- Registered owner
- Air Evac Ems Inc
- Location
- O Fallon, MO
- Owner type
- Corporation
- Serial number
- 52436
- Year built
- 2012
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- April 2, 2012
- Certificate issued
- August 18, 2018
- Expires
- August 31, 2028
- Mode S code
- A3AC1E
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 N336AEMatched 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
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EVCA202007302Blade · crackedTWO CRACKS FOUND ON MAIN ROTOR BLADE NICKEL ABRASION STRIP AT BLADE STATION 204.5 EXTENDING CORD WISE 40 % AND 30% OF LEADING EDGE.SDR EVCA202007301Blade · crackedCRACK FOUND ON MAIN ROTOR BLADE NICKEL ABRASION STRIP AT BLADE STATION 203 EXTENDING CORD WISE 60% OF LEADING EDGE.SDR EVCA20201210001Blade · delaminatedDURING PERIODIC INSPECTIONS MAIN ROTOR BLADE PN: 206-015-001-115 SN: A-7245 TRAILING EDGE WAS FOUND TO BE CRACKED AND DELAMINATED. DELAMINATION SPANS FROM 142 INCHES TO 150 INCHES FROM ROOT END. THE CRACK IS WITHIN THE DELAMINATED AREA AT 146.5 INCHES FROM ROOSDR EVCA201802021Mount · crackedWHILE PERFORMING SCHEDULED 100 HOUR INSPECTION, NOTED A 1.5 INCH CRACK IN THE TAILBOOM MOUNTING RING EXTENDING FROM THE UPPER LT MOUNTING HOLE TO THE EDGE OF THE BULKHEAD.
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.