr/COMA9810013), Jan 6, 1998: CROSSBEAM. CORRODED. 2C TASK 532D-147-03I REVEALED RIGHT CENTER CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICEBLE PART USING EMB 120 STANDARD - [SDR COMA9810012](https://openairdocs.org/sdr/COMA9810012), Jan 6, 1998: CROSSBEAM. CORRODED. 2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICABLE PART USING EMB 120 STANDARD PRACTIC - [SDR COMA9810011](https://openairdocs.org/sdr/COMA9810011), Jan 6, 1998: CROSSBEAM. CORRODED. 2C TASK 5320-147-03I REVEALED CROSSBEAM (RIGHT) AT FRAME 23 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB STANDARD PRACTICES. - [SDR COMA9810010](https://openairdocs.org/sdr/COMA9810010), Jan 6, 1998: CROSSBEAM. CORRODED. 2C INSPECTION TASK 5310-131-01I REVEALED THAT THE RIGHT CROSSBEAM AT FRAME 16 WAS CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USIN - [SDR COMA9810003](https://openairdocs.org/sdr/COMA9810003), Jan 6, 1998: BUTTSTRAP. CORRODED. DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED PART AND INSTALLED SERVICEABLE PART USING EMB 120 - [SDR COMA9810002](https://openairdocs.org/sdr/COMA9810002), Jan 6, 1998: FRAME T-SECTION. CORRODED. DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT MIDDLE T-SECTION AT FRAME 16 TO BE HEAVILY CORRODED. REMOVED CORRODED T-SECTION AND INSTALLED SERVICABLE T - [SDR COMA9710483](https://openairdocs.org/sdr/COMA9710483), Nov 26, 1997: SOLENOID. SHORTED. ON 1C TASK 35-09, THE OXYGEN MASKS AT ROW 9 FAILED TO DEPLOY. INVESTIGATION FOUND THE OXYGEN MASK DOOR SOLENOID TO BE SHORTED. THE SOLENOID WAS REPLACED WITH A - [SDR COMA9710467](https://openairdocs.org/sdr/COMA9710467), Oct 31, 1997: RELAY BOX. MALFUNCTIONED. SMOKE IN COCKPIT AND CABIN AFTER PUSH BACK. FOUND GROUND COOLING FANS NOT OPERATING. REPLACED THE LANDING GEAR RELAY BOX. - [SDR COMA9710333](https://openairdocs.org/sdr/COMA9710333), Jul 17, 1997: PCU. DAMAGED. PCU ASSEMBLY REMOVED FROM AIRCRAFT FOR AD 95-22-12 COMPLIANCE. UPON INITIAL RECEIVING INSPECTION SEVERAL OF THE FORWARD PORTION OF THE SPLINES WERE FOUND TO BE - [SDR COMA9710315](https://openairdocs.org/sdr/COMA9710315), Jun 17, 1997: RADAR ANTENNA. FAILED. WEATHER RADAR DOES NOT WORK. REPLACED THE ANTENNA. - [SDR COMA9710298](https://openairdocs.org/sdr/COMA9710298), May 24, 1997: ACTUATOR. MALFUNCTION. FLAP CONTROL FAULT WARNING WITH FLAPS RETRACTED. REPLACED THE LT OUTBOARD FLAP ACTUATOR. - [SDR COMA9710276](https://openairdocs.org/sdr/COMA9710276), May 19, 1997: SKIN. BIRD STRIKE. BIRD STRIKE ON LOWER FUSELAGE. INSPECTED EXTERIOR OF AIRCRAFT AND FOUND NO EVIDENCE OF BIRD STRIKE. - [SDR COMA9710262](https://openairdocs.org/sdr/COMA9710262), May 8, 1997: FLAP CONTL UNIT. MALFUNCTIONED. FLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP CONTROL UNIT. - [SDR COMA9610338](https://openairdocs.org/sdr/COMA9610338), Dec 3, 1996: DEICE BOOTS. WORN. LT AND RT WING DEICE BOOTS AND LT AND RT ENGINE INLET DEICE BOOTS FAILED DURING FLIGHT. REPLACED WING AND ENGINE INLET DEICE BOOTS. - [SDR COMA9610298](https://openairdocs.org/sdr/COMA9610298), Oct 8, 1996: SIGN. MISSING. EMERGENCY EXIT SIGN AT ROW 5 IS MISSING. REPLACED EMERGENCY EXIT SIGN. - [SDR COMA9610263](https://openairdocs.org/sdr/COMA9610263), Aug 27, 1996: FLAP CONTL UNIT. MALFUNCTION. FLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 2,052. - [SDR COMA9610158](https://openairdocs.org/sdr/COMA9610158), Jun 1, 1996: PROPELLER. LEAKING. LEFT ENGINE LEAKED A LARGE AMOUNT OF OIL DURING TAXI FROM HANGAR TO GATE. REPLACED THE LT PROPELLER ASSY. - [SDR COMA9610137](https://openairdocs.org/sdr/COMA9610137), Apr 26, 1996: CONTROL VALVE. FAILED. LEFT INLET BOOT FAILED IN-FLIGHT. REPLACED LEFT INLET DEICE EJECTOR VALVE. - [SDR COMA9610116](https://openairdocs.org/sdr/COMA9610116), Mar 28, 1996: WIRE. CHAFED. RT HYDRAULIC RESERVOIR LOW PRESSURE INDICATOR ILLUMINATED. REPAIRED CHAFED WIRE AT PRESSURE SWITCH. - [SDR COMA9610095](https://openairdocs.org/sdr/COMA9610095), Mar 7, 1996: CONTROL BOX. MALFUNCTION. LANDING GEAR INTRANSIT LIGHTS REMAINED ON WITH GEAR RETRACTED. REPLACED THE LANDING GEAR CONTROL BOX. - [SDR COMA9610084](https://openairdocs.org/sdr/COMA9610084), Feb 17, 1996: FLAP TRACKS. DIRTY. FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. CLEANED AND INSPECTED FLAP TRACKS AND OPERATIONAL CHECK NORMAL. - [SDR COMA9610046](https://openairdocs.org/sdr/COMA9610046), Jan 28, 1996: ANNUNCIATOR. DEFECTIVE. TAKEOFF FLAPS AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE FLAP ANNUNCIATOR UNIT. - [SDR COMA9512035](https://openairdocs.org/sdr/COMA9512035), Dec 20, 1995: IVA-81A AV. DEFECTIVE. THE PILOTS VSI IS COMPLETELY UNUSABLE IN ALL PHASES OF FLIGHT. REPLACED THE PILOTS TCASIVSI. - [SDR COM11936](https://openairdocs.org/sdr/COM11936), Jul 27, 1995: TQ SIG COND. DEFECTIVE. LEFT TORQUE INDICATION ERRATIC. LEFT PROPELLER AUTOFEATHERED. REPLACED THE TORQUE SIGNAL CONDITIONER. - [SDR COM11924](https://openairdocs.org/sdr/COM11924), Jun 28, 1995: AHRS. DEFECTIVE. PILOTS ESHI SHOWS RED FLAG. REPLACED THE NR NR 1 AHRS. - [SDR COM11859](https://openairdocs.org/sdr/COM11859), Apr 13, 1995: ENGINE. FAILED. LEFT ENGINE FAILED ABRUPTLY IN FLIGHT. REMOVED AND REPLACED LEFT ENGINE. - [SDR COM11843](https://openairdocs.org/sdr/COM11843), Mar 30, 1995: SKIN SUPPORT. CRACKED. THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERODE - [SDR COM11838](https://openairdocs.org/sdr/COM11838), Mar 27, 1995: SENSOR. DEFECTIVE. NLG A SYSTEM INTRANSIT LIGHT IS ILLUMINATING INTERMITTENTLY. REPLACED THE NLG DOWNLOCK PROXIMITY SENSOR. ## Other aircraft with N205CA - [Registered now](https://openairdocs.org/aircraft/N205CA): Cessna 402C, S/N 402C0207, built 1979 --- 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.