# N247CA: 1991 Embraer EMB-120ER, registration cancelled 2025-08-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 13, 2025
- Status when cancelled: Valid registration
- Airframe: [Embraer EMB-120ER](https://openairdocs.org/model/embraer-emb-120er) (registry code 3260203)
- Engine: [Pratt & Whitney Canada PW118B](https://openairdocs.org/engine/pratt-whitney-canada-pw118b) (registry code 52131)
- Data sheets: [TCDS A31SO](https://openairdocs.org/tcds/A31SO), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 120.225
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: April 13, 2001
- Certificate issued: January 10, 2014
- Last registry action: September 30, 2023
- Mode S code: A24A33
- Owner when cancelled: [Uas Transervices Inc](https://openairdocs.org/faa-owner/UAS%20TRANSERVICES%20INC)
- Location: [Boca Raton, FL](https://openairdocs.org/faa-place/FL/Boca%20Raton)
- Owner type: Corporation
- Owner's area on the map: 26.3746° N, 80.1066° W: Placed by OpenAirDocs at the center of ZIP code 33431, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N247CA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=247CA
- Page: https://openairdocs.org/deregistered/N247CA-2025-08-13

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 (60, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR COMA0010314](https://openairdocs.org/sdr/COMA0010314), Aug 3, 2000: CHANNEL. CRACKED. UPON COMPLIANCE OF 1C-CHECK TASK 52-14, THE PASSENGER DOOR INNER CHANNEL WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORDANCE WITH EMB-120 STUCT
- [SDR COMA0010313](https://openairdocs.org/sdr/COMA0010313), Aug 3, 2000: BULKHEAD. CRACKED. UPON COMPLIANCE OF 1C-CHECK TASK 433-01Z, THE LEFT NACELLE FRAME 14 EXHAUST PAN SUPPORT BULKHEAD WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCOR
- [SDR COMA0010312](https://openairdocs.org/sdr/COMA0010312), Aug 3, 2000: SKIN. GOUGED. UPON COMPLIANCE OF 1C-CHECK TASK 100-01Z, THE FUSELGE FWD LOWER RT SKIN JUST BELOW LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED 
- [SDR COMA0010311](https://openairdocs.org/sdr/COMA0010311), Aug 3, 2000: SKIN. DENTED. UPON COMPLIANCE OF 1C-CHECK TASK 5310-122-01E, THE FUSELAGE RT FWD LOWER SKIN WAS FOUND TO BE DENTED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 S
- [SDR COMA0010310](https://openairdocs.org/sdr/COMA0010310), Aug 3, 2000: SHEAR TIE. CRACKED. WHILE PERFORMING OTHER MAINTENANCE, THE FUSELAGE LEFT HAND SKIN SUPPORT AT FRAME 9, WAS FOUND TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED IN ACCORDANCE WITH EM
- [SDR COMA0010309](https://openairdocs.org/sdr/COMA0010309), Aug 3, 2000: SKIN. GOUGED. UPON COMPLIANCE OF 1C-CHECK TASK 813-01Z THE CARGO DOOR SKIN WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR 
- [SDR COMA0010308](https://openairdocs.org/sdr/COMA0010308), Aug 3, 2000: ANGLE. CRACKED. UPON COMPLIANCE OF 1C-CHECK TASK 194-01Z THE RIGHT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACCORD
- [SDR COMA0010307](https://openairdocs.org/sdr/COMA0010307), Aug 3, 2000: ANGLE. CRACKED. UPON COMPLIANCE OF 1C-CHECK TASK 193-01Z, THE LEFT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IN ACORDA
- [SDR COMA0010306](https://openairdocs.org/sdr/COMA0010306), Aug 3, 2000: SKIN. DAMAGED. UPON COMPLIANCE OF 1C-CHECK TASK 5720-622-02E, THE RIGHT WING LOWER SKIN RIVET HOLE AT RIB 6, STRINGER 10 WAS FOUND TO BE IMPROPERLY COUNTERSUNK. THE DAMAGED SK
- [SDR COMA0010305](https://openairdocs.org/sdr/COMA0010305), Aug 3, 2000: STRAP. CORRODED. WHILE PERFORMING OTHER MAINTENANCE, THE FUSELAGE FORWARD CENTER CABIN FLOOR BEAM BUTT-STRAP WAS FOUND TO BE CORRODED. THE BUTT-STRAP WAS REPLACED IN ACCORDANCE 
- [SDR COMA0010202](https://openairdocs.org/sdr/COMA0010202), Jun 17, 2000: BATTERY. DISCHARGED. EMERGENCY FLOOR PATH LIGHTING IS INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY.
- [SDR COMA0060258](https://openairdocs.org/sdr/COMA0060258), Mar 11, 2000: BOOT. LEAKING. WING DE-ICE FAIL WARNING. REPLACED THE RIGHT WING INBOARD DE-ICE BOOT.
- [SDR COMA0010028](https://openairdocs.org/sdr/COMA0010028), Feb 20, 2000: BATTERY. DISCHARGED. CABIN EMERGENCY LIGHT SYSTEM WAS PARTIALLY INOP. REPLACED EMERGENCY BATTERY.
- [SDR COMA0010026](https://openairdocs.org/sdr/COMA0010026), Feb 16, 2000: BATTERY. DISCHARGED. 5 EXIT LIGHTS ON FLOOR AND 1 ON OVERHEAD ARE INOPERABLE. REPLACED THE NR 1 AND NR 2 EMERGENCY BATTERIES.
- [SDR COMA9910198](https://openairdocs.org/sdr/COMA9910198), Dec 25, 1999: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN AT ROW 8 IS INOPERABLE. REPAIRED DAMAGED WIRES AT EXIT SIGN.
- [SDR COMA9910190](https://openairdocs.org/sdr/COMA9910190), Dec 15, 1999: CONTROLLER. MALFUNCTIONED. RT PROPELLER RPM WAS 99.2 TO 99.6 AFTER TAKEOFF. GROUND RUNS SHOWED PROPELLER RPM TO BE IN LIMITATIONS.
- [SDR COMA9910184](https://openairdocs.org/sdr/COMA9910184), Dec 14, 1999: RCCB. FAILED. RIGHT HAND PROPELLER DEICE FAIL WARNING. REPLACED RCCB (CB0226).
- [SDR COMA9910169](https://openairdocs.org/sdr/COMA9910169), Oct 29, 1999: LIGHT. INOP. FWD EMERGENCY FLOOR LIGHT WAS INOP. REPLACED LIGHT ASSY.
- [SDR COMA9910149](https://openairdocs.org/sdr/COMA9910149), Sep 19, 1999: WARNING. ACTIVATED. SERVICE DOOR WARNING DURING TAKEOFF. DOOR WARNING SYSTEM PREVIOUSLY DEFERRED PER MEL.
- [SDR COMA9910150](https://openairdocs.org/sdr/COMA9910150), Sep 18, 1999: WARNING. ACTIVATED. SERVICE DOOR WARNING DURING TAKEOFF. DEFERRED DOOR WARNING SYSTEM PER MEL.
- [SDR COMA9910084](https://openairdocs.org/sdr/COMA9910084), May 25, 1999: SENSOR. FAILED. LEFT MLG DOWN INDICATOR ON WITH GEAR RETRACTED. LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. FREE FALL SYSTEM USED TO EXTEND GEAR. REPLACED DOWN LOCK PROXIMITY 
- [SDR COMA9910034](https://openairdocs.org/sdr/COMA9910034), Feb 16, 1999: DEICE. INOP. RIGHT HAND PROPELLER DEICE IS INOPERABLE. REPLACED THE NR 3 BLADE ON RIGHT HAND PROPELLER.
- [SDR COMA9910026](https://openairdocs.org/sdr/COMA9910026), Feb 2, 1999: FRAME. CRACKED. LEFT NACELLE, FRAME WEB NR 10 CRACKED AT INBOARD RADIUS OF THE FLANGE. REPAIRED BY SPLICING IN A NEW FLANGE PER AERODESIGN REPORT NR 1076-2 AND EMB120 SRM 51-40
- [SDR COMA9910025](https://openairdocs.org/sdr/COMA9910025), Jan 27, 1999: BATTERY PACK. DISCHARGED. FORWARD SECTION OF CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK FOR THE FORWARD EMERGENCY LIGHTING.
- [SDR COMA9910005](https://openairdocs.org/sdr/COMA9910005), Jan 3, 1999: CONTACTOR. FAILED. EXTERNAL POWER CONTACTOR BURNT/OVERHEATED AT TERMINAL ENDS. REPLACED CONTACTOR AND POSITIVE CABLE.
- [SDR COMA9810277](https://openairdocs.org/sdr/COMA9810277), Dec 2, 1998: FASTENER. BROKEN. SERVICE DOOR WARNING DURING TAKEOFF. REPLACED BROKEN CAM LOCK FASTENER ON SINGLE POINT FUEL SERVICE DOOR.
- [SDR COMA9810274](https://openairdocs.org/sdr/COMA9810274), Dec 1, 1998: SENSOR. MALFUNCTIONED. AFTER LANDING GEAR RETRACTED, RIGHT HAND MLG DOWN INDICATOR REMAINED ON. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR.
- [SDR COMA9810270](https://openairdocs.org/sdr/COMA9810270), Nov 18, 1998: LATCH. NOT SECURED. SERVICE DOOR WARNING DURING CLIMBOUT. AIRCRAFT RETURNED TO THE FIELD. CLOSED DOOR AND SECURED LATCH.
- [SDR COMA9810238](https://openairdocs.org/sdr/COMA9810238), Oct 19, 1998: PIN. NOT REMOVED. NOSE LANDING GEAR WOULD NOT RETRACT. REMOVED NLG PIN. GEAR SWINGS GOOD.
- [SDR COMA9810235](https://openairdocs.org/sdr/COMA9810235), Oct 8, 1998: CROSSBEAM. CORRODED. DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT CENTER CROSSBEAM TO BE CORRODED AT FRAME 16. REMOVED AND REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRA
- [SDR COMA9810233](https://openairdocs.org/sdr/COMA9810233), Oct 8, 1998: SILL. CORRODED. DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT NR 1 STILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICE
- [SDR COMA9810232](https://openairdocs.org/sdr/COMA9810232), Oct 8, 1998: SILL. CORRODED. DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT NR 1 SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES
- [SDR COMA9810231](https://openairdocs.org/sdr/COMA9810231), Oct 8, 1998: BUTTSTRAP. CORRODED. DURING 2C INSPECTION TASK 151-01Z REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 STANDARD PRAC
- [SDR COMA9810230](https://openairdocs.org/sdr/COMA9810230), Oct 8, 1998: BUTTSTRAP. CORRODED. DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT FORWARD BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 SRM 
- [SDR COMA9810229](https://openairdocs.org/sdr/COMA9810229), Oct 7, 1998: WIRE HARNESS. OUT OF POSITION. DURING 2C INSPECTION, TASK 5720-622-01I, REVEALED THE WIRE HARNESS FOR THE RIGHT WING FORWARD FUEL BOOST PUMP TO BE CHAFFING ON THE METAL BRAIDED FUEL LINE. PUM
- [SDR COMA9810236](https://openairdocs.org/sdr/COMA9810236), Oct 6, 1998: BUTTPLATE. CORRODED. DURING 2C INSPECTION TASK 5310-131-O1I REVEALED CENTER BUTTPLATE TO HAVE SPOTS OF CORROSION THAT WERE BEYOND LIMITS. REMOVED CENTER BUTTPLATE AND INSTALLED SERV
- [SDR COMA9810172](https://openairdocs.org/sdr/COMA9810172), Aug 10, 1998: WHEEL. CRACKED. DURING TEARDOWN VISUAL INSPECTION FOR TIRE CHANGE, THE INNER HALF OF THE MAIN WHEEL ASSY WAS FOUND TO HAVE A CRACK APPROXIMATELY 2 INCHES IN LENGTH RUNNING INWA
- [SDR COMA9810123](https://openairdocs.org/sdr/COMA9810123), May 17, 1998: BATTERY. DISCHARGED. SOME OF THE CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.
- [SDR COMA9710506](https://openairdocs.org/sdr/COMA9710506), Dec 23, 1997: WIRE. BROKEN. SOME OF THE CABIN FLOOR PATH EMERGENCY LIGHTS ARE INOP. REPAIRED BROKEN WIRE.
- [SDR COMA9710316](https://openairdocs.org/sdr/COMA9710316), Jun 17, 1997: FUEL DOOR. NOT LATCHED. SERVICE DOOR WARNING CAME ON AFTER TAKEOFF. SINGLE POINT FUEL SERVICE DOOR NOT LATCHED. SECURED DOOR AND AIRCRAFT RETURNED TO SERVICE.
- [SDR COMA9710089](https://openairdocs.org/sdr/COMA9710089), Jan 26, 1997: ROLLER. DIRTY. FLAP DISAGREEMENT AFTER FLAPS SELECTED TO 0 DEGREES. REPLACED FLAP ROLLERS ON LEFT AND RIGHT OUTBOARD FLAPS.
- [SDR COMA9710013](https://openairdocs.org/sdr/COMA9710013), Dec 30, 1996: RELAY. FAILED. EMERGENCY LIGHTING NOT ARMED WARNING ON MAP, CIRCUIT BREAKER TRIPPED. COULD NOT DUPLCIATE DISCREPANCY. REPLACED RELAY K201 FOR TROUBLESHOOTING.
- [SDR COMA9610401](https://openairdocs.org/sdr/COMA9610401), Dec 15, 1996: TUBING. CHAFED. HYDRAULIC FLUID LEAKING FROM LT ENGINE NACELLE. REPLACED DAMAGED SECTION OF GREEN SYSTEM HYDRAULIC PRESSURE TUBING BETWEEN NACELLE 13 AND 14.
- [SDR COMA9610334](https://openairdocs.org/sdr/COMA9610334), Nov 20, 1996: POTENTIOMETER. MALFUNCTION. CLUNKING SOUND AND UNCOMMANDED MOVEMENT FROM NOSE WHEEL STEERING SYSTEM. REPLACED THE NWS FEEDBACK POTENTIOMETER.
- [SDR COMA9610288](https://openairdocs.org/sdr/COMA9610288), Sep 26, 1996: SWITCH. OUT OF ADJUST. CARGO DOOR WARNING SOUNDED DURING TAKEOFF. ADJUSTED CARGO DOOR MICROSWITCH. AIRCRAFT CONTINUED SERVICE.
- [SDR COMA9610223](https://openairdocs.org/sdr/COMA9610223), Jul 12, 1996: CONTROLLER. FAILED. TRANSPONDER NR 1 AND NR 2 REPORTED INOPERATIVE BY AIR TRAFFIC CONTROL. REPLACED CTL-92.
- [SDR COMA9610225](https://openairdocs.org/sdr/COMA9610225), Jul 11, 1996: FUEL NOZZLE. LEAKING. FUEL LEAKING FROM RT ENGINE NACELLE. REPLACED THE RT ENGINE FUEL NOZZLES.
- [SDR COMA9610166](https://openairdocs.org/sdr/COMA9610166), Jun 4, 1996: SENSOR. DEFECTIVE. WHEN LANDING GEAR SELECTED DOWN, GEAR DID NOT EXTEND. INDICATION WAS 5 RED INTRANSIT AND ONE GREEN DOWNLOCK. EMERGENCY SYSTEM USED TO EXTEND GEAR. REPLACED DEFE
- [SDR COMA9610154](https://openairdocs.org/sdr/COMA9610154), May 27, 1996: LATCH. BROKEN. RIGHT MLG OUTBOARD GEAR DOOR WILL NOT CLOSE. REPLACED BROKEN DOOR LATCH ASSY.
- [SDR COMA9610145](https://openairdocs.org/sdr/COMA9610145), May 14, 1996: PROP CONTL UNIT. MALFUNCTION. LEFT PROPELLER TAKES 30 SECONDS TO TRANSITION FROM FEATHER TO BETA RANGE. REPLACED THE PROPELLER CONTROL UNIT.

All 60: https://openairdocs.org/deregistered/N247CA-2025-08-13/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 19990525033429I](https://openairdocs.org/incident/19990525033429I), May 25, 1999: Emb EMB120RT (N247CA), Indianapolis, IN. (-23) When the landing gear was selected to the down position no indication of the gear being or down was indicated. The landing was aborted and the flight…
- [Incident 19950129005889I](https://openairdocs.org/incident/19950129005889I), Jan 29, 1995: Emb EMB120RT (N247CA), Covington/Cinci, KY. Narrative: coma #4280, departed Cincinnati/Northern Kentucky international airport, Covington, Kentucky, 1000 local enroute to evansville, Indiana, after…

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