# N264CA: 1992 Embraer EMB-120RT, registration cancelled 2006-10-05 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 5, 2006 - Status when cancelled: Valid registration - Airframe: [Embraer EMB-120RT](https://openairdocs.org/model/embraer-emb-120rt) (registry code 3260202) - 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: 120.256 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: February 7, 1992 - Last registry action: October 5, 2006 - Mode S code: A28E0C - Owner when cancelled: [Mtw Aerospace Inc](https://openairdocs.org/faa-owner/MTW%20AEROSPACE%20INC) - Location: [Montgomery, AL](https://openairdocs.org/faa-place/AL/Montgomery) - Owner type: Corporation - Owner's area on the map: 32.3391° N, 86.4011° W: Placed by OpenAirDocs at the center of ZIP code 36108, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N264CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=264CA - Page: https://openairdocs.org/deregistered/N264CA-2006-10-05 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 (88, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COMA0210029](https://openairdocs.org/sdr/COMA0210029), Jul 18, 2002: LAMP. BURNED OUT. FLIGHT 5047 EMERGENCY LIGHT INOP.REPLACED LIGHT BULB. - [SDR COMA0210015](https://openairdocs.org/sdr/COMA0210015), Apr 12, 2002: BRACKET. CRACKED. DURING AN E-10 PART A INSPECTION THE FUSELAGE SKIN SUPPORT BRACKET (P/N 120-34416-001) ON THE LEFT SIDE JUST BELOW THE PILOTS WINDSHIELD SIDE POST AT FRAME 9 WA - [SDR COMA0210012](https://openairdocs.org/sdr/COMA0210012), Apr 2, 2002: CONTROL BOX. MALFUNCTIONED. FLIGHT 5070 LANDING GEAR CONTROL COULD NOT BE SELECTED TO THE UP POSITION.REPLACED THE L/G CONTROL HANDLE ASSY. - [SDR COMA0210010](https://openairdocs.org/sdr/COMA0210010), Mar 26, 2002: ENGINE. FAILED. FLIGHT 5059 R/H ENGINE FAILED WITH NO WARNINGS. IFSD REPLACED ENGINE. - [SDR COMA0210003](https://openairdocs.org/sdr/COMA0210003), Feb 1, 2002: BATTERY. DISCHARGED. FLIGHT 5044 EMERGENCY FLOOR PATH LIGHTS ARE INOP IN SEVERAL PLACES. REPLACED THE NR 2 EMERGENCY BATTERY. - [SDR COMA0110156](https://openairdocs.org/sdr/COMA0110156), Nov 12, 2001: BATTERY. DISCHARGED. FLIGHT #5044. EMERGENCY LIGHTS ARE INOP.REPLACED THE EMERGENCY LIGHTS BATTERY. - [SDR COMA0110148](https://openairdocs.org/sdr/COMA0110148), Sep 28, 2001: ROLLER. WORN. FLIGHT 5070 FLAP SELECTION BEYOND 25 DEGREES RESULTS IN FLAP DISAGREEMENT WARNING.REPLACED THE R/H OUTBD FLAP ROLLERS. SYSTEM CHECK SATISFACTORY. - [SDR COMA0110139](https://openairdocs.org/sdr/COMA0110139), Aug 26, 2001: INDICATOR. FAULTY. FLIGHT #5053. DURING APPLICATION OF POWER FOR TAKE OFF AT MCO THE #2 NH ANALOG INDICATION FAILED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE NH/NL INDICATOR. - [SDR COMA0110136](https://openairdocs.org/sdr/COMA0110136), Aug 26, 2001: INDICATOR. FAULTY. FLIGHT #5053. DURING APPLICATION OF POWER FOR TAKE OFF AT MCO THE #2 NH ANALOG INDICATION FAILED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE NH/NL INDICATOR. - [SDR COMA0110042](https://openairdocs.org/sdr/COMA0110042), Mar 9, 2001: BOOT. DAMAGED. WING DE-ICE FAIL WARNING. REPAIRED HOLES IN WING LEADING EDGE DE-ICE BOOTS, USING PATCH KIT. - [SDR COMA0110032](https://openairdocs.org/sdr/COMA0110032), Feb 5, 2001: DISPLAY. MALFUNCTIONED. ATTITUDE DISPLAY AND FLIGHT DIRECTOR FAILURE WARNINGS. REPLACED THE NR 2 AHRS. - [SDR COMA0110031](https://openairdocs.org/sdr/COMA0110031), Jan 26, 2001: RESERVOIR. LOW. HYDRAULIC RESERVOIR LOW LEVEL CAUTION. SERVICED HYD RESERVOIR, NO DEFECTS FOUND WITH HYDRAULIC SYSTEM. - [SDR COMA0010377](https://openairdocs.org/sdr/COMA0010377), Nov 10, 2000: BUTTSTRAP. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE FORWARD RH FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUC - [SDR COMA0010376](https://openairdocs.org/sdr/COMA0010376), Nov 10, 2000: BUTTSTRAP. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z THE FORWARD LH FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUC - [SDR COMA0010375](https://openairdocs.org/sdr/COMA0010375), Nov 10, 2000: BUTTSTRAP. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z THE FORWARD CENTER FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-1 - [SDR COMA0010374](https://openairdocs.org/sdr/COMA0010374), Nov 10, 2000: SKIN. GOUGED. UPON COMPLIANCE OF 2 YEAR CORROSION CHECK TASK 5310-132-CO1E THE FUSELAGE SKIN BELOW THE LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REP - [SDR COMA0010402](https://openairdocs.org/sdr/COMA0010402), Nov 10, 2000: SKIN. CHAFED. UPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCT - [SDR COMA0010401](https://openairdocs.org/sdr/COMA0010401), Nov 10, 2000: SKIN. CHAFED. UPON COMPLANCE OF 2C INSPECTION TASK 5410-432-04I THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTUR - [SDR COMA0010400](https://openairdocs.org/sdr/COMA0010400), Nov 10, 2000: SKIN. CHAFED. UPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTU - [SDR COMA0010399](https://openairdocs.org/sdr/COMA0010399), Nov 10, 2000: SKIN. CHAFED. UPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCT - [SDR COMA0010398](https://openairdocs.org/sdr/COMA0010398), Nov 10, 2000: SILL. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z THE LT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR - [SDR COMA0010397](https://openairdocs.org/sdr/COMA0010397), Nov 10, 2000: FLOORBEAM. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT T-SECTION WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL RE - [SDR COMA0010396](https://openairdocs.org/sdr/COMA0010396), Nov 10, 2000: CHANNEL. CRACKED. UPON COMPLIANCE OF 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER CHANNEL, FOURTH FROM BOTTOM WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-12 - [SDR COMA0010395](https://openairdocs.org/sdr/COMA0010395), Nov 10, 2000: CHANNEL. CRACKED. UPON COMPLIANCE OF 2C INSPECTION TASK 811-02Z THE PAX DOOR INNER CHANNEL, SECOND FROM BOTTOM WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-12 - [SDR COMA0010394](https://openairdocs.org/sdr/COMA0010394), Nov 10, 2000: SHEAR TIE. CRACKED. UPON COMPLIANCE OF 2C INSPECTION 232-01Z THE FUSELAGE SKIN SUPPORT AT FRAME 13A, STRINGER 14R WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-1 - [SDR COMA0010393](https://openairdocs.org/sdr/COMA0010393), Nov 10, 2000: SKIN. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z THE CARGO DOOR CUTOUT INNER SKIN WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL - [SDR COMA0010392](https://openairdocs.org/sdr/COMA0010392), Nov 10, 2000: BUTTSTRAP. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z THE CARGO COMPARTMENT ENTRY THRESHOLD BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB- - [SDR COMA0010391](https://openairdocs.org/sdr/COMA0010391), Nov 10, 2000: FLOORBEAM. CRACKED. UPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I THE RT FLOOR PROP AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL - [SDR COMA0010390](https://openairdocs.org/sdr/COMA0010390), Nov 10, 2000: FLOORBEAM. CRACKED. UPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I THE LT FLOOR PROP AT FRAME 12 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED I/A/W EMB-120 STRUCTURAL - [SDR COMA0010389](https://openairdocs.org/sdr/COMA0010389), Nov 10, 2000: SHEAR TIE. CRACKED. UPON COMPLIANCE OF 2C INSPECTION TASK 221-01Z THE LT FUSELAGE SKIN SUPPORT BRACKET WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTUR - [SDR COMA0010388](https://openairdocs.org/sdr/COMA0010388), Nov 10, 2000: SILL. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 164-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR - [SDR COMA0010387](https://openairdocs.org/sdr/COMA0010387), Nov 10, 2000: SILL. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 162-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR - [SDR COMA0010386](https://openairdocs.org/sdr/COMA0010386), Nov 10, 2000: CROSSBEAM. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z THE RT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL RE - [SDR COMA0010385](https://openairdocs.org/sdr/COMA0010385), Nov 10, 2000: CROSSBEAM. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z THE LT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL RE - [SDR COMA0010384](https://openairdocs.org/sdr/COMA0010384), Nov 10, 2000: CROSSBEAM. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 145-01Z THE LT FLOOR SUPPORT CROSSBEAM WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL RE - [SDR COMA0010383](https://openairdocs.org/sdr/COMA0010383), Nov 10, 2000: SILL. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z THE LT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR - [SDR COMA0010382](https://openairdocs.org/sdr/COMA0010382), Nov 10, 2000: SILL. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR - [SDR COMA0010381](https://openairdocs.org/sdr/COMA0010381), Nov 10, 2000: BUTTSTRAP. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z THE LT FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL RE - [SDR COMA0010380](https://openairdocs.org/sdr/COMA0010380), Nov 10, 2000: BUTTSTRAP. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z THE CENTER FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUC - [SDR COMA0010379](https://openairdocs.org/sdr/COMA0010379), Nov 10, 2000: T-SECTION. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z THE RT FLOOR SUPPORT T-SECTION AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 S - [SDR COMA0010378](https://openairdocs.org/sdr/COMA0010378), Nov 10, 2000: FLOORBEAM. CORRODED. UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z THE LT FLOOR SUPPORT T-SECTION AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 S - [SDR COMA0010372](https://openairdocs.org/sdr/COMA0010372), Oct 9, 2000: BATTERY. DISCHARGED. FWD SECTION OF EMERGENCY FLOOR LIGHTING IS INOP. REPLACED THE NR 1 EMERGENCY BATTERY. - [SDR COMA0010331](https://openairdocs.org/sdr/COMA0010331), Sep 8, 2000: LIGHT. INOPERATIVE. EMERGENCY LIGHT AT ROW 5 IS INOPERABLE. COULD NOT DUPLICATE. EMERGENCY LIGHT OPS NORMAL. - [SDR COMA0010327](https://openairdocs.org/sdr/COMA0010327), Aug 29, 2000: CONNECTOR. DIRTY. AUTOFEATHER WARNING DURING TAKEOFF. CLEANED CONNECTORS CL4 AND CL28, SYSTEM TESTED SATISFACTORY. - [SDR COMA0010066](https://openairdocs.org/sdr/COMA0010066), May 13, 2000: RECEPTACLE. SHORTED. MECHANIC NOTICED SMOKE COMING FROM THE GPU PLUG WHILE AIRCRAFT WAS PARKED AT THE GATE. REPLACED THE EXTERNAL POWER RECEPTACLE AND MULTIPLE AVIONICS COMPONENTS D - [SDR COMA0010067](https://openairdocs.org/sdr/COMA0010067), May 12, 2000: PCU. OUT OF RIG. RIGHT PROPELLER RPM 102.7 PERCENT. CHECKED PROPELLER TO PCU RIGGING, FOUND NO DEFECTS AND FUNCTION CHECK NORMAL. A/C RETURNED TO SERVICE. - [SDR COMA0010052](https://openairdocs.org/sdr/COMA0010052), Apr 18, 2000: SKIN. CORRODED. ON A MAINTENANCE SERVICE CHECK, MECHANIC NOTED POPPED RIVET HEAD ON EXTERNAL SKIN, FRAME 21, LOWER LEFT SIDE, AND SEVERAL BULGES IN SKIN. UPON FURTHER INSPECTIO - [SDR COMA0010053](https://openairdocs.org/sdr/COMA0010053), Apr 17, 2000: POTENTIOMETER. MALFUNCTIONED. LANDING GEAR SELECTOR COULD NOT BE SELECTED UP. REPLACED THE NWS FEEDBACK POT. - [SDR COMA0010047](https://openairdocs.org/sdr/COMA0010047), Mar 26, 2000: BATTERY. DISCHARGED. FORWARD SECTION OF EMERGENCY FLOOR PATH LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY. - [SDR COMA0010037](https://openairdocs.org/sdr/COMA0010037), Mar 14, 2000: SENSOR. MALFUNCTIONED. LANDING GEAR FAILED TO RETRACT, ALL GREEN INDICATORS ON WITH SELECTOR UP. REPLACED RIGHT HAND MLG UPLOCK SENSOR. All 88: https://openairdocs.org/deregistered/N264CA-2006-10-05/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 19930620023459I](https://openairdocs.org/incident/19930620023459I), Jun 20, 1993: Emb EMB120RT (N264CA), Fort Wayne, IN. Loss of power in right engine. Shut engine down. Precautionary landing. Found facture in P3 control line. ## Other aircraft with N264CA - [Registered now](https://openairdocs.org/aircraft/N264CA): Cessna 172M, S/N 17266035, built 1975 - [Cancelled 2008-12-30](https://openairdocs.org/deregistered/N264CA-2008-12-30): British Aerospace BAE JETSTREAM 3201, S/N 907. Exported to Haiti. Owner: [Xxxx, OK](https://openairdocs.org/faa-place/OK/Xxxx) --- 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.