- Registered owner
- Air Evac Ems Inc
- Location
- O Fallon, MO
- Owner type
- Corporation
- Serial number
- 51421
- Year built
- 1990
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- February 15, 2001
- Certificate issued
- October 26, 2005
- Expires
- September 30, 2028
- Mode S code
- A2C082
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Allison 250-C30 model are included below.
On this page
Airworthiness directives that may apply · 74
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1979 | 1 |
|---|---|
| 1980 | 2 |
| 1982 | 1 |
| 1983 | 1 |
| 1984 | 1 |
| 1985 | 3 |
| 1986 | 6 |
| 1987 | 1 |
| 1988 | 3 |
| 1989 | 2 |
| 1991 | 4 |
| 1992 | 2 |
| 1994 | 3 |
| 1995 | 3 |
| 1996 | 2 |
| 1999 | 3 |
| 2001 | 1 |
| 2002 | 1 |
| 2003 | 3 |
| 2004 | 2 |
| 2005 | 3 |
| 2006 | 2 |
| 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 |
See all 84 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Bell 206L-3
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-04-92Engine · Allison 250-C30 series
SAIB NE-06-52Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N277AEMatched 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 206L-3 aircraft
FAA incident reports
No FAA accident or incident reports matched to N277AEMatched 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 206L-3 aircraft
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR EVCA2020093003Disc Pack · corrodedDURING ROUTINE INSPECTION, NR 6 TAIL ROTOR DRIVE SHAFT DISC PACK HAS CORROSION BETWEEN DISCS.SDR EVCA201910100003Blade · corrodedBOTH RED & WHITE MR BLADES HAVE CORROSION IN BLADE PIN RETENTION RECEPTACLES. REMOVED MR BLADE ASSY(S). PN: 206-015-001-115, SN(S) BH482876 & BH482878, AND REPLACED WITH SERVICEABLE MR BLADES PN: 20633000-101, SN(S): A074 & A075. SEE FAA FORM 337 DATED 10/8/2SDR EVCA201803090001Structure · corrodedPILOT DISCOVERED A CRACK IN WING WALK COMPOUND LOCATED ON THE RT CABIN ROOF. INVESTIGATED AND FOUND CORROSION UNDER THE WING WALK COMPOUND.SDR EVCA20160215001Angle · crackedFOUND CRACKS AT BOX BEAM INTERFACE WITH FWD VERTICAL CONTROL TUNNEL ON RT SIDE. FOUND ANGLE, PN 206-033-110-229 & WEB PN 206-033-110-183, CRACKED. MAXIMUM CRACK LENGTH OF APPROX 2 INCHES.SDR EVCA201307120040Bulkhead · crackedON A ROUTINE INSPECTION, THE MECHANIC FOUND THE LT BULKHEAD CRACKED AT TWO LOCATIONS, THE LOCATION OF THE LT BULKHEAD IS AT BS 145. THIS WAS LOCATED BY VISUAL INSPECTION DUE TO THE FACT THE RIVETS WERE WORKING AND MAKING "MUD".
STCs that may be installed · 471
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.