- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 7293
- Year built
- 2011
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- January 2, 2013
- Certificate issued
- January 21, 2021
- Expires
- January 31, 2028
- Mode S code
- A08712
Eurocopter France EC 130 B4TCDS H9EUAirframe · Eurocopter France EC 130 B4TCDS E00054ENEngine · Turbomeca ARRIEL-2B1
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 64
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2002 | 1 |
|---|---|
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 2 |
| 2007 | 4 |
| 2008 | 3 |
| 2009 | 2 |
| 2010 | 7 |
| 2011 | 3 |
| 2012 | 4 |
| 2013 | 4 |
| 2014 | 6 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 4 |
| 2018 | 2 |
| 2019 | 2 |
| 2020 | 5 |
| 2021 | 10 |
| 2022 | 3 |
| 2023 | 2 |
| 2024 | 1 |
| 2025 | 7 |
| 2026 | 7 |
Airframe · Eurocopter France EC 130 B4
AD 2026-20-03Placards and MarkingsAD 2026-16-01Main rotor driveAD 2026-14-02Indication/Recording SystemInformation bulletins that may apply · 5
Advisory, not mandatory.
Airframe · Eurocopter France EC 130 B4
SAIB SW-17-23R2Fuel SystemSAIB SW-15-20Air Conditioning System WiringSAIB SW-12-45Garmin Model 400W/500W Series GPS-WAAS Navigation SystemSAIB SW-12-17Autopilot SystemSAIB SW-11-07Star Flex Arm Failures on Eurocopter France Model AS350, AS355, and EC130 HelicoptersHistorical bulletins · 1
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R1124202574604Skin · damagedOVERSIZED FASTENER HOLE DAMAGE WAS FOUND ON THE L/H FUSELAGE SKIN (P/N: 350A210053.BW), FWD FRAME ANGLE (P/N: 350A211036.28), AFT FRAME (P/N: 350A211240.00), LOWER FRAME (P/N: 350A211245.22), AND MAINTENANCE STEP (P/N: 350A21137.20) DURING REMOVAL AND REPLACEMSDR 2A6R2025111804604Angle · damagedDAMAGE WAS IDENTIFIED ON THE ATTACHMENT ANGLE (PN 350A21-4064-21), AS ILLUSTRATED IN FIGURE 1 OF DOCUMENT 17-5300-EA-5339, REV. –. THE DAMAGED COMPONENT, LOCATED BENEATH THE MAIN CABIN FLOOR AT BS 845 AND SHOWN IN THE SAME FIGURE, COULD NOT BE OBTAINED IN TIMESDR 2A6R1118202574602Xmsn Deck · chafedCHAFING DAMAGE WAS FOUND ON THE L/H TRANSMISSION DECK BESIDE THE 7° BULKHEAD BRACE STRUT MOUNT. THIS DAMAGE MEASURED 0.5” IN WIDTH, 0.5” IN LENGTH, AND 0.048” IN DEPTH. AN APPROXIMATE LOCATION OF THE DAMAGE IS AT F.S 3640.26MM, W.L -1776.64MM, AND L.B.L -718MMSDR 2A6R1024202574601Rail · chafedCHAFING DAMAGE WAS FOUND ON THE TAIL BOOM L/H TRDS SUPPORT RAIL/STIFFENER SHEET (P/N: 350A231028.66) JUST FORWARD OF THE #3 TRDS BEARING SUPPORT. THIS DAMAGE IS A 0.25” IN LENGTH AND 0.1” IN HEIGHT SECTION THAT IS CHAFED THROUGH THE FULL THICKNESS OF THE RAIL.SDR 2022F00466Probe · malfunctionedFUEL QUANTITY PROBE INDICATOR UPGRADE - 00-2800-EO-3766 STC SR02492AK INSTALLED 05/26/2022 - MONTH AFTER INSTALLATION, 06/14/2022 BEGAN GETTING ERRATIC FUEL LEVEL READINGS. READING HIGH, UP/DOWN, MAXED OUT OR READING 0. REPLACED QUANTITY COMPUTER, REPLACED FUSDR QMLA2019121119097Duct · odorPILOT REPORTED: ELECTRICAL/SMELL FROM HEATING/DEMISTER SYSTEM.
UPON ARRIVAL AND BRIEFING FROM PILOT OF PROBLEM, HE COULD NOT EXACTLY DETERMINE THE TYPE OF SMELL. JUST ELECTRICAL CAME TO MIND, BUT THE SMELL WASN’T EXACTLY THAT. I HAD REMEMBERED SEEING A DISSDR QMLA2019043019044Evaporator · malfunctionedCREW SMELLED BURNING ELECTRICAL SMELL IN COCKPIT. TURNED OFF AC AND OTHER UNNECESSARY CONSUMERS. SMELL SOMEWHAT DISSIPATED AND WE MADE A PRECAUTIONARY LANDING AT OUR COMPANY OTHER BASE AS WAS CLOSEST AND BEST OPTION. LANDED SAFELY. UPON POST FLIGHT, FOUND THATSDR QMLA201806011868Unknown · odorTOOK OFF , AFTER APPROXIMATELY 5 MINUTES IN FLIGHT, THE CREW STARTED TO DETECT AN ODOR OF ELECTRICAL BURNING IN THE CABIN. THE PILOT TURNED OFF THE AIR CONDITIONER AND STARTING TO HEAD BACK TO BASE IMMEDIATELY. ALL ELECTRICAL SYSTEMS WERE WITH IN NORMAL LISDR 2A6R201805174791Gusset · crackedFUEL TANK CRADLE REAR CRADLE HAS A CRACK IN THE GUSSETSDR QMLA2018051018056Blower Motor · odorTAKING OFF FROM BASE TO PR EVENT, THE MED CREW BEGAN TO SMELL ELECTRICAL TYPE BURNING SMELL WITH THE CABIN. THE SMELL WAS STRONG FROM THE PILOT SEAT SO I COULD ONLY ASSUME THAT IT WAS POSSIBLY SOMETHING FROM THE COCKPIT AREA. STARTED TO ISOLATE THE PROBLEM BY SDR QMLA2014051414053Bulkhead · crackedDURING AMC EC130 B4 AAIP A0560 100HR 12 MONTH INSPECTION ITEM 5.1 CHECK, PICK UP OF WEB OF CANOPY FOUND AN 80 MM CRACK AT THE JUNCTION.SDR QMLA2013091213131Mount · crackedDURING SCHEDULED INSPECTION OF HORIZONTAL STABILIZER MOUNTS, FOUND RT LOWER MOUNT CRACKED, ACROSS ROW OF BOLT HOLES. ACFT OUT OF SERVICE.
STCs that may be installed · 134
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 134 STCs