- Registered owner
- Air Evac Ems Inc
- Location
- O Fallon, MO
- Owner type
- Corporation
- Serial number
- 52425
- Year built
- 2011
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- March 7, 2011
- Certificate issued
- December 7, 2022
- Expires
- December 31, 2029
- Mode S code
- A3F765
Bell Helicopter Textron Canada 206L-4TCDS H2SWAirframe · Bell Helicopter Textron Canada 206L-4TCDS E1GLEngine · Rolls-Royce 250-C30P
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 55
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1980 | 2 |
|---|---|
| 1982 | 1 |
| 1983 | 1 |
| 1986 | 5 |
| 1988 | 1 |
| 1989 | 1 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 1 |
| 1999 | 5 |
| 2001 | 2 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 2 |
| 2007 | 2 |
| 2008 | 2 |
| 2009 | 2 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 4 |
| 2014 | 2 |
| 2015 | 2 |
| 2017 | 1 |
| 2018 | 1 |
| 2019 | 2 |
| 2021 | 4 |
| 2022 | 4 |
| 2023 | 2 |
| 2024 | 1 |
Airframe · Bell Helicopter Textron Canada 206L-4
AD 2024-20-07Emergency Equipment; Emergency Flotation SectionAD 2023-11-07Ground Proximity SystemAD 2023-06-05Tail Rotor Drive ShaftInformation bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Bell Helicopter Textron Canada 206L-4
SAIB SW-19-05Tail Rotor Drive System, Spline DamageSAIB SW-18-02Loss of Hardware Tail Rotor Drive Shaft CouplingsSAIB SW-12-45Garmin Model 400W/500W Series GPS-WAAS Navigation SystemSAIB SW-10-42R1Emergency Float KitsSAIB SW-08-42Emergency Float with Liferaft Kits (kits)SAIB SW-05-87SAIB SW-05-24SAIB SW-04-92Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N355AEMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Bell Helicopter Textron Canada 206L-4 aircraft
Investigations on N355AE not matched to an aircraft · 1
They name N355AE, but no registry record covers the date, the aircraft registered then was built later, or the investigation describes another aircraft.
FAA incident reports
No FAA accident or incident reports matched to N355AEMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Bell Helicopter Textron Canada 206L-4 aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EVCA0202450300024Rivet · shearedRIVET SHEARED ON TRANSMISSION DECK, LEFT HAND SIDE NEXT TO LEFT REAR NODAL BEAM SUPPORT. UPON INSPECTION OF RIVETS, FOUND CRACK IN STRUCTURE AT APPROXIMATELY STA 155, BL 13-16, WL 71-73 UNDERNEATH L/H REAR NODAL BEAM DECK MOUNT.SDR EVCA202209290001Blower Motor · odorELECTRICAL SMELL NOTED DURING FLIGHT. FOUND TO BE THE FORWARD AIR CONDITIONER BLOWER MOTOR.SDR EVCA201707180001Attach Fitting · crackedFOUND LT TAILBOOM ATTACHMENT FITTING PN: 206-031-403-005 TO HAVE A 1.6" LONG CRACK. FITTING LOCATED ON TAILBOOM SIDE OF BULKHEAD.SDR EVCA201610061Elec Connector · burnedWHILE FLYING PILOT AND PASSENGERS REPORTED A BURNING SMELL WHEN AIRCRAFT WAS APPROACHING BASE FOR LANDING. DURING INSPECTION, MECHANIC FOUND THE MOLEX CONNECTOR WAS MELTED ON THE BRACKET TO THE AFT BLOWER MOTOR HOUSING.
STCs that may be installed · 369
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.