N912EM1994 Eurocopter AS 355N
This N-number isn't registered right now. Below is its last known registration, canceled Nov 8, 2016.
Safety record in brief:No NTSB accidents or incidents since 19828 ADs may apply5 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Avcorp US Registrations LLC Trustee
- Owner type
- Corporation
- City, state
- Wilmington, DE
- Certificate issued
- Sep 1, 2016
- Canceled
- Nov 8, 2016
- Airworthiness
- Standard · Normal
- Airworthiness date
- Mar 20, 2003
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
- Eurocopter
- Model
- AS 355N
- Year
- 1994
- Serial number
- 5560
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 6
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Type certificate data sheet
- H11EU
- Mode S code
- AC9E89
Engine
- Make and model
- Turbomeca Arrius 1a
- Type
- Turbo-shaft
- Power
- 456 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2016Avcorp US Registrations LLC TrusteeWilmington, DE
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.
ADs published since 1998 that may apply (8)
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 |
|---|---|---|---|
| 2021-04-15 | Vertical Stabilizer, Spar/Rib | Mar 23, 2021 | Airframe (AS 355N)Only with: AS350B3 helicopters excluded if Modification 07.3148 embodied in production or Eurocopter AS350 Service Bulletin 55.00.14 (any revision) embodied in service; AS355 models all serial numbers. |
| 2013-23-09 | Eurocopter France Helicopters | Dec 27, 2013 | Airframe (AS 355N)Only with: Helicopters with sliding doors installed, except those with modification AL.4262. |
| 2013-21-01 | Eurocopter France (Eurocopter) Helicopters | Oct 25, 2013 | Airframe (AS 355N)Only with: Tail rotor hub pitch horn assembly P/N 350A121368.01, .02, .03, or .04, with pitch horn P/N 350A121368.XX, installed. |
| 2013-08-19 | Eurocopter France Helicopters | Jun 5, 2013 | Airframe (AS 355N)Only with: Sliding door pre-modification (MOD) 073298 or pre-MOD 073308 installed. |
| 2010-11-51 | Eurocopter France (Eurocopter) Model AS350B, BA, B1, B2, C, D, and D1 Helicopters and… | Sep 2, 2010 | Airframe (AS 355N)Only with: Tail gearbox control lever P/N 350A33-1058-00, -01, -02, or -03 not marked with an "X" near the P/N installed. |
Show all 8 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2009-21-11 | Turbomeca S.A. ARRIUS 1A Turboshaft Engines | Nov 20, 2009 | Engine (ARRIUS 1A)Only with: Balancing pistons P/N 0 319 20 152 0 installed. |
| 2005-11-01 | Turbomeca S.A. Arrius 1A Turboshaft Engines | Jun 13, 2005 | Engine (ARRIUS 1A) |
| 2000-06-09 | Turbomeca Arrius 1A Series Turboshaft Engines | Jun 12, 2000 | Engine (ARRIUS 1A) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (5)
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.
- Tail rotor drive · bearing · failedDec 9, 2005
AC ON NORMAL FLIGHT. AT END OF FIRST LEG OF FLIGHT, PILOT SHUTDOWN THE ENGINES. PILOT THEN NOTICED A NOISE NEAR THE REAR OF AC. MAINT WAS NOTIFIED AND AC WAS GROUNDED UNTIL FURTHER NOTICE. AC WAS MOVED BY TRUCK TO HANGER. DISASSEMBLY WAS CONTINUED AND FOLLOWING PART HAD TO BE REPLACED DUE TO…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · starter gen · vibrationDec 10, 2004
STARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND THE STARTER WAS REMOVED AND THE STARTER GEN ADAPTER WAS FOUND TO HAVE 2 MOUNTING FLANGES BROKEN OFF AND ONE CRACKED. THINK THAT THE STARTER GEN VIBRATION SHOULD BE CHECKED EVERY 25…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust pipe · vibrationDec 10, 2004
STARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND THE STARTER WAS REMOVED AND REPLACED WITH O/H STARTER GEN. SERVICEABLE EXHAUST PIPE WAS INSTALLED. (CE07200506287) (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Electrical power · starter gen · vibrationDec 10, 2004
STARTER GEN VIBRATION WAS CHECKED AFTER A NR 1 ENGINE EXHAUST PIPE WAS FOUND CRACKED. VIBRATION WAS ABOVE LIMITS AND THE STARTER WAS REMOVED AND REPLACED WITH O/H STARTER GEN. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Exhaust · exhaust pipe · failedOct 26, 2004
(3) OUT OF (4) STRUTS THAT HOLD THE OUTSIDE PART OF THE EXHAUST ON FAILED. TT OF THE PART IS UNKNOWN. MFG THINKS THE PROBLEM IS RELATED TO A HIGH VIBRATION IN THE STARTER GEN. THE VIBRATION LEVEL WAS .04 WHICH IS WELL BELOW THE LIMIT. (CE07200502200) (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.
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