- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 4311
- Year built
- 2007
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- October 19, 2007
- Certificate issued
- September 27, 2013
- Expires
- September 30, 2029
- Mode S code
- A7032E
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 N551AMMatched 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 N551AMMatched 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2012091312151Unknown · odorDURING FLIGHT, PPROXIMATELY 5 MINUTES FROM DESTINATION HEARD A POP ON THE LT SIDE OF THE ACFT. OPERATIONS SEEMED NORMAL. ON LANDING, THERE WAS A FAINT RUBBER BURNING ODOR NOTED IN THE AIRCRAFT. DID A NORMAL SHUTDOWN, INSPECTED THE ACFT AND FOUND NOTHING UNUSDR QMLA2012090712148Wire · shortedWHEN THE INSTRUMENT LIGHTS WERE TURNED ON SPARKS EMINATED FROM BEHIND AND BELOW THE INSTRUMENT PANEL, LANDED ON THE PILOT'S FEET AND IMMEDIATELY EXTINGUISHED. MECHANIC ADDED. INSPECTED AREA INDICATED BY PILOT FOUND WIRE FROM NVIS GOOSE NECK LIGHT CHAFED AND SDR QMLA2012072312123Horn · crackedTAIL ROTOR PITCH CHANGE HORN CRACKED: VISIBLE FROM THE OTBD FACE OF THE TAIL ROTOR PITCH CHANGE HORN, RUNNING TANGENT FROM THE BOLT HOLE, ALONG THE EDGE THICKNESS, TO THE EDGE OF THE CONICAL INSERT ON THE INBD FACE. WITH THE ROTOR BRAKE SET AND APPLYING FORCESDR QMLD201112054591Guide Vane · crackedWHILE DISASSEMBLING ENGINE TO PERFORM MODIFICATION TU 166 FOUND THE POWER TURBINE NOZZLE GUIDE VANE CRACKED. MODULE 3 MUST BE RETURNED TO MFG FOR REPAIR.SDR QMLA2011061711067Air Filter · overservicedENGINE INLET FILTER OVER SERVICED, EXCESS OIL ACCUMUATED IN INLET TO ENGINE AND SMOKED WHEN OPERATING TEMPS IN ENGINE BECAME HOT.
Reports on N551AM not matched to an aircraft · 4
They name N551AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2002FA0001303Tube · failedPILOTS COMPLAINT OF RT ANTI-ICE HOT MESSAGE WHEN SYSTEM TURNED ON. VERIFIED SENSOR AND LOGIC CARD OPERATION OK. REMOVED RT LEADING EDGE AND FOUND MAIN TUBE HAD BURST WITH A 2.5 X .375 INCH HOLE, BLOWING AWAY INSULATION AROUND ASSEMBLY. THIS WAS JUST INBOARD OFSDR 2002FA0000662Magnetic Seal · wornCREW RECEIVED ENGINE CHIP-L CAS MESSAGE. AIRCRAFT LANDED AT DESTINATION. MAGNETIC INDICATOR PLUG INSPECTED AND SINGLE SLIVER FOUND. 3RD INCIDENT OF THIS NATURE ON THIS ENGINE. ANALYSIS BY ROLL-ROYCE ON 2ND INCIDENT SLIVER SHOWED STAINLESS 410 ALLOY. FOUND WAVESDR 2002FA0000363Duct · out of positionLEADING EDGES REMOVED FOR INSPECTION IT WAS DISCOVERED THE BLEED AIR TUBE IN BOTH SIDES, P/N UNAVAILABLE, HAD MIGRATED OUTBOARD. THE RETAINING SHEET METAL DIFFUSER WAS GOUGING INTO THE WELDED -T-.
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