# N267CA: 1992 Embraer EMB-120RT, registration cancelled 2007-11-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 27, 2007 - Exported to: Kenya - Status when cancelled: Sale reported - 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: 120.259 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: March 28, 1992 - Last registry action: April 4, 2007 - Mode S code: A29931 - Location: Johannesburg, South Africa - Owner type: Individual - The mark today: https://openairdocs.org/aircraft/N267CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=267CA - Page: https://openairdocs.org/deregistered/N267CA-2007-11-27 From the FAA registry file of October 31, 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 (99, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COMA0210023](https://openairdocs.org/sdr/COMA0210023), May 31, 2002: LAMP. FLIGHT 5005 ONE EMERGENCY FLOOR LIGHT AT ROW 8 IS INOP.DEFERRED MAINT PER MEL. - [SDR COMA0210018](https://openairdocs.org/sdr/COMA0210018), May 3, 2002: SIGN. BROKEN. FLIGHT 5021 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN.REPLACED EXIT SIGN. - [SDR COMA0210016](https://openairdocs.org/sdr/COMA0210016), Apr 18, 2002: DOOR. FLIGHT 5061 SERVICE DOOR WARNING DURING T/O.CLOSED AND LATCHED SERVICE DOOR. - [SDR COMA0210005](https://openairdocs.org/sdr/COMA0210005), Feb 17, 2002: SERVO. BINDING. FLIGHT 5009 PILOT AND COPILOT RUDDER PEDALS BINDING.REPLACED THE RUDDER SERVO. - [SDR COMA0110152](https://openairdocs.org/sdr/COMA0110152), Oct 23, 2001: PIN. BROKEN. FLIGHT MECHANICS TAXIED A/C TO HANGAR FROM GATE AND FELT A BRAKE DRAGGING. A/C WAS JACKED AND THE LEFT INBD BRAKE WAS FOUND TO BE DRAGGING. AFTER THE BRAKE WAS - [SDR COMA0110153](https://openairdocs.org/sdr/COMA0110153), Oct 22, 2001: CONTROLLER. FAULTY. FLIGHT #5009. DURING CLIMB OUT OF MCO A LOUD AIR NOISE EMANATING FROM THE NOSE AREA, AIRCRAFT RETURNED TO THE FIELD.REPLACED THE LANDING GEAR RELAY BOX. - [SDR COMA0110150](https://openairdocs.org/sdr/COMA0110150), Oct 1, 2001: SENSOR. MALFUNCTIONED. FLIGHT 5038. T/O TRIM AURAL WARNING WHEN POWER LEVERS ADVANCED. COULD NOT DUPLICATE DISCREPANCY AND A/C RETURNED TO SERVICE. DURING CALLBACK MAINTENANCE THE LEF - [SDR COMA0110141](https://openairdocs.org/sdr/COMA0110141), Sep 4, 2001: COMPUTER. FAULTY. FLIGHT #5027. DURING CLIMB-OUT OF MCO RECEIVED HEADING AND PITCH CAPTIONS, RE-SETTING THE HEADING MONITOR CLEARED THE PITCH CAPTION, BUT HEADING CAPTION REMAINE - [SDR COMA0110135](https://openairdocs.org/sdr/COMA0110135), Aug 1, 2001: PROXIMITY SWITCH. MALFUNCTIONED. TAKE OFF TRIM AURAL WARNING.REPLACED DEFECTIVE ELEV. TRIM PROXIMITY SENSOR. - [SDR COMA0110131](https://openairdocs.org/sdr/COMA0110131), Aug 1, 2001: PROXIMITY SWITCH. MALFUNCTIONED. TAKE OFF TRIM AURAL WARNING. REPLACED DEFECTIVE ELEV. TRIM PROXIMITY SENSOR. - [SDR COMA0110022](https://openairdocs.org/sdr/COMA0110022), Jan 12, 2001: SKIN. GOUGED. THE AIRCRAFT SKIN BELOW THE LAVATORY DUMP VALVE DOUBLER IS GOUGED. THE DAMAGE WAS REPAIRED BY INSTALLING AN INTERNAL PATCH (DOUBLER) IN ACCORDANCE WITH EMBRAER - [SDR COMA0110021](https://openairdocs.org/sdr/COMA0110021), Jan 12, 2001: SUPPORT BRACKET. CRACKED. A SKIN SUPPORT FOR FRAME 13A IS CRACKED. THE REPAIR IS TO INSTALL A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT NR 3653-1. - [SDR COMA0110020](https://openairdocs.org/sdr/COMA0110020), Jan 12, 2001: BRACKET. CRACKED. THE AIRCRAFT''S CARGO DOOR TRACK BRACKET IS CRACKED. THE CARGO DOOR AFT TRACK BRACKET WAS REPLACED USING ALTERNATE RIVETS IN ACCORDANCE WITH AERODESING REPORT N - [SDR COMA0110019](https://openairdocs.org/sdr/COMA0110019), Jan 12, 2001: FRAME. NICKED. THE AIRCRAFT''S FRAME 46A HAS A NICK IN THE UPPER FRAME FLANGE AT A PREVIOUSLY INSTALLED ANGLE. THE FRAME WAS REPAIRED BY REMOVING THE OLD ANGLE, DRESSING AND B - [SDR COMA0110018](https://openairdocs.org/sdr/COMA0110018), Jan 12, 2001: STRAP. CORRODED. THE AIRCRAFT HAS CORROSION PAST THE LIMIT ON THE FLOORBEAM BUTT STRAP UNDER THE FLOOR PANEL, LOCATED AT FRAME 13A. THE FLOORBEAM BUTT STRAP WAS REPLACED IN ACCO - [SDR COMA0110017](https://openairdocs.org/sdr/COMA0110017), Jan 12, 2001: STRAP. CORRODED. THE AIRCRAFT HAS CORROSION PAST THE LIMIT ON THE FLOORBEAM BUTT STRAP UNDER THE FLOOR PANEL, LOCATED AT FRAME 13A. THE FLOORBEAM BUTT STRAP WAS REPLACED IN ACCO - [SDR COMA0110015](https://openairdocs.org/sdr/COMA0110015), Jan 12, 2001: SKIN. CRACKED. THE LEFT HAND NACELLE AFT OUTBOARD SKIN IS CRACKED. A DOUBLER WAS INSTALLED IN ACCORDANCE WITH AERODESIGN REPORT NR 3860-1. - [SDR COMA0110014](https://openairdocs.org/sdr/COMA0110014), Jan 12, 2001: SUPPORT BRACKET. CRACKED. THE AIRCRAFT''S SKIN SUPPORT FOR FRAME 40 IS CRACKED. SKIN SUPPORT WAS REPLACED WITH A SERVICEABLE UNIT IN ACCORDANCE WITH AERODESIGN REPORT NR 3859-1. - [SDR COMA0110013](https://openairdocs.org/sdr/COMA0110013), Jan 12, 2001: FLOOR SUPPORT. CORRODED. THE AIRCRAFT''S TWO FLOOR SUPPORT ANGLES UNDER THE PAX DOOR ENTRYWAY THRESHOLD ARE CORRODED. THE PARTS WERE REPLACED IN ACCORDANCE WITH AERODESIGN REPORT NR 371 - [SDR COMA0110012](https://openairdocs.org/sdr/COMA0110012), Jan 12, 2001: FIREWALL. CRACKED. THE AIRCRAFT HAS A CRACK IN THE APU FIREWALL WEB. INSTALLED A DOUBLER IN ACCORDANCE WITH AERODESIGN REPORT NR 2677-3. - [SDR COMA0110011](https://openairdocs.org/sdr/COMA0110011), Jan 12, 2001: FLOORBEAM. CORRODED. THE AIRCRAFT SUSTAINED DAMAGE IN THE FORM OF CORROSION TO THE UPPER SURFACE OF THE CENTER OMEGA FLOORBEAM. THE OMEGA FLOORBEAM WAS REPAIRED IN ACCORDANCE WITH A - [SDR COMA0110010](https://openairdocs.org/sdr/COMA0110010), Jan 12, 2001: FLOORBEAM. CORRODED. THE AIRCRAFT OMEGA BEAMS (P/N 120-46158-001) QTY 2, AND 120-46258-002 QTY 1, HAVE EXCESSIVE CORROSION. THE OMEGA BEAMS WERE REPLACED IN ACCORDANCE WITH AERODESI - [SDR COM0160009](https://openairdocs.org/sdr/COM0160009), Jan 12, 2001: ATTACH ANGLE. CRACKED. THE AIRCRAFT LEFT AND RIGHT WING ATTACH ANGLES ARE CRACKED. THE ANGLES WERE REPAIRED IN ACCORDANCE WITH SRM CHAPTER 53-20-13 PAGES 205 AND 206 AND AERODESIGN RE - [SDR COMA0110016](https://openairdocs.org/sdr/COMA0110016), Jan 12, 2001: FLOOR SUPPORT. CRACKED. THE AIRCRAFT FLOOR PROPS IN THE COCKPIT ARE CRACKED. THE REPAIR CONSISTS OF CUTTING OUT THE DAMAGED AREA AND SPLICING IN A NEW PIECE IN ACCORDANCE WITH AERODESI - [SDR COMA0110009](https://openairdocs.org/sdr/COMA0110009), Jan 12, 2001: FAIRING. CRACKED. THE AIRCRAFT LEFT AND RIGHT WING ATTACH ANGLES ARE CRACKED. THE ANGLES WERE REPAIRED IN ACCORDANCE WITH SRM CHAPTER 53-20-13 PAGES 205 AND 206 AND AERODESIGN RE - [SDR COMA0060795](https://openairdocs.org/sdr/COMA0060795), Oct 4, 2000: SOLENOID. SHORTED. LEFT HAND FLIGHT IDLE STOP CIRCUIT BREAKER IS TRIPPED. REPLACED FIS SOLENOID. - [SDR COMA0010365](https://openairdocs.org/sdr/COMA0010365), Sep 15, 2000: SWITCH. BROKEN. AUTOFEATHER WARNING DURING TAKEOFF ROLL, AIRCRAFT RETURNED TO THE GATE. REPLACED BROKEN MICRO-SWITCH ON THE LEFT POWER LEVER. - [SDR COMA0010319](https://openairdocs.org/sdr/COMA0010319), Aug 24, 2000: SKIN. CRACKED. DURING A 1C INSPECTION FOUND A CRACK APPROXIMATELY .125 INCH LONG EXTENDING FROM A RIVET ON THE RIGHT SIDE POST SKIN BETWEEN THE RIGHT DV WINDOW AND THE RIGHT W - [SDR COMA0010247](https://openairdocs.org/sdr/COMA0010247), Jul 3, 2000: SOLENOID. FAILED. FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER IS TRIPPED.\NREPLACED THE FLIGHT-IDLE STOP SOLENOID. - [SDR COMA0010244](https://openairdocs.org/sdr/COMA0010244), Jul 2, 2000: COMPUTER. MALFUNCTIONED. ATTITUDE DISPLAY WARNING ON MAP. REPLACED THE NR 2 AHRS COMPUTER. - [SDR COMA0010243](https://openairdocs.org/sdr/COMA0010243), Jun 30, 2000: WARNING SYSTEM. FALSE ACTIVATION. TAKE OFF TRIM CONFIG WARNING. COULD NOT DUPLICATE. TRIM AURAL WARNING SYSTEM CHECKS SATISFACTORY. - [SDR COMA0010162](https://openairdocs.org/sdr/COMA0010162), Jun 9, 2000: SENSOR. MALFUNCTIONED. TAKEOFF TRIM WARNING. REPLACED THE LEFT HAND ELEVATOR TRIM PROXIMITY SENSOR. - [SDR COMA0010054](https://openairdocs.org/sdr/COMA0010054), Apr 16, 2000: SOLENOID. MALFUNCTIONED. FLIGHT IDLE SOLENOID CIRCUIT BREAKER TRIPPED. REPLACED THE LEFT HAND SOLENOID. - [SDR COMA0010044](https://openairdocs.org/sdr/COMA0010044), Mar 24, 2000: WARNING SYSTEM. ACTIVATED. TRIM FAIL T/O CONFIG WARNING. COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL. - [SDR COMA0010006](https://openairdocs.org/sdr/COMA0010006), Jan 9, 2000: WIRE. DISCONNECTED. TAKEOFF CONFIG WARNING. REPAIRED ELEVATOR TRIM PROXIMITY SENSOR WIRING CONNECTIONS. - [SDR COMA9910187](https://openairdocs.org/sdr/COMA9910187), Dec 16, 1999: BLADE. DAMAGED. FOUND NR 4 BLADE RIGHT PROP HAD TIP DAMAGE. REMOVED AND REPLACED NR 4 BLADE RIGHT PROP. - [SDR COMA9910153](https://openairdocs.org/sdr/COMA9910153), Sep 21, 1999: BULB. FAILED. FLOOR TRACK LIGHT AT SEAT 9A IS INOPERABLE. REMOVED AND REPLACED BULB. - [SDR COMA9910130](https://openairdocs.org/sdr/COMA9910130), Aug 9, 1999: LIGHT. MISSING. EMERGENCY EXIT LIGHT CONVER MISSING ROW 5. REPLACED LIGHT ASSY. - [SDR COMA9910119](https://openairdocs.org/sdr/COMA9910119), Jul 23, 1999: HYD PUMP. LEAKING. BLUE HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED ENGINE HYDRAULIC PUMP. - [SDR COMA9910087](https://openairdocs.org/sdr/COMA9910087), May 28, 1999: LIGHT. INOPERATIVE. GRR - FLT 5024 - EMERGENCY LIGHTS ARE INOPERABLE. COULD NOT DUPLICATE. EMERGENCY LIGHTS OPERATE NORMAL. (M) - [SDR COMA9910044](https://openairdocs.org/sdr/COMA9910044), Mar 21, 1999: PCU. MALFUNCTIONED. RIGHT HAND PROPELLER OVER SPEED TO 103 DEGREES. REPLACED THE PROPELLER CONTROL UNIT. - [SDR COMA9910037](https://openairdocs.org/sdr/COMA9910037), Feb 20, 1999: FUEL DOOR. MISSING. SINGLE POINT FUEL SERVICE DOOR MISSING. REPAIRED DAMAGE CAUSED BY SEPARATION OF FUEL SERVICE DOOR AND REPLACED DOOR. - [SDR COMA9810245](https://openairdocs.org/sdr/COMA9810245), Oct 29, 1998: SENSOR. BURNT. LAVATORY SMOKE ALARM ACTIVATED SMOKE IN COCKPIT. REPLACED BURNT AOA VANE CURRENT SENSOR. - [SDR COMA9810136](https://openairdocs.org/sdr/COMA9810136), Jun 5, 1998: CONTROL UNIT. FAILED. AIRCRAFT HAS NO BRAKES DURING LANDING ROLL. REPLACED THE BRAKE CONTROL UNIT. - [SDR COMA9810080](https://openairdocs.org/sdr/COMA9810080), Apr 1, 1998: SENSOR. MALFUNCTION. RT MLG, GREEN DOWN INDICATION, CAME ON WITH GEAR RETRACTED. REPLACED THE RT MLG DOWNLOCK SENSOR. - [SDR COMA9810047](https://openairdocs.org/sdr/COMA9810047), Feb 23, 1998: CONTROL BOX. MALFUNCTION. LANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR CONTROL BOX. - [SDR COMA9810039](https://openairdocs.org/sdr/COMA9810039), Feb 5, 1998: SENSOR. MALFUNCTION. TAKEOFF TRIM WARNING SOUNDED. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSORS. - [SDR COMA9810032](https://openairdocs.org/sdr/COMA9810032), Jan 24, 1998: BULB. FAILED. FLOOR EMERGENCY LIGHT AT GALLEY AREA IS INOP. REPLACED BULB. - [SDR COMA9710471](https://openairdocs.org/sdr/COMA9710471), Nov 9, 1997: BATTERY. DISCHARGED. EMERGENCY LIGHTS ARE INOP. REPLACED THE EMERGENCY LIGHTS BATTERIES. - [SDR COMA9710387](https://openairdocs.org/sdr/COMA9710387), Aug 20, 1997: FLOORBEAM. CORRODED. DURING 4C INSEPCTION TASK 5320-151/152-01I, FOUND RIGHT HAND FLOORBEAM AT FRAME 33 TO BE CORRODED. REMOVED CORRODED FLOORBEAM AND INSTALLED SERV PART IAW EMB 12 All 99: https://openairdocs.org/deregistered/N267CA-2007-11-27/reports.md ## Other aircraft with N267CA - [Registered now](https://openairdocs.org/aircraft/N267CA): Cessna 402C, S/N 402C0030, 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.