- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 4114
- Year built
- 2006
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- September 19, 2006
- Certificate issued
- September 9, 2014
- Expires
- September 30, 2027
- Mode S code
- A0CEED
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 N151LNMatched 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 N151LNMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2026101275802Frame · corrodedDAMAGE TO THE LT EDGE FRAME, IN THE FORM OF CORROSION, WAS IDENTIFIED ON THE OTBD FACES OF THE FRAME.SDR 2A6R2026101275801Frame · corrodedDAMAGE TO THE RT EDGE FRAME IN THE FORM OF CORROSION, WAS IDENTIFIED ON THE OUTBOARD FACES OF THE FRAME.SDR 2A6R2026310875801Doubler · corrodedCORROSION DAMAGE WAS DISCOVERED ON THE FORWARD FUEL TANK SADDLE DOUBLER. REPLACEMENT PART WAS UNAVAILABLE WITHIN THE REQUIRED RETURN-TO-SERVICE SCHEDULE. A REPLACEMENT FORWARD FUEL TANK SADDLE DOUBLER, WAS FABRICATED LOCALLY USING THE DISCREPANT PART AS A GUISDR QMLA2024101720134Unknown · smokeCRUISE STAGE OF FLIGHT, HEAT AND WINDOW DEFROST ON, SMOKE IN CABIN, INSPECTED AIRCRAFT, RTS'D THIS AIRCRAFT HAS BEEN RETURNED TO REVENUE SERVICE, REF # MEC-001100.SDR QMLA2012071012112Fairing · crackedANTI-VIBRATING DOME FAIRING FOUND CRACKED AT 2 OTBD ATTACHMENT SCREWS.SDR QMLA2012060812094Skin · crackedFOUND CRACK IN HORIZONTAL STABILIZER ON THE RT UPPER SKIN - CRACK LOCATION FROM RT OTBD EDGE 43.1250 TO 46" - FROM AFT EDGE 3,5" TO 5.5" AND 10.1250" AFT OF RT ATTACH POINT. CRACK IS APPROX 3.5" IN LENGTH AT AN ANGLE STARTING FROM 3.5" FROM AFT EDGE TO 5.5" PSDR QMLA2012011212004Module · defectiveDURING ROUTINE ENGINE INSPECTION OF THE MAGNETIC CHIP DETECTORS, THE OIL CHECK VALVE FOR THE MAGENETIC CHIP DETECTOR FOR THE M05 MODULE WOULD NOT CLOSE. REMOVED THE HSG ASSY AND FOUND A METAL TAB STUCK TO THE CHIP DETECTOR. THIS ACFT IS CURRENTLY OUT OF SERVSDR QMLA2011042011049Unknown · odorSHORTLY AFTER TAKEOFF, RETURNED TO THE BASE, THE MEDIC ANNOUNCED HE SMELLED A STRONG PRESENCE OF FUEL. THE NURSE CONFIRMED THE ODOR AS WELL. THE PILOT IMMEDIATELY BEGAN A COURSE TO THE NEAREST AIRPORT WHERE ON FINAL APPROACH, THE ODOR HAD DISAPPEARED. AFTER
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