N639ASEmbraer EMB-120ER
This N-number isn't registered right now. Below is its last known registration, canceled May 5, 2006.
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply21 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Individual owner
- City, state
- Providenciales
- Canceled
- May 5, 2006
- Airworthiness
- Standard · Transport
- Airworthiness date
- Sep 4, 1993
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
- Serial number
- 120.283
- 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
- A85F3C
Engine
- Make and model
- P&W Canada Pw118
- 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- until 2006Individual ownerProvidenciales
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) |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (PW118)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) |
| 2007-26-21 | EMBRAER Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes | Feb 20, 2008 | Airframe (EMB-120ER) |
Show all 6 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2003-21-03 | Pratt & Whitney Canada Models PW118, PW120, PW120A, and PW121 Turboprop Engines | Nov 20, 2003 | Engine (PW118) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (21)
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.
- Lights · wire · looseJul 14, 2003
FLT 4824 - DURING A GROUND INSPECTION IN DFW, THE GALLEY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED LOOSE WIRING TO THE EMERGENCY LGIHTS UNDER THE GALLEY FLOOR. OPERAITONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery pack · inoperativeMay 31, 2003
FLT 4894 - DURING A GROUND INSPECTION IN DFW, THE FORWARD AND OVERHEAD EMERGENCY LIGHTS DIMMED OUT AFTER APPROXIMATELY TWO SECONDS WHILE THE REMAINING LIGHT STAYED ON. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · seal · looseFeb 21, 2003
FLT 4955 - DURING CLIMB-OUT FROM DFW-AEX, AT APPROXIMATELY 25,000 FT CABIN PRESSURIZATION STARED TO CLIMB RAPIDLY. THE CREW MADE AN EMERGENCY DESCENT AND LEVELED OFF AT APPROXIMATELY 9,000 FEET. THE AIRCRAFT LANDED SAFELY IN AEX. S/D - MAINTENANCE RE-INSTALLED THE LOOSE CARGO DOOR SEAL INTO ITS…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · stringer · corrodedJul 15, 2002
DURING C-CHECK INSPECTION IN BNA, STRINGER 21 LEFT WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 12 AND 13. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTION OF STRINGER IAW SRM'S 53-00-00 AND 51-21-02. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · stringer · corrodedJul 15, 2002
DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND OUT OF LIMITS ON STRINGER 18 LEFT BETWEEN FRAMES 13A AND 15A. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER SECTION IAW SRM'S 51-25-00 AND 51-40-02. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · stringer · corrodedJul 15, 2002
DURING C-CHECK INSPECTION IN BNA, STRINGER 17 LEFT WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 20 AND 22. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 51-40-02. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · crossbeam · corrodedJul 15, 2002
DURING C-CHECK INSPECTION IN BNA, CORROSION WAS FOUND OUT OF LIMITS ON THE CROSS BEAM AT FRAME 15 NEAR THE PASSENGER ENTRY DOOR. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM'S 51-25-00, 51-21-00 AND 51-40-02. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · crossbeam · corrodedJul 15, 2002
DURING C-CHECK INSPECTION IN BNA, THE CROSSBEAM AT FRAME 16 WAS FOUND TO BE CORRODED BEYOND LIMITS BETWEEN THE RIGHT BUTT STRAP AND THE RIGHT FLOOR SILL. MAINTENANCE REMOVED AND REPLACED THE CORRODED CROSSBEAM IAW SRM 51-40-02. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · sill · corrodedJul 15, 2002
DURING C-CHECK INSPECTION IN BNA, THE RIGHT BUTT STRAP FLOOR SILL WERE FOUND TO BE CORRODED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED THE CORRODED BUTT STRAP AND FLOOR SILL IAW SRM'S 53-00, 51-25-00, AND 51-40-02. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · butt strap · corrodedJul 15, 2002
DURING C-CHECK INSPECTION IN THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 13 AND 15. ANOTHER LEFT BUTT STRAP WAS CORRODED BETWEEN FRAMES 14 AND 21. MAINTENANCE REMOVED AND REPLACED THE CORRODED SECTIONS OF BUTT STRAP IAW SRM 51-25-00, 51-21-02, AND 51-40-02 E25. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 21 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