- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 3941
- Year built
- 2005
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 22, 2005
- Certificate issued
- January 27, 2012
- Expires
- January 31, 2028
- Mode S code
- A837B8
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 N629AMMatched 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 N629AMMatched 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
Reports on N629AM not matched to an aircraft · 1
They name N629AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6D20251106001Bulkhead · chafedCHAFING DAMAGE ON THE LT LONGITUDINAL BULKHEAD (X-FRAME) ON THE UPPER INBD FACE MEASURING APPROXIMATELY 0.017" IN DEPTH, 0.10" IN WIDTH, AND 0.210" IN LENGTH. THE DAMAGE WAS REPAIRED WITH A DOUBLER IAW AIR METHODS ENGINEERING AUTHORIZATION 33-5300-EA-5308.SDR 2A6D20251105001Beam · chafedDAMAGE TO THE RH Y398.5 BEAM (P/N: 350A211351.22) AND STOP DOUBLER (P/N: 350A211363.25) IN THE FORM OF A CHAFE. THE CHAFE DAMAGE IS NEAR THE FWD UPPER SIDE OF THE CUTOUT AND WAS MEASURED TO BE APPROXIMATELY 0.4" IN LENGTH AND 0.040" IN DEPTH.SDR 2024FA0000301Floor Skin · crackedCRACK DISCOVERED AT R/H UPPER FASTENER HOLE FOR AFT FUEL TANK SADDLE ON OUTBOARD SIDE.SDR 2A6D20240402001Xmsn Deck · chafedCHAFING DAMAGE WAS DISCOVERED ON THE L/H SIDE TRANSMISSION DECK.SDR QMLA2020092820049Starter Gen · malfunctionedON SEPTEMBER 24TH 2020, AT APPROXIMATELY 15:30, THE GENERATOR ON AIRCRAFT N629AM FAILED IN FLIGHT. THE AIRCRAFT LOST ELECTRICAL POWER AND THE RADIOS AND VEMD WENT OFFLINE. THE PILOT EXECUTED A PRECAUTIONARY LANDING AT AN OFF AIRPORT LOCATION. AFTER LANDING,SDR 2A6D202007244001Floor Panel · corrodedTHERE IS CORROSION DAMAGE TO THE CABIN FLOOR PANEL EDGINGSDR 2A6D202007230001Bulkhead · chafedCHAFING DAMAGE WAS DISCOVERED ON THE LH LATERAL BULKHEAD (X FRAME) (PN: 350A21-1051) ON THE INBOARD FACE. THE CHAFE DAMAGE IS OUTLINED BELOW AND SHOW IN IN FIGURE 1. THE DAMAGE IS LOCATED ON THE INTERIOR (INBOARD) SIDE OF THE X FRAME. L/H AFT LOWER LEG STA 364SDR QMLA2018042418049Fan · odorDURING FINAL APPROACH, HAD A BURNING ODOR COME THROUGH AC VENTS. SHUT OFF AC COMPRESSOR, AND ODOR CLEARED. THE CONDENSER FAN WAS CAUSING THE ODOR. THE FAN WAS REMOVED AND REPLACED.
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