- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 3996
- Year built
- 2005
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- November 21, 2005
- Certificate issued
- May 3, 2011
- Expires
- May 31, 2027
- Mode S code
- A3E4D9
Eurocopter AS 350 B3TCDS H9EUAirframe · Eurocopter AS 350 B3TCDS E00054ENEngine · Turbomeca ARRIEL-2B1
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 98
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1985 | 1 |
|---|---|
| 1990 | 2 |
| 1999 | 1 |
| 2000 | 3 |
| 2001 | 2 |
| 2002 | 6 |
| 2003 | 8 |
| 2004 | 3 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 6 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 9 |
| 2011 | 4 |
| 2012 | 5 |
| 2013 | 11 |
| 2014 | 7 |
| 2015 | 4 |
| 2016 | 2 |
| 2017 | 5 |
| 2018 | 6 |
| 2019 | 3 |
| 2020 | 5 |
| 2021 | 16 |
| 2022 | 7 |
| 2023 | 2 |
| 2024 | 1 |
| 2025 | 4 |
| 2026 | 10 |
Airframe · Eurocopter AS 350 B3
AD 2026-20-03Placards and MarkingsAD 2026-16-01Main rotor driveAD 2026-14-02Indication/Recording SystemInformation bulletins that may apply · 9
Advisory, not mandatory.
Airframe · Eurocopter AS 350 B3
SAIB AIR-21-13Engine Emergency Shutdown SystemSAIB SW-17-23R2Fuel SystemSAIB SW-15-20Air Conditioning System WiringSAIB SW-15-04Cabin Ventilation Air Scoop DrainingSAIB SW-12-45Garmin Model 400W/500W Series GPS-WAAS Navigation SystemSAIB SW-11-07Star Flex Arm Failures on Eurocopter France Model AS350, AS355, and EC130 HelicoptersSAIB SW-07-22R1Serrated lock washersSAIB SW-07-13Oxygen Reserve CylinderSAIB SW-06-48 corrected 07/20/2006Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N350AMMatched 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 Eurocopter AS 350 B3 aircraft
FAA incident reports
No FAA accident or incident reports matched to N350AMMatched 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 Eurocopter AS 350 B3 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 2A6D2024043002Beam · damagedDAMAGE TO THE LH BEAM UNDER THE ENGINE DECK (P/N: 355A21-2110.25) IN THE FORM OF AN ELONGATED HOLE IN THE LOWER FLANGE NEAR THE AFT END OF THE PART. THE ORIGINAL HOLE IS 1/8” DIAMETER, AND THE ELONGATED HOLE WAS MEASURED TO BE APPROXIMATELY 0.4” X 0.2”.SDR 2A6D20240329001Xmsn Deck · chafedCHAFING DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK. THE DAMAGE MEASURES APPROXIMATELY 0.3” LONG, 0.1 WIDE WITH A MAXIMUM DEPTH OF 0.010".SDR 2A6D20210903001Bulkhead · chafedCHAFING DAMAGE TO THE AFT SIDE OF THE AFT CABIN BULKHEAD (PN 350A21-1032-86). ADDITIONALLY, THERE IS CHAFING DAMAGE TO THE VERTICAL SUPPORT (PN 350A21-1032-32).SDR 2A6D20210902001Deck Plate · damagedCHAFING DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK AT APPROXIMATE STATION X 3900, Z 1759, R/H Y 210. THE DAMAGE IS APPROXIMATELY 0.014” DEEP AND 1.2” LONG BY 0.2” WIDE.SDR 2A6D20200827001Deck Plate · dentedDAMAGE TO THE ENGINE DECK (PN: 350A21-1239.21) IN THE FORM OF SEVERAL DENTS. THE DAMAGE AREAS WERE DISCOVERED TO BE NEAR THE SCUPPER DRAIN HOLE AND AFT ON EITHER SIDE OF A STIFFENING FEATURE. THE LARGEST DENT WAS MEASURED TO BE APPROXIMATELY 1.20” X 0.20” AND SDR 2A6R2018042004732Frame · corrodedWHILE REMOVING CORROSION FROM THE UNDERSIDE OF THE LEFT SIDE OF THE COCKPIT FLOOR BELOW THE LITTER BASE MOUNT, FOUND CORROSION ON THE FRAME AT BS 1294.20.SDR 2A6R2018MG4731Structure · corrodedDURING INSPECTION, FOUND CORROSION ON THE LEFT & RIGHT EDGING OF THE FUSELAGE TO THE EXTENT THAT REPLACEMENTS HAD TO BE SPLICED IN.SDR QMLA2012081912135Starter Gen · burnedGENERATOR LIGHT ILLUMINATED IN CRUISE FLIGHT FOLLOWED IMMEDIATELY BY A STRONG ODOR OF BURNING AND VISIBLE SMOKE IN THE COCKPIT. ELECTED TO LAND. STARTER GENERATOR WAS ON FIRE.SDR QMLA2011101211098Clutch · brokenDURING FLIGHT OPERATIONS FLIGHT CREW STATED THAT WHEN THEY ENGAGED THE AIR CONDITIONING THERE WAS AN ELECTRICAL TYPE SMELL AND WHEN THE AIR CONDITIONING WAS DISENGAGED THE SMELL WOULD DISIPATE . THE ACFT DID NOT HAVE ANY WARNINGS OR CAUTIONS SO THEY PROCEEDED
STCs that may be installed · 401
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 401 STCs