- Registered owner
- Air Evac Ems Inc
- Location
- O Fallon, MO
- Owner type
- Corporation
- Serial number
- 45660
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Certificate issued
- October 26, 2005
- Expires
- July 31, 2028
- Mode S code
- A16F9E
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 64
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1980 | 3 |
|---|---|
| 1981 | 3 |
| 1982 | 1 |
| 1983 | 1 |
| 1985 | 2 |
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 2 |
| 1989 | 2 |
| 1991 | 4 |
| 1992 | 2 |
| 1994 | 3 |
| 1995 | 3 |
| 1996 | 2 |
| 1999 | 2 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 1 |
| 2007 | 2 |
| 2008 | 2 |
| 2009 | 2 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 3 |
| 2014 | 2 |
| 2015 | 1 |
| 2017 | 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 N192AEMatched 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 · 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EVCA202404150001B-Nut · looseCREW REPORTS STRONG FUEL SMELL IN AFT CABIN. FINDINGS: REMOVED CENTER AFT FACING SEAT PANEL AND ACCESS COVER TO GAIN ACCESS TO FUEL SYSTEM. FOUND FUEL SEEPING AT AFT B-NUT OF EJECTOR PUMP. TIGHTENED B-NUT AND PERFORMED LEAK CHECK WITH BOOST PUMPS ON WITH NO LSDR EVCA2024041000001Panel · crackedDURING SCHEDULED MAINTENANCE EVENT AMT FOUND 2.0" LONG CRACK IN AIRFRAME AT OIL COOLER BLOWER SHAFT HANGER ASSEMBLY, AFT RH, ATTACHMENT POINT. APPROXIMATE STA 209.0, WL 73.586.SDR EVCA201711131Tach Generator · failedDURING FLIGHT PILOT LOST HYDRAULIC POWER TO FLIGHT CONTROLS AND PERFORMED AN UNPLANNED LANDING AT AN AIRPORT. DURING MAINTENANCE INVESTIGATION IT WAS FOUND THAT THE SPLINES IN THE TACHOMETER GENERATOR DRIVE THAT DRIVE THE SHAFT FOR THE HYDRAULIC PUMP HAD FAILESDR EVCA201608061Attach Fitting · crackedUPPER LT TAILBOOM ATTACHMENT FITTING, PN: 206-032-409-001P, CRACKED.SDR EVCA00004Frame · crackedDURING THE INSTALLATION OF A BELL KIT (BHT-SI-2050) TAILBOOM REQUIRED REMOVAL FOR REPLACEMENT. AFTER REMOVAL OF TAILBOOM, CRACKED NOTICED ON AIRFRAME AFT BULKHEAD RING. AIRFRAME AFT BULKHEAD RING R & R.
STCs that may be installed · 459
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.