# N152CA: Embraer EMB-120RT, registration cancelled 2001-01-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 11, 2001 - Exported to: Australia - Status when cancelled: Valid registration - Airframe: [Embraer EMB-120RT](https://openairdocs.org/model/embraer-emb-120rt) (registry code 3260202) - Data sheets: [TCDS A31SO](https://openairdocs.org/tcds/A31SO) (OpenAirDocs) - Serial number: 120.152 - Type of aircraft: Fixed wing multi engine - Certificate issued: June 19, 2000 - Last registry action: June 19, 2000 - Mode S code: A0D1D0 - Owner when cancelled: [Bombardier Capital Inc](https://openairdocs.org/faa-owner/BOMBARDIER%20CAPITAL%20INC) - Location: [Colchester, VT](https://openairdocs.org/faa-place/VT/Colchester) - Owner type: Non-citizen corporation - Owner's area on the map: 44.5541° N, 73.2255° W: Placed by OpenAirDocs at the center of ZIP code 05446, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N152CA - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=152CA - Page: https://openairdocs.org/deregistered/N152CA-2001-01-11 From the FAA registry file of October 29, 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 (59, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR COMA0010014](https://openairdocs.org/sdr/COMA0010014), Jan 25, 2000: BATTERY. DISCHARGED. AFT SECTION OF CABIN EMERGENCY LIGHTS WERE INOPERABLE. REPLACED THE NR 3 EMERGENCY BATTERY. - [SDR COMA0010013](https://openairdocs.org/sdr/COMA0010013), Jan 24, 2000: WARNING SYSTEM. ACTIVATED. FLAP DISAGREE WHEN FLAPS SELECTED UP. COULD NOT DUPLICATE. OPERATON OF FLAPS NORMAL. - [SDR COMA0010010](https://openairdocs.org/sdr/COMA0010010), Jan 16, 2000: BATTERY. DISCHARGED. EMERGENCY FLOOR PATH LIGHTS ARE INOPERABLE ROWS 1-5. REPLACED EMERGENCY BATTERY. - [SDR COMA0010001](https://openairdocs.org/sdr/COMA0010001), Dec 30, 1999: WARNING SYSTEM. ACTIVATED. SERVICE DOOR WARNING DURING TAKEOFF. CLOSED AND SECURED SIGNLE POINT FUEL SERVICE DOOR. - [SDR COMA9910162](https://openairdocs.org/sdr/COMA9910162), Oct 9, 1999: NP INDICATOR. FAILED. DURING TAKEOFF ROLL, THE RIGHT PROPELLER INDICATED 97.6 PERCENT NP. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. REPLACED THE RIGHT NP INDICATOR. - [SDR COMA9910107](https://openairdocs.org/sdr/COMA9910107), Jul 8, 1999: SIGN. BROKEN. EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPAIRED EXIT SIGN. - [SDR COMA9910088](https://openairdocs.org/sdr/COMA9910088), May 28, 1999: BATTERIES. DISCHARGED. HTS - FLT 5730 - EMERGENCY LIGHTS ARE INOPERABLE. REPLACED THE EMERGENCY BATTERIES. (M) - [SDR COMA9910085](https://openairdocs.org/sdr/COMA9910085), May 25, 1999: BATTERY. DISCHARGED. LAN - FLT 5076 - EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERIES. (M) - [SDR COMA9910078](https://openairdocs.org/sdr/COMA9910078), May 10, 1999: ACTUATOR. FAILED. FLAP CONTROL FAULT AT 80 KTS ON TAKEOFF. REPLACED RIGHT INBOARD FLAP ACTUATOR. - [SDR COMA9910068](https://openairdocs.org/sdr/COMA9910068), Apr 30, 1999: WARNING. ACTIVATED. FLAP CONTROL FAULT WARNING. COULD NOT DUPLICATE, NO DEFECTS FOUND. - [SDR COMA9810292](https://openairdocs.org/sdr/COMA9810292), Dec 29, 1998: BULB. FAILED. EMERGENCY LIGHT AT SEAT 2A IS INOPERABLE. REPLACED LIGHT BULB. - [SDR COMA9810272](https://openairdocs.org/sdr/COMA9810272), Nov 30, 1998: ACTUATOR. MALFUNCTION. FLAP CONTROL FAULT DURING APPROACH. REPLACED THE LEFT HAND NACELLE FLAP ACTUATOR. - [SDR COMA9810258](https://openairdocs.org/sdr/COMA9810258), Nov 6, 1998: CONNECTOR. DEFECTIVE. FLAP CONTROL FAULT. REPLACED ACTUATOR WIRNG CONNECTOR JO 365. - [SDR COMA9810254](https://openairdocs.org/sdr/COMA9810254), Nov 4, 1998: BATTERY. DISCHARGED. ROW 1 AND ROW 4 EXIT LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY. - [SDR COMA9810194](https://openairdocs.org/sdr/COMA9810194), Sep 14, 1998: SIGN. BROKEN. EMERGENCY LIGHT COVER AT 5C IS BROKEN. REPLACED EXIT SIGN. - [SDR COMA9810167](https://openairdocs.org/sdr/COMA9810167), Jul 31, 1998: WARNING. ACTIVATED. FLAP SYSTEM WARNING DURING TAKEOFF. COULD NOT DUPLICATE, SYSTEM TEST NORMAL. - [SDR COMA9810126](https://openairdocs.org/sdr/COMA9810126), May 21, 1998: BATTERY. DISCHARGED. FORWARD CABIN EMERGENCY LIGHTING IS INOP. REPLACED EMERGENCY BATTERY. - [SDR COMA9810115](https://openairdocs.org/sdr/COMA9810115), May 10, 1998: SIGN. BROKEN. EXIT SIGN AT ROW 5A IS BROKEN. REPLACED EXIT SIGN. - [SDR COMA9810111](https://openairdocs.org/sdr/COMA9810111), Apr 29, 1998: DE-ICE BOOT. WORN. RIGHT ENGINE INLET DE-ICE SYSTEM FAILURE DURING CRUISE FLIGHT. REPLACED LEFT AND RIGHT ENGINE INLET DE-ICE BOOTS. - [SDR COMA9810073](https://openairdocs.org/sdr/COMA9810073), Mar 23, 1998: ROLLERS. WORN. FLAP CONTROL FAULT WHEN FLAPS SELECTED FOR LANDING APPROACH. REPLACED THE RIGHT HAND INBOARD FLAP ROLLERS. - [SDR COMA9810041](https://openairdocs.org/sdr/COMA9810041), Feb 6, 1998: ACTUATOR. MALFUNCTION. FLAP CONTROL FAULT WARNING. REPLACED THE RIGHT HAND NACELLE FLAP ACTUATOR. - [SDR COMA9710489](https://openairdocs.org/sdr/COMA9710489), Dec 5, 1997: PRESS REGULATOR. MALFUNCTION. LEFT AIR FOIL DE-ICE SYSTEM INOP. REPLACED THE DE-ICE PRESSURE REGULATOR. - [SDR COMA9710327](https://openairdocs.org/sdr/COMA9710327), Jul 6, 1997: BATTERY. DISCHARGED. FORWARD CABIN EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LIGHT BATTERY. - [SDR COMA9710323](https://openairdocs.org/sdr/COMA9710323), Jul 2, 1997: CHANNEL. WORN. LEFT WING FAIRING COMPOSITE HAS SLIGHT DELAMINATION AT EDGE. REPAIRED WING FAIRING IAW SRM. - [SDR COMA9710297](https://openairdocs.org/sdr/COMA9710297), May 20, 1997: BATTERY. DISCHARGED. EMERGENCY LIGHTS FAIL AFTER 5 SECONDS OF USE. REPLACED THE EMERGENCY LIGHT BATTERIES (S/N 1236, 810, AND 956). - [SDR COMA9710222](https://openairdocs.org/sdr/COMA9710222), Apr 19, 1997: ROLLERS. WORN. FLAP DISAGREEMENT AFTER TAKEOFF. REPLACED RT OUTBOARD FLAP ROLLERS. - [SDR COMA9710128](https://openairdocs.org/sdr/COMA9710128), Feb 11, 1997: PITCHLOCK SCREW. MALFUNCTIONED. PROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR ACTUATOR AND HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB WAS FOUND DISPLACED .025 - [SDR COMA9710126](https://openairdocs.org/sdr/COMA9710126), Feb 1, 1997: CONNECTOR. LOOSE. WHEN FLAPS EXTENDED, INBOARD FLAPS REMAINED UP AND OUTBOARD FLAPS WENT FULL DOWN. REPAIRED LOOSE WIRE CONNECTOR AT THE FLAP CONTROL UNIT. - [SDR COMA9710098](https://openairdocs.org/sdr/COMA9710098), Jan 31, 1997: FLAP CONTL UNIT. MALFUNCTION. FLAP CONTROL FAULT WARNING DURING TAXI. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 2,093. - [SDR COMA9710091](https://openairdocs.org/sdr/COMA9710091), Jan 28, 1997: HINGE. BROKEN. LT M.L.G. DOORS DO NOT CLOSE PROPERLY. REPLACED BROKEN DOOR HINGE ON LT M.L.G. AFT DOOR. - [SDR COMA9610422](https://openairdocs.org/sdr/COMA9610422), Dec 23, 1996: BUTT STRAP. MISDRILLED. DURING 2C CHECK THE FUSELAGE AFT FLOOR SUPPORT STRUCTURE BUTT STRAP AT CARGO DOOR OPENING WAS FOUND TO HAVE MISDRILLED HOLES. THE BUTT STRAP WAS REPAIRED PER AE - [SDR COMA9610421](https://openairdocs.org/sdr/COMA9610421), Dec 23, 1996: JOINT SHEET. GOUGED. DURING 2C CHECK, INSPECTION REVEALED THE WING AUX SPAR CENTER SECTION JOINT SHEET DAMAGED BY SCREWS THAT ATTACH THE LOWER FAIRING. THE DAMAGE CONSISTS OF A SMAL - [SDR COMA9610420](https://openairdocs.org/sdr/COMA9610420), Dec 23, 1996: BUTT STRAP. CORRODED. DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT RT BUTT STRAP FOUND CORRODED. BUTT STRAP REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIR - [SDR COMA9610419](https://openairdocs.org/sdr/COMA9610419), Dec 23, 1996: SILL. CORRODED. DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE LT SILL FOUND CORRODED. SILL REPLACED WITH NEW PART PER SRM CHAPT. 51 STANDARD PRACTICES. AIRCRA - [SDR COMA9610418](https://openairdocs.org/sdr/COMA9610418), Dec 23, 1996: SILL. CORRODED. DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE LT SILL CORRODED. SILL WAS REPAIRED PER AERODESIGN REPORT NR 2140-1, REV IR, DATED 12-22-96. AIR - [SDR COMA9610417](https://openairdocs.org/sdr/COMA9610417), Dec 23, 1996: SILL. CORRODED. DURING 2C CHECK FUSELAGE CENTER SECTION FLOOR SUPPORT STRUCTURE RT SILL FOUND CORRODED. SILL WAS REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. - [SDR COMA9610416](https://openairdocs.org/sdr/COMA9610416), Dec 23, 1996: SILL. CORRODED. DURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE RT SILL FOUND CORRODED. REPLACED SILL WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. AIRCRAFT TOTAL C - [SDR COMA9610415](https://openairdocs.org/sdr/COMA9610415), Dec 23, 1996: BUTT STRAP. CORRODED. DURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP FOUND CORRODED. REPLACED BUTT STRAP WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. - [SDR COMA9610414](https://openairdocs.org/sdr/COMA9610414), Dec 23, 1996: BUTT STRAP. CORRODED. DURING 2C CHECK FWD FUSELAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP FOUND CORRODED. BUTT STRAP REPLACED WITH NEW PART PER SRM CHAPT. 51, STANDARD PRACTICES. - [SDR COMA9610413](https://openairdocs.org/sdr/COMA9610413), Dec 23, 1996: BUTT STRAP. CORRODED. DURING 2C CHECK FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT BUTT STRAP FOUND CORRODED. BUTT STRAP WAS REPLACED WITH NEW PART PER SRM CHAPT 51, STANDARD PRACTICES. A - [SDR COMA9610412](https://openairdocs.org/sdr/COMA9610412), Dec 23, 1996: SILL. CORRODED. DURING 2C CHECK FUSELAGE FWD CABIN FLOOR SUPPORT STRUCTURE LT SILL FOUND CORRODED. SILL WAS REPLACED WITH NEW PART PER SRM 51-40, STANDARD PRACTICES. AIRCRAFT T - [SDR COMA9610411](https://openairdocs.org/sdr/COMA9610411), Dec 23, 1996: STRINGER. CORRODED. DURING 2C CHECK INSPECTION FOUND CORROSION ON FUSELAGE STRINGER 19L BETWEEN FRAMES 19 AND 20. STRINGER 19L WAS REPAIRED PER AERODESIGN REPORT NR 1990-2, REV.IR - [SDR COMA9610405](https://openairdocs.org/sdr/COMA9610405), Dec 17, 1996: HYDRAULIC HOSE. FAILED. HYDRAULIC FLUID LEAKING FROM LT LANDING GEAR AREA. REPLACED LEAKING LANDING GEAR ACTUATOR HYDRAULIC HOSE. - [SDR COMA9610309](https://openairdocs.org/sdr/COMA9610309), Oct 17, 1996: FLAP CONTL UNIT. MALFUNCTION. FLAP CONTROL FAULT WARNING, INBD FLAPS ARE FAILED. REPLACED THE FLAP CONTROL UNIT. - [SDR COMA9610306](https://openairdocs.org/sdr/COMA9610306), Oct 15, 1996: FLAP SELECTOR. MALFUNCTION. FLAP CONTROL FAULT WARNING. REPLACED THE FLAP SELECTOR UNIT. - [SDR COMA9610301](https://openairdocs.org/sdr/COMA9610301), Oct 9, 1996: T SECTION. CORRODED. FOUND FUSELAGE FLOOR SUPPORT STRUCTURE T-SECTION CORRODED IN FWD CABIN AREA. REMOVED CORRODED T-SECTION AND INSTALLED NEW PART PER REPORT NR 2057-1, REV. IR, DA - [SDR COMA9610300](https://openairdocs.org/sdr/COMA9610300), Oct 9, 1996: BUTT STRAP. CORRODED. FOUND FUSELAGE FLOOR SUPPORT STRUCTURE FORWARD LT BUTT STRAP CORRODED. REMOVED CORRODED BUTT STRAP AND INSTALLED NEW PART PER EMB120 SRM STANDARD PRACTICES, CH - [SDR COMA9610272](https://openairdocs.org/sdr/COMA9610272), Sep 3, 1996: BATTERY. DISCHARGED. AFT SECTION OF CABIN EMERGENCY LIGHTING IS INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY. PART TOTAL CYCLES, 13,088. - [SDR COMA9610260](https://openairdocs.org/sdr/COMA9610260), Aug 25, 1996: CIRCUIT BREAKER. DAMAGED. EMERGENCY BUS LOST POWER, CONTROL BUS INOP, RT ENGINE INSTRUMENTS INOP, COPILOTS EFIS AND COMM RADIO INOP, A LANDING GEAR INDICATION INOP. FOUND BUS BAR CONNECT - [SDR COMA9610224](https://openairdocs.org/sdr/COMA9610224), Jul 11, 1996: FLAP WARNING. ACTIVATED. FLAP CONTROL FAULT WARNING AFTER LANDING. INSPECTED FLAP SYSTEM AND FOUND TO OPERATE NORMALLY. COULD NOT DUPLICATE DISCREPANCY. All 59: https://openairdocs.org/deregistered/N152CA-2001-01-11/reports.md ## Other aircraft with N152CA - [Registered now](https://openairdocs.org/aircraft/N152CA): Bell 206B, S/N 2342, built 1978 --- 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.