- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 4613
- Year built
- 2009
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- February 23, 2009
- Certificate issued
- August 4, 2015
- Expires
- August 31, 2028
- Mode S code
- A75D51
American Eurocopter AS350B3TCDS H9EUAirframe · American Eurocopter AS350B3TCDS E00054ENEngine · Turbomeca ARRIEL-2B1
From the FAA registry file of October 22, 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 · American Eurocopter AS350B3
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 · American Eurocopter AS350B3
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 N574AMMatched 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 American Eurocopter AS350B3 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6D20231102001Floor Support · corrodedCORROSION WAS FOUND ON THE CABIN FLOOR EDGING ON THE LH AND RH SIDE (P/N: 350A21-1359-20/21)SDR 2A6D20220623001Support Beam · elongatedDAMAGE WAS DISCOVERED ON THE L/H 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 PARTSDR 2A6D2021070185002Deck Plate · chafedTHE RH TRANSMISSION DECK EDGING (PN 350A21-1041-22) HAS A GOUGE THAT IS UP TO 0.200” IN DIAMETER AND ALMOST THROUGH THE PART.SDR QMLA2020122120068Structure · separatedRT LOWER MAIN GEARBOX COWLING DEPARTED AIRCRAFT IN FLIGHT AND STRUCK THE TAIL ROTOR OF THE AIRCRAFT AFTER THE IMPACT THE AIRCRAFT HAD TO MAKE A PRECAUTIONARY LANDING. THIS AIRCRAFT REMAINS OUT OF SERVICE AT THIS TIME WHILE ALL OF THE REQUIRED INSPECTIONS ARE SDR 2A6D20201116001Floor Panel · corrodedCORROSION WAS DISCOVERED ON THE RIGHT HAND SIDE CABIN FLOOR EDGE SECTION (AIRBUS PN 350A21-1359) RANGING FROM STA 1120 TO 2437.SDR 2A6D20201112001Skin · dentedAC 4613 HAS A SMOOTH DENT ON THE TAILBOOM’S RT SKIN LOCATED AT APPROXIMATELY STA 8098, WL 1829, AND BL 70R JUST FORWARD OF THE HORIZONTAL STABILIZER OPENING. THE DENT IS .4 BY .4 AND .035 AT ITS DEEPEST.SDR 2A6D20201109001Deck Plate · dentedA/C 4613 HAS SEVERAL DENTS LOCATED ON THE ENGINE DECK LOCATED AT APPROXIMATELY STA 4387, WL 1759, AND BL 650L. THE DAMAGE IS IN AN AREA 2.4 BY 1.8 WITH THE DEEPEST DENT MEASURING .045. THE DENTS ARE LOCATED ABOVE A FRAME WHICH IS UNDAMAGED.SDR 2A6R04012019Frame · chafedCHAFING NOTED ON THE LEFT HAND X-FRAME P/N: 350A21-1051SDR QMLA2015123015112Unknown · odorPILOT & CREW REPORTED STRONG BURNING RUBBER SMELL IN COCKPIT AT ENG RUN UP TO IDLE. PILOT ABORTED FLIGHT & CALLED MECHANIC. CHECKED ACFT SYS, FINDING NO OBVIOUS DEFECTS. HAD PILOT RUN ENG AT IDLE & FULL POWER WHILE CHECKING VARIOUS SYSTEMS INCLUDING BLEED ASDR QMLA2013012513016Access Panel · crackedFOUND 10MM CRACK IN TAILBOOM MOUNTED BATTERY ACCESS DOOR, TOP RT CORNER, DURING 100HR A/F INSPECTION.SDR QMLA2011062311071Unknown · smokeSMOKE IN CABIN FRONT LT SIDE OF INSTRUMENT PANEL, WHILE IN HOVER. PERFORMED COMPLETE INSP OF AFFECTED AND SURROUNDING AREAS. NO EVIDENCE OF SMOKE OR FAULTY WIRING FOUND. SUSPECT SMOKE WAS POSSIBLY CHAFED FROM GLARESHIELD/WINDSHIELD CENTER POST, BLOWN THRU V
Reports on N574AM not matched to an aircraft · 1
They name N574AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
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
Earlier aircraft with this N-number · 1
This aircraft carried N574AM before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.