# N463CA: 1992 Embraer EMB-120RT, registration cancelled 2013-09-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 6, 2013 - Exported to: South Africa - Status when cancelled: Valid registration - Airframe: [Embraer EMB-120RT](https://openairdocs.org/model/embraer-emb-120rt) (registry code 3260202) - Engine: [Pratt & Whitney Canada PW118A](https://openairdocs.org/engine/pratt-whitney-canada-pw118a) (registry code 52214) - Data sheets: [TCDS A31SO](https://openairdocs.org/tcds/A31SO), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs) - Serial number: 120.267 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: October 23, 2009 - Certificate issued: June 26, 2006 - Last registry action: July 13, 2011 - Mode S code: A5A4F3 - Owners when cancelled: [Tatonduk Outfitters Ltd DBA Everts Air Alaska DBA](https://openairdocs.org/faa-owner/TATONDUK%20OUTFITTERS%20LTD%20DBA%20EVERTS%20AIR%20ALASKA%20DBA), [Everts Air Cargo](https://openairdocs.org/faa-owner/EVERTS%20AIR%20CARGO) - Location: [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks) - Owner type: Corporation - Owner's area on the map: 64.0097° N, 144.6830° W: Placed by OpenAirDocs at the center of ZIP code 99706, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N463CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=463CA - Page: https://openairdocs.org/deregistered/N463CA-2013-09-06 From the FAA registry file of November 3, 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-120RT: https://openairdocs.org/model/embraer-emb-120rt.md ## Service difficulty reports (92, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COMA0210027](https://openairdocs.org/sdr/COMA0210027), Jun 17, 2002: ROLLER. WORN. FLIGHT 6043 FLAP DISAGREEMENT WARNING AFTER T/O.REPLACED WORN ROLLERS ON R/H OUTBD FLAP. - [SDR COMA0210026](https://openairdocs.org/sdr/COMA0210026), Jun 15, 2002: GENERATOR. FLIGHT 5067 #1 GENERATOR FAILED AFTER T/O.DEFERRED MAINT ON #1 GENERATOR PER MEL. - [SDR COMA0210022](https://openairdocs.org/sdr/COMA0210022), May 23, 2002: ENGINE. FLIGHT 5067 - DURING CRUISE FLIGHT, DESTINATION EYW THE RIGHT ENGINE WAS SHUT DOWN DUE TO LOSS OF OIL PRESSURE.REPLACED THE RIGHT ENGINE ASSEMBLY DUE TO HOT SEC - [SDR COMA0210013](https://openairdocs.org/sdr/COMA0210013), Apr 7, 2002: VALVE. MALFUNCTIONED. FLIGHT 5069 CABIN VERY HOT A/C SYSTEM NOT WORKING.REPLACED THE L/H TEMP CONTROL VALVE. - [SDR COMA0110159](https://openairdocs.org/sdr/COMA0110159), Dec 3, 2001: GYRO. FLIGHT #5049 - AFTER T/O, RED FD FLAP ON PILOTS AND COPILOTS EADI.COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE. - [SDR COMA0110145](https://openairdocs.org/sdr/COMA0110145), Sep 25, 2001: CIRCUIT BREAKER. FLIGHT #5057. DURING PRE-FLIGHT CREW DISCOVERED THE CIRCUIT BREAKER FOR THE FLIGHT IDLE STOP SOLENOID TRIPPED.PERFOMRED RESET AND OPERATIONAL CHECK OF THE FLIGH - [SDR COMA0110143](https://openairdocs.org/sdr/COMA0110143), Sep 22, 2001: INDICATOR. FAULTY. FLIGHT #5017. DURING TAKE OFF AT MCO THE LEFT ENGINE DIGITAL TORQUE INDICATION WAS INTERMITTENT, TAKE OFF WAS ABORTED AND REUTRNED TO THE GATE.REPLACED THE LEFT - [SDR COMA0110137](https://openairdocs.org/sdr/COMA0110137), Aug 29, 2001: COMPUTER. FAULTY. FLIGHT #5005. DURING TAXI OUT RECEIVED A HEADING COMPUTER WARNING, AIRCRAFT RETURNED TO THE GATE.REPLACED THE AHC-85. - [SDR COMA0110130](https://openairdocs.org/sdr/COMA0110130), Apr 18, 2001: SILL. CORRODED. DURING 2C-CHECK TASK 141-01Z, THE AFT LEFT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICE - [SDR COMA0110129](https://openairdocs.org/sdr/COMA0110129), Apr 18, 2001: SKIN. GOUGED. DURING 2 YEAR CORROSION CHECK TASK 5310-132-C01E, THE LOWER RH FUSELAGE SKIN WAS FOUND GOUGED JUST BELOW THE LAV DUMP VALVE DOUBLER. THE SKIN WAS REPAIRED PER E - [SDR COMA0110128](https://openairdocs.org/sdr/COMA0110128), Apr 18, 2001: STRINGER. DENTED. DURING 2C-CHECK TASK 5410-442-04I, THE RIGHT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE DENTED BY THE GEAR DOOR TENSIONER. THE STRINGER WAS REPLACED PER EMB - [SDR COMA0110127](https://openairdocs.org/sdr/COMA0110127), Apr 18, 2001: SUPPORT. CRACKED. DURING 2C-CHECK TASK 5710-652-01I, THE RIGHT WING UPPER SKIN SUPPORT ON RIB NR 21, BETWEEN STRINGERS NR 2 AND 3, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS R - [SDR COMA0110126](https://openairdocs.org/sdr/COMA0110126), Apr 18, 2001: SKIN. CRACKED. DURING 2C-CHECK (NO SPECIFIC TASK APPLIES), THE LEFT NACELLE FLAP LOWER SKIN WAS FOUND TO BE CRACKED AT ACCESS PANEL NR 436AB CUTOUT. THE NACELLE FLAP WAS REMOV - [SDR COMA0110125](https://openairdocs.org/sdr/COMA0110125), Apr 18, 2001: SUPPORT. CRACKED. DURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB NR 21, BETWEEN FRONT SPAR AND STRINGER NR 2, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS - [SDR COMA0110124](https://openairdocs.org/sdr/COMA0110124), Apr 18, 2001: SUPPORT. CRACKED. DURING 2C-CHECK 5720-552-01I, THE LEFT WING UPPER SKIN SUPPORT AT RIB 21, BETWEEN STRINGER NR 2 AND 3, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REMOVED AND - [SDR COMA0110123](https://openairdocs.org/sdr/COMA0110123), Apr 18, 2001: FLOOR SUPPORT. CRACKED. DURING 2C-CHECK TASK 5310-121-01I, THE LEFT FUSELAGE FLOOR PROP AT FRAME NR 13 WAS FOUND TO BE CRACKED. THE FLOOR PROP WAS REPAIRED PER EMB-120 SRM STANDARD PRA - [SDR COMA0110122](https://openairdocs.org/sdr/COMA0110122), Apr 18, 2001: FLOOR SUPPORT. CRACKED. DURING 2C-CHECK TASK 5310-122-01I, THE RIGHT FUSELAGE FLOOR PROP AT FRAME NR 13 WAS FOUND TO BE CRACKED. THE FLOOR PROP WAS REPAIRED PER EMB-120 SRM STANDARD PR - [SDR COMA0110121](https://openairdocs.org/sdr/COMA0110121), Apr 18, 2001: ANGLE. CRACKED. DURING 2C-CHECK TASK 5320-243-01I, THE LEFT WING UPPER SKIN ATTACH ANGLE FOR FAIRING NR 193 WAS FOUND TO BE CRACKED. THE ANGLE WAS REPAIRED PER EMB-120 SRM STAN - [SDR COMA0110120](https://openairdocs.org/sdr/COMA0110120), Apr 18, 2001: SHEAR TIE. CRACKED. DURING 2C-CHECK TASK 232-01Z, THE RIGHT FUSELAGE SKIN SUPPORT AT FRAME NR 13A AND STRINGER NR 14R, WAS FOUND TO BE CRACKED. THE SUPPORT WAS REPAIRED PER EMB-120 - [SDR COMA0110119](https://openairdocs.org/sdr/COMA0110119), Apr 18, 2001: SHEAR TIE. CRACKED. DURING 2C-CHECK TASK 221-01Z, THE LEFT FUSELAGE SKIN SUPPORT JUST BEHIND CAPTAIN''S DV WINDOW, BETWEEN FRAMES 12A AND 23, WAS FOUND TO BE CRACKED. THE SUPPORT W - [SDR COMA0110118](https://openairdocs.org/sdr/COMA0110118), Apr 18, 2001: BRACKET. CRACKED. DURING 2C-CHECK TASK 262-01Z, THE AFT CARGO DOOR TRACK UPPER MOUNTING BRACKET WAS FOUND TO BE CRACKED. THE BRACKET WAS REPLACED PER EMB-120 SRM STANDARD PRACTIC - [SDR COMA0110117](https://openairdocs.org/sdr/COMA0110117), Apr 18, 2001: CHANNEL. CRACKED. DURING 2C-CHECK TASK 811-02Z, THE CHANNEL INSIDE THE PASSENGER DOOR WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110116](https://openairdocs.org/sdr/COMA0110116), Apr 18, 2001: SHEAR TIE. CRACKED. DURING 2C-CHECK TASK 221-01Z, THE FUSLEAGE SKIN SUPPORT ON LEFT SIDE OF COCKPIT AT FRAME NR 9 WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-120 - [SDR COMA0110115](https://openairdocs.org/sdr/COMA0110115), Apr 18, 2001: SHEAR TIE. CRACKED. DURING 2C-CHECK TASK 222-01Z, THE FUSELAGE SKIN SUPPORT ON RIGHT SIDE OF COCKPIT AT FRAME NR 9 WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED PER EMB-12 - [SDR COMA0110114](https://openairdocs.org/sdr/COMA0110114), Apr 18, 2001: CHANNEL. CRACKED. DURING 2C-CHECK TASK 811-02Z, THE U-CHANNEL INSIDE THE PASSENGER DOOR WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110113](https://openairdocs.org/sdr/COMA0110113), Apr 18, 2001: SILL. CORRODED. DURING 2-C CHECK TASK 164-01Z, THE AFT RIGHT FLOOR SUPPORT SILL INSIDE THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STA - [SDR COMA0110112](https://openairdocs.org/sdr/COMA0110112), Apr 18, 2001: SILL. CORRODED. DURING 2C-CHECK TASK 162-01Z, THE FORWARD RIGHT FLOOR SUPPORT SILL INSIDE THE CARGO COMPARTMENT WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM - [SDR COMA0110111](https://openairdocs.org/sdr/COMA0110111), Apr 18, 2001: STRAP. CORRODED. DURING 2-C CHECK TASK 152-01Z, THE AFT RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STAND - [SDR COMA0110110](https://openairdocs.org/sdr/COMA0110110), Apr 18, 2001: STRAP. CORRODED. DURING 2-C CHECK TASK 152-01Z, THE AFT RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STAND - [SDR COMA0110109](https://openairdocs.org/sdr/COMA0110109), Apr 18, 2001: STRAP. CORRODED. DURING 2C-CHECK TASK 151/152-01Z, THE AFT CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM S - [SDR COMA0110108](https://openairdocs.org/sdr/COMA0110108), Apr 18, 2001: STRAP. CORRODED. DURING 2C-CHECK TASK 151-01Z, THE AFT LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDAR - [SDR COMA0110107](https://openairdocs.org/sdr/COMA0110107), Apr 18, 2001: STRAP. CORRODED. DURING 2C-CHECK TASK 141-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTIC - [SDR COMA0110106](https://openairdocs.org/sdr/COMA0110106), Apr 18, 2001: STRAP. CORRODED. DURING 2C-CHECK TASK 141-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PR - [SDR COMA0110105](https://openairdocs.org/sdr/COMA0110105), Apr 18, 2001: STRAP. CORRODED. DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD P - [SDR COMA0110104](https://openairdocs.org/sdr/COMA0110104), Apr 18, 2001: STRAP. CORRODED. DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EM-120 SRM STANDARD PR - [SDR COMA0110103](https://openairdocs.org/sdr/COMA0110103), Apr 18, 2001: SILL. CORRODED. DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110102](https://openairdocs.org/sdr/COMA0110102), Apr 18, 2001: SILL. CORRODED. DURING 2C-CHECK TASK 142-01Z, THE RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110101](https://openairdocs.org/sdr/COMA0110101), Apr 18, 2001: SUPPORT. CORRODED. DURING 2C-CHECK TASK 243-01Z, THE LEFT SIDEWALL SUPPORT SECTION INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORTING SECTION WAS REPLACED PER EMB-120 SRM S - [SDR COMA0110100](https://openairdocs.org/sdr/COMA0110100), Apr 18, 2001: STRAP. CORRODED. DURING 2C-CHECK TASK 132-01Z, THE RIGHT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD P - [SDR COMA0110099](https://openairdocs.org/sdr/COMA0110099), Apr 18, 2001: STRAP. CORRODED. DURING 2C-CHECK TASK 131/132-01Z, THE CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STAND - [SDR COMA0110098](https://openairdocs.org/sdr/COMA0110098), Apr 18, 2001: STRAP. CORRODED. DURING 2C-CHECK TASK 131-01Z, THE LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 SRM STANDARD PR - [SDR COMA0110097](https://openairdocs.org/sdr/COMA0110097), Apr 18, 2001: STRAP. CORRODED. DURING 2C-CHECK TASK 131-01Z, THE FORWARD LEFT FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER SRM STANDARD PR - [SDR COMA0110096](https://openairdocs.org/sdr/COMA0110096), Apr 18, 2001: STRAP. CORRODED. DURING 2C-CHECK TASK 131/132-01Z, THE FORWARD CENTER FLOOR SUPPORT BUTTSTRAP INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE BUTTSTRAP WAS REPLACED PER EMB-120 S - [SDR COMA0110095](https://openairdocs.org/sdr/COMA0110095), Apr 18, 2001: SILL. CORRODED. DURING 2C-CHECK TASK 132-01Z, THE FOWARD RIGHT FLOOR SUPPORT SILL INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED PER EMB-120 SRM STANDARD PRAC - [SDR COMA0110094](https://openairdocs.org/sdr/COMA0110094), Apr 18, 2001: SUPPORT. CORRODED. DURING 2C-CHECK TASK 232-01Z, THE FORWARD RIGHT SIDEWALL SEAT TRACK SUPPORT INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORT WAS REPLACED PER EMB-120 SRM - [SDR COMA0110093](https://openairdocs.org/sdr/COMA0110093), Apr 18, 2001: SUPPORT. CORRODED. DURING 2C-CHECK TASK 242-01Z, THE RIGHT SIDEWALL SEAT TRACK SUPPORT INSIDE THE CABIN WAS FOUND TO BE CORRODED. THE SUPPORT WAS REPLACED PER EMB-120 SRM STANDARD - [SDR COMA0110092](https://openairdocs.org/sdr/COMA0110092), Apr 18, 2001: FLOORBEAM. CORRODED. DURING 2C-CHECK TASK 131-01Z, THE FORWARD LEFT FLOOR SUPPORT T-SECTION AT FRAME 16 INSIDE THE CABIN ,WAS FOUND TO BE CORRODED. THE T-SECTION WAS REPLACED PER EM - [SDR COMA0110091](https://openairdocs.org/sdr/COMA0110091), Apr 18, 2001: CROSSBEAM. CORRODED. DURING 2C-CHECK TASK 151-01Z, THE LEFT FLOOR SUPPORT CROSSBEAM AT FRAME 36, INSIDE THE CABIN, WAS FOUND TO BE CORRODED. THE CROSSBEAM WAS REPLACED PER EMB-120 S - [SDR COMA0110090](https://openairdocs.org/sdr/COMA0110090), Apr 18, 2001: DOOR FRAME. CORRODED. DURING 2C-CHECK TASK 811-02Z, THE PASSENGER DOOR LOWER LONGITUDINAL FRAME, WAS FOUND TO BE CORRODED. THE FRAME WAS REPLACED PER EMB-120 SRM STANDARD PRACTICES. - [SDR COMA0110089](https://openairdocs.org/sdr/COMA0110089), Apr 18, 2001: ANGLE. CORRODED. DURING 2C-CHECK TASK 131/132-01Z, THE FUSELAGE FORWARD FLOOR SUPPORTING Z-SECTION AT FRAME 13 WAS FOUND TO BE CORRODED. THE Z-SECTION WAS REPLACED PER EMB-120 S All 92: https://openairdocs.org/deregistered/N463CA-2013-09-06/reports.md ## 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 20020523019639I](https://openairdocs.org/incident/20020523019639I), May 23, 2002: Emb EMB120RT (N463CA), Orlando, FL. (-23) Climbing through 10,000 ft there was a drop in np on the #2 engine. Shortly after the drop in np on the #2 engine the oil press dropped to 0. The #2 oil… - [Incident 20000924016639I](https://openairdocs.org/incident/20000924016639I), Sep 24, 2000: Emb EMB120RT (N463CA), Orlando, FL, Minor damage. (-23) Attached incident narrative ## Other aircraft with N463CA - [Registered now](https://openairdocs.org/aircraft/N463CA): Textron 182T, S/N 18283297, built 2025 --- 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.