- Registered owner
- Air Evac Ems Inc
- Location
- O Fallon, MO
- Owner type
- Corporation
- Serial number
- 45782
- Year built
- 1983
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- September 16, 1983
- Certificate issued
- October 26, 2005
- Expires
- July 31, 2028
- Mode S code
- A098EE
Bell Helicopter Textron 206L-1TCDS H2SWAirframe · Bell Helicopter Textron 206L-1TCDS E1GLEngine · Allison 250-C28 series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Allison 250-C28 model are included below.
On this page
Airworthiness directives that may apply · 85
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1978 | 1 |
|---|---|
| 1979 | 2 |
| 1980 | 4 |
| 1981 | 3 |
| 1982 | 3 |
| 1983 | 2 |
| 1985 | 2 |
| 1986 | 7 |
| 1987 | 1 |
| 1988 | 2 |
| 1989 | 3 |
| 1991 | 4 |
| 1992 | 2 |
| 1994 | 3 |
| 1995 | 3 |
| 1996 | 3 |
| 1999 | 3 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 3 |
| 2005 | 3 |
| 2006 | 1 |
| 2007 | 2 |
| 2008 | 2 |
| 2009 | 2 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 3 |
| 2014 | 2 |
| 2015 | 1 |
| 2017 | 1 |
| 2018 | 1 |
| 2019 | 2 |
| 2021 | 4 |
| 2022 | 4 |
| 2023 | 2 |
| 2024 | 1 |
Airframe · Bell Helicopter Textron 206L-1
AD 2024-20-07Emergency Equipment; Emergency Flotation SectionAD 2023-11-07Ground Proximity SystemAD 2023-06-05Tail Rotor Drive ShaftInformation bulletins that may apply · 7
Advisory, not mandatory.
Airframe · Bell Helicopter Textron 206L-1
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-05-24SAIB SW-04-92Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N138AEMatched 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 206L-1 aircraft
FAA incident reports
No FAA accident or incident reports matched to N138AEMatched 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 206L-1 aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EVCA0202490600241Unknown · crackedCRACK IN 145 STATIONSDR EVCA09262023Frame · crackedCRACK IN R/H ROLLOVER CLOSE OUT PANEL APPROX 1 INCH LONG EXTENDING TO EDGE OF PANEL. P/N 206-031-117-443. THIS PART WILL PROBABLY HAVE TO BE REMOVED TO REPAIR THE FRAME MIGHT CONSIDER REPLACEMENT OF PANEL IF PROCURABLE.SDR EVCA2023011100001Blade · crackedVAN HORN MAIN ROTOR BLADE INBOARD TAB ATTACHMENT TO BLADE SURFACE HAS CRACKS AT BOTH INBOARD AND OUTBOARD ATTACH POINTS ON BOTH UPPER AND LOWER BLADE SURFACES.SDR EVCA20200104001Structure · crackedDURING 300 HOUR INSPECTION, AN AMT DISCOVERED CLIP P/N 206-033-306-008 CRACKED JUST FWD OF TB ATTACH ACCESS AREA IN THE UPPER R/H QUADRANT ADJACENT TO THE TR AND ELEVATOR BELL CRANK SUPPORT FITTING.SDR EVCA00007Chin Bubble · detachedAPPROX 3 NM NW OF AIRPORT HEARD A NOISE. A FEW MOMENTS PASSED AND THEN THERE WAS A "POP", A QUICK PRESSURE CHANGE AND AIRFLOW INTO THE COCKPIT. DISCOVERED THE GAPING HOLE WHERE THE CHIN BUBBLE SHOULD BE INSTALLED. IMMEDIATELY TURNED TOWARD THE AIRPORT AND NOTSDR EVCA00006Bulkhead · crackedDURING A ROUTINE INSP, MECHANIC FOUND CRACK ON BULKHEAD STA NR 142, WL 61, ON THE RT SIDE GENERATING FROM A NUTPLATE SCREW LOCATION.
STCs that may be installed · 465
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.