- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 7371
- Year built
- 2012
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- September 25, 2012
- Certificate issued
- November 4, 2022
- Expires
- November 30, 2029
- Mode S code
- A095EE
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 N137HNMatched 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 N137HNMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2024042520043Potentiometer · wornTOOK OFF FROM BASE GOT TO LEVEL FLIGHT STARTED POWER CHECK GOT THE SOLID AMBER GOV LIGHT. RETURNED TO BASE.SDR 2A6D2020042201101Structure · gougedCHAFING DAMAGE WAS DISCOVERED ON THE TRANSMISSION DECK. THE DAMAGE IS APPROXIMATELY 0.028” DEEP AND 0.35” WIDE BY 0.52”SDR QMLA2019052019048Frame · crackedWHILE WORKING AAIP A 1660.25.1 A CRACK AROUND 68MM LONG WAS FOUND I THE RT PICKUP WEB OF CANOPY FRAME UNDER THE FLOOR. REMOVED PAINT AND PRIMER TO CONFIRM THE CRACK. FOUND THAT IT WAS INDEED CRACKED. DOCUMENTED THE CRACK AND REPORTED IT TO AMC SERVICE ENGINEERSDR QMLA2019012319011Gas Generator · abnormalPILOT REPORTED LOSS OF FLI INDICATION ON APPROACH TO THE BASE. AFTER LANDING AND ROLLING THE THROTTLE TO IDLE, A FLASHING AMBER GOV LIGHT WAS ILLUMINATED. UPON INSPECTION OF THE T4 HARNESS , I FOUND THE T4 HARNESS WAS DAMAGED. AFTER GETTING A VIDEO SCOPE TOSDR QMLA2016071016073Bearing · corrodedWHILE TAKING OFF, THE RIGHT PEDAL BECAME INCREASINGLY HARDER TO MOVE AS POWER WAS APPLIED. AFTER LIFTING, ABORTED TAKEOFF. EXECUTED A NORMAL LEFT AND RIGHT PEDAL TURN, MEDIC STATED HE SMELLED SMOKE. RIGHT PEDAL FELT LIKE IT WAS BINDING WHEN APPLIED DURING PSDR QMLA2014092414114Stabilizer · crackedWHILE PERFORMING AN AIRWORTHINESS CHECK, A CRACK WAS FOUND ON THE UPPER SURFACE OF THE HORIZONTAL STABILIZER ON THE LT SIDE. THE CRACK BEGAN IN THE RIVET LINE OF THE METAL LAP ATTACHMENT POINT ALONG THE TAIL BOOM AT APPROX 3 INCHES FROM THE TE & CURVED FORWARSDR QMLA2014061914075Valve · faultyDEPARTED BASE FOR A SCENE FLIGHT AT 16:06. LANDED ON SCENE AT 16:35. AFTER AN EXTENDED RUN TIME ON THE GND SHUT DOWN THE ENG TO SAVE MY FUEL FOR THE MISSION. AFTER LOADING THE PATIENT IN THE ACFT THE ENG FAILED TO RESTART. IT REACHED 210 RPM & ACTED AS IF SDR QMLA2014013014012Engine · making metalTHE PILOT & MEDICAL CREW WERE ON THEIR WAY TO A SCENE LOCATION TO PICK UP A PATIENT WHEN APPROXIMATELY 4 MILES FROM THEIR DESTINATION, THE ENG CHIP LIGHT ILLUMINATED. THE PILOT NOTIFIED THE CREW THAT THEY WOULD NOT BE ABLE TO CONTINUE & PROCEEDED TO FIND A SUSDR QMLA2013111413166Drive Assy · seizedAT CRUISE ALTITUDE 2500 FT MSL, COCKPIT BEGAN TO FILL WITH SMOKE. HYD AND SERVO LIGHTS ON CAUTION PANEL ILLUMINATED. REDUCED AIRSPEED AND MADE EMERGENCY LANDING. AFTER LANDING AND ENGINE SHUTDOWN THE PRIMARY HYD BELT WAS FOUND BROKE AND MISSING. NO OTHER A
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