N247CA1991 Embraer EMB-120ER
This N-number isn't registered right now. Below is its last known registration, canceled Aug 13, 2025.
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply54 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Uas Transervices INC
- Owner type
- Corporation
- City, state
- Boca Raton, FL
- Certificate issued
- Jan 10, 2014
- Canceled
- Aug 13, 2025
- Airworthiness
- Standard · Transport
- Airworthiness date
- Apr 13, 2001
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Embraer
- Model
- EMB-120ER
- Year
- 1991
- Serial number
- 120.225
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 32
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A24A33
Engine
- Make and model
- P&W Canada Pw118b
- Type
- Turbo-prop
- Power
- 1800 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2014 – 2025Uas Transervices INCBoca Raton, FL
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (6)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2025-02-09 | Fuselage | Mar 18, 2025 | Airframe (EMB-120ER) |
| 2017-10-04 | Landing Gear | Jun 29, 2017 | Airframe (EMB-120ER) |
| 2013-15-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Sep 17, 2013 | Engine (PW118B)Serial numbers per Table 1 of the Appendix of P&WC Service Bulletin No. PW100-72-21823, Revision 3. Only with: First-stage power turbine blade P/N 3120973-01, 3120983-01, or 3054053-01 installed with a serial number listed in the referenced SB table. |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (PW118B)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs. |
| 2008-04-18 R1 | EMBRAER Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes | Nov 16, 2009 | Airframe (EMB-120ER) |
Show all 6 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2007-26-21 | EMBRAER Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes | Feb 20, 2008 | Airframe (EMB-120ER) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (54)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Fuselage · strap · corrodedAug 3, 2000
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 WITH THE EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · damagedAug 3, 2000
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 SKIN WAS REPAIRED IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3745-1,IR,7-25-00.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · angle · crackedAug 3, 2000
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 ACORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, IR, 7-6-99.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Doors · skin · gougedAug 3, 2000
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 MANUAL STANDARD PRACTICES AND EMB-120 SRM 52-30-01, FIGURE 201.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · shear tie · crackedAug 3, 2000
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 EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, IR, 2-16-93.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · dentedAug 3, 2000
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 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMB120 SRM 53-00-01, FIGURE 201.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · gougedAug 3, 2000
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 IN ACCORDANCE WITH EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR NR SST-1872/00 DATED 7-25-00.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Nacelles and pylons · bulkhead · crackedAug 3, 2000
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 ACCORDANCE WITH EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 33712-1, IR-7-28-00.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · channel · crackedAug 3, 2000
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 STUCTURAL REPAIR MANUAL STANDARD PRACTICES.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Ice and rain protection · boot · leakingMar 11, 2000
WING DE-ICE FAIL WARNING. REPLACED THE RIGHT WING INBOARD DE-ICE BOOT.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 54 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026