- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 7029
- Year built
- 2010
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- November 15, 2010
- Certificate issued
- June 20, 2016
- Expires
- June 30, 2029
- Mode S code
- A462C4
Eurocopter EC 130 B4TCDS H9EUAirframe · Eurocopter 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 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.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N382AMMatched 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 EC 130 B4 aircraft
FAA incident reports
No FAA accident or incident reports matched to N382AMMatched 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 EC 130 B4 aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2025160673201Channel · crackedA CRACK WAS DISCOVERED ON THE TOP FLANGE OF THE RH EDGE FRAME "Z" CHANNEL JUST AFT OF THE STA 845 FRAME. THE CRACK IS APPROXIMATELY 0.75" LONG.SDR QMLA2025032420040Motor · shortedELECTRICAL SMOKE ODOR IN CABIN. AFT EVAPORATOR MOTOR HAD INTERNAL SHORT CAUSING SMOKE SMELL AND CAUSING AFT PORTION OF A/C TO BE INOP.SDR QMLA2024042920044Attach Fitting · damagedN382AM 7029 WENT OOS FOR SCHEDULED HEAVY MAINTENANCE, WHILE REMOVING THE HORIZONTAL STABILIZER TO FOM, IT WAS NOTED THAT THE RH ATTACHMENT BOLT WAS VERY HARD TO REMOVE. UPON FURTHER INSPECTION, FOUND THE HORIZONTAL RH UPPER ATTACHMENT FITTING TO BE CRACKED.SDR QMLA2022050920027Nozzle · faultyUPON DEPARTURE FROM THE AIRFIELD AT 0133, AT 500' AGL, 70 KIAS, AND 8.5 FLI WITH THE DEMIST ON, SMOKE BEGAN FILLING THE COCKPIT ORIGINATING FROM THE DEMIST NOZZLES. CREW OPENED THE SLIDING WINDOWS TO VENT THE COCKPIT, DEMIST WAS SHUT OFF, AND THE AIRCRAFT WAS SDR 2019F00075Rail · corrodedDURING PAINT STRIPPING, MAJOR CORROSION WAS FOUND ON THE RT CABIN THRESHOLD RAIL FROM FS 1436.0 MM TO FS 2230.0 MM.SDR QMLA2017042317043Windscreen · debondedWHILE ON A FLIGHT, STARTED EXPERIENCING INCREASE LIGHT NOISE IN THE FRONT AND RIGHT PORTION OF THE CABIN TO THE POINT WHERE IT STARTED TO LIMIT OUR NVGS CAPABILITIES. MENTIONED TO THE CREW THERE WAS A LIGHT FLICKERING TOWARDS THE FRONT OF THE CABIN AND IF ANYSDR QMLA2016122016146Windshield · crackedAFTER DEPARTURE, CREW NOTICED A TEN INCHES CRACK IN THE RIGHT WINDOW. THIS CRACK WAS NOT NOTICED DURING PREFLIGHT. FLIGHT WAS IMMEDIATELY TERMINATED AND RETURNED TO BASE. FURTHER INSPECTION BY PILOT REVEALED NO OBVIOUS DAMAGE RESULTING IN THE CRACK NOR INDICATSDR QMLA2016100816115Antenna · shortedPILOTE SMELLED AN ELECTRICAL BURNING ODOR IN THE COCKPIT. NO VISABLE SMOKE. THE ODOR SEEMED TO ORIGINATE WHEN TRANSMITTING ON THE MEDICAL RADIO INSTALLED IN THE AIRCRAFT. MECHANIC STATED THERE WAS NO EVIDENCE OF A BURNING ODOR IN THE COCKPIT. MECHANIC TRANSMSDR QMLA2015072715063Webbing · crackedWHILE DIAGNOSING WIRING ISSUE, LEFT FRONT BELLY PANEL WAS REMOVED & A CANOPY WEB CRACK WAS DISCOVERED.SDR QMLA2014011714006Structure · crackedDURING A0560 100 HR 12 MONTH AIRFRAME INSPECTION, TWO CRACKS WERE DISCOVERED. ONE ON LT SIDE OF ACFT BETWEEN SLIDING DOOR & BAGGAGE DOOR, EXTENDING 115MM DOWN THE SIDE OF THE AIRCRAFT & UPWARD TO FRONT OF THE DOOR TRACK. THE OTHER CRACK IS ON THE RT SIDE OF SDR QMLA2013122113176Attach Fitting · crackedDURING AAIP A1040 300 HOUR, 12 MONTH INSPECTION, STEP A1040 2.4, A CRACK WAS FOUND IN THE LT UPPER STABILIZER MOUNT DURING THE VISUAL INSPECTION. THE CRACK RAN FROM THE FWD EDGE OF THE MOUNT THROUGH THE FWD OTBD BOLT HOLE & TO THE MIDLINE OF THE MOUNT.SDR QMLA2013091913135Skin · crackedDURING A 100 HOUR INSPECTION, A CRACK WAS FOUND IN THE SKIN ADJACENT OF THE RT CANOPY WEB. THE SKIN CRACK HAS APPROXIMATELY 30MM VISIBLE LENGTH PARALLEL TO INBD EDGE OF THE RT CANOPY WEB. IT TURNS OTBD ALONG THE TOP RADIUS OF THE CANOPY WEB. IT IS POSSIBLE THSDR QMLA2013080613111Carrier Assy · crackedDURING A ROUTINE AIRWORTHINESS CHECK, MECHANIC PERFORMED A VISUAL INSPECTION OF THE ACFT. ON INSPECTING THE HORIZONTAL STABILIZER AREA, A CRACK WAS NOTICED ON THE RT LOWER CARRIER ATTACH FITTING. REPLACED CRACKED CARRIER.
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