- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 4960
- Year built
- 2010
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- December 12, 2014
- Certificate issued
- August 23, 2016
- Expires
- August 31, 2029
- Mode S code
- A1B472
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 N209LFMatched 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 N209LFMatched 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 · 16
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6D20220504004Bulkhead · damagedSHORT ED AND SHORT PD HOLES WERE DISCOVERED ON THE 7 DEGREE BULKHEAD ADJACENT TO THE RECESSED MEDICAL WALL INSTALLATION.SDR 2A6D20220503003Xmsn Deck · chafedR/H SIDE FWD. TRANSMISSION DECK WEB (P/N: 350A21-4418) IS DAMAGED IN THE FORM OF A CHAFING. THE DAMAGE IN THE FWD IS APPROXIMATELY 0.3” IN LENGTH, 0.3” IN WIDTH AND 0.019” IN DEPTH AND DAMAGE AT AFT IS APPROXIMATELY 0.3” IN LENGTH, 0.25” IN WIDTH AND 0.010” INSDR 2A6D20220429002Xmsn Deck · chafedCHAFING DAMAGE WAS DISCOVERED ON THE RH SIDE OF THE TRANSMISSION DECK. THE DEEPEST DEPTH IS 0.015" WITH A LENGTH OF 2.1" AND WIDTH OF 0.1.
See all 16 reportsSTCs 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