- Registered owner
- Air Evac Ems Inc
- Location
- O Fallon, MO
- Owner type
- Corporation
- Serial number
- 53367
- Year built
- 1999
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 13, 2010
- Certificate issued
- August 26, 2010
- Expires
- February 29, 2028
- Mode S code
- A6318C
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 49
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1982 | 1 |
|---|---|
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 4 |
| 1999 | 4 |
| 2000 | 6 |
| 2001 | 4 |
| 2002 | 5 |
| 2003 | 4 |
| 2004 | 1 |
| 2005 | 3 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 4 |
| 2011 | 2 |
| 2012 | 3 |
| 2013 | 5 |
| 2014 | 1 |
| 2015 | 2 |
| 2018 | 1 |
| 2019 | 2 |
| 2021 | 2 |
| 2023 | 4 |
| 2024 | 2 |
| 2025 | 1 |
| 2026 | 2 |
See all 72 ADs
Information bulletins that may apply · 7
Advisory, not mandatory.
Airframe · Bell 407
SAIB SW-15-20Air Conditioning System WiringSAIB 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-05-70SAIB SW-04-92Engine · Allison 250-C47B
SAIB NE-06-12R1Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N499AEMatched 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 407 aircraft
FAA incident reports
No FAA accident or incident reports matched to N499AEMatched 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 407 aircraft
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EVCA08182023Motor · unknownSMOKE IN COCKPIT. AFT A/C BLOWER MOTOR INOP.SDR EVCA202210250001Line · looseWE FOUND THE RETURN LINE INSIDE THE MAIN FUEL CELL HAND TIGHT WHICH CAUSE A FUEL LEAK AND THE SMELL OF FUEL IN THE CABIN.SDR EVCA202210240001Fuel Cell · leakingFUEL SMELL NOTED IN FLIGHTSDR EVCA202201210001Fuel · odorCREW NOTED A FUEL SMELL IN FLIGHT AND RETURNED TO BASESDR EVCA2020030600000Freewheel Unit · crackedDURING PERIODIC INSPECTION, THE FREEWHEELING UNIT HOUSING WAS VISUALLY DISCOVERED TO BE CRACKED ON THE MATING SURFACE TO THE ENGINE. THE CRACK EXTENDED APPROXIMATELY 0.5 INCHES FROM THE ATTACHMENT HOLE.SDR EVCA201607221Computer · failedUPON DEPARTURE FROM HOSPITAL HELIPAD AT APPROXIMATELY 100 FT AGL PILOT REPORTED EXPERIENCING A COMPLETED FADEC FAILURE. FADEC FAIL AND FADEC MAN CAUTION LIGHTS ILLUMINATED AND FADEC WARNING HORN SOUNDED. N2 AND NR IMMEDIATELY DECREASED. UPON INSPECTION THE FADSDR EVCA20150930Gearbox · unserviceableWHEN PERFORMING OIL CHANGE OF TAIL ROTOR GEARBOX, FOUND OIL REMAINING IN GEARBOX TO ONLY MEASURE APPROX 1 OZ. FLUID LOSS APPEARED TO ORIGINATE FROM TAIL ROTOR PITCH CHANGE CONTROL ROD SEAL.SDR EVCA2014042800058Compressor · crackedENG COMPRESSOR SCROLL CRACKED.SDR EVCA2012111200038Spline · failedIN FLIGHT, HYD CAUTION LIGHT ILLUMINATED FOLLOWED WITH IN 10-15 SECONDS A COMPLETE LOSS OF HYD PRESSURE. PILOT PERFORMED EMERGENCY PROCEDURE UNABLE TO RESTORE HYD PRESSURE. LANDED AS SOON AS PRATICAL. MX REMOVED THE HYD PUMP BUT FOUND THE TRANSMISSION OIL PUM
STCs that may be installed · 327
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 327 STCs