- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 4644
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 19, 2009
- Certificate issued
- August 10, 2016
- Expires
- August 31, 2029
- Mode S code
- A3F798
American Eurocopter AS350B3TCDS H9EUAirframe · American Eurocopter AS350B3TCDS E00054ENEngine · Turbomeca ARRIEL-2B1
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 98
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1985 | 1 |
|---|---|
| 1990 | 2 |
| 1999 | 1 |
| 2000 | 3 |
| 2001 | 2 |
| 2002 | 6 |
| 2003 | 8 |
| 2004 | 3 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 6 |
| 2008 | 1 |
| 2009 | 2 |
| 2010 | 9 |
| 2011 | 4 |
| 2012 | 5 |
| 2013 | 11 |
| 2014 | 7 |
| 2015 | 4 |
| 2016 | 2 |
| 2017 | 5 |
| 2018 | 6 |
| 2019 | 3 |
| 2020 | 5 |
| 2021 | 16 |
| 2022 | 7 |
| 2023 | 2 |
| 2024 | 1 |
| 2025 | 4 |
| 2026 | 10 |
Airframe · American Eurocopter AS350B3
AD 2026-20-03Placards and MarkingsAD 2026-16-01Main rotor driveAD 2026-14-02Indication/Recording SystemInformation bulletins that may apply · 9
Advisory, not mandatory.
Airframe · American Eurocopter AS350B3
SAIB AIR-21-13Engine Emergency Shutdown SystemSAIB SW-17-23R2Fuel SystemSAIB SW-15-20Air Conditioning System WiringSAIB SW-15-04Cabin Ventilation Air Scoop DrainingSAIB SW-12-45Garmin Model 400W/500W Series GPS-WAAS Navigation SystemSAIB SW-11-07Star Flex Arm Failures on Eurocopter France Model AS350, AS355, and EC130 HelicoptersSAIB SW-07-22R1Serrated lock washersSAIB SW-07-13Oxygen Reserve CylinderSAIB SW-06-48 corrected 07/20/2006Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N355CFMatched 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 American Eurocopter AS350B3 aircraft
FAA incident reports
No FAA accident or incident reports matched to N355CFMatched 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 American Eurocopter AS350B3 aircraft
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2025022620028Unknown · vibrationVIBRATION IN SEAT AND PEDALSSDR 2022FA0000205Bulkhead Web · chafedDAMAGE TO THE AFT BULKHEAD WEB (PN: 350A21-1036.60) WAS NOTED IN THE FORM OF NUMEROUS CHAFES. THE CHAFES WERE MEASURED TO BE ON AVERAGE 0.50" IN LENGTH WITH THE DEEPEST CHAFE BEING 0.008" DEEP.SDR 2022FA0000204Tail Boom · dentedDAMAGE TO THE TAIL BOOM AFT SKIN PANEL (PN: 350A23-0020.22). THE CREASE AND GOUGE DAMAGES WERE DISCOVERED TO BE JUST FORWARD OF THE TAIL ROTOR GEAR BOX. THE CREASE DAMAGE IS APPROXIMATELY 0.40" WIDE AND THE GOUGE DAMAGE IS APPROXIMATELY 0.10" IN LENGTH, 0.05" SDR 2A6D20220315002None · usedCUSTOMER HAS REPORTED DAMAGE TO THE TAIL BOOM AFT SKIN PANEL (PN: 350A23-0020.22). THE CREASE AND GOUGE
DAMAGES WERE DISCOVERED TO BE JUST FORWARD OF THE TAIL ROTOR GEAR BOX. THE CREASE DAMAGE IS APPROXIMATELY 0.40”
WIDE AND THE GOUGE DAMAGE IS APPROXIMATELYSDR 2A6D20220315001None · usedCUSTOMER HAS REPORTED DAMAGE TO THE AFT BULKHEAD WEB (PN: 350A21-1036.60) IN THE FORM OF NUMEROUS
CHAFES. THE CHAFES WERE MEASURED TO BE ON AVERAGE 0.50” IN LENGTH WITH THE DEEPEST CHAFE
BEING 0.008” DEEP.SDR 2A6D620220309001Bulkhead · usedDAMAGE TO THE 15° BULKHEAD LH POST (PN: 350A21-1031.33) WAS NOTED IN THE FORM OF CHAFING. THE CHAFING DAMAGE IS APPROXIMATELY 0.40” IN LENGTH, 0.07” IN WIDTH AND 0.017” IN DEPTH.SDR 2A6D2020082872604Support · chafedCHAFING ON THE TRANSMISSION DECK SUPPORT (350A21-1041-143) THAT IS .5” BY .2” AND .013” AT ITS DEEPEST POINTSDR 2A6D2020082702603Frame · chafedCHAFING ON THE LT X-FRAMES AFT UPPER AND LOWER LEGS. THE AFT UPPER LEG DAMAGE IS .24” BY .22” AND IS .024” AT ITS DEEPEST POINT LOCATED AT STA 3650, WL 1979, AND BL 430L. THE AFT LOWER LEG DAMAGE IS .74” BY .19” AND MEASURES .002” LOCATED AT STA 3650, WL 2305,SDR 2A6D2020082402602Floor Panel · corrodedCORROSION WAS DISCOVERED ON THE RT HAND SIDE CABIN FLOOR EDGE SECTION AIRBUS PN 350A21-1359 RANGING FROM STA 1000 TO 1550.SDR 2A6D2020082002601Skin · chafedCHAFING ON THE RT INTERIOR SIDE OF THE TAILBOOM SKIN LOCATED AT APPROXIMATELY STA 7898, WL 2089, AND BL 90R JUST FORWARD OF THE HORIZONTAL STABILIZER OPENING. THE CHAFE IS .95” BY .12” AND IS .007” AT ITS DEEPEST POINT.SDR 2A6R201807110001Frame · chafedCHAFING FOUND ON LF X FRAME. BLENDED OUT DAMAGE IAW RDAS-AHI 350-53-030-18.
STCs that may be installed · 401
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 401 STCs