- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 7015
- Year built
- 2010
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- October 21, 2010
- Certificate issued
- October 4, 2021
- Expires
- October 31, 2028
- Mode S code
- AB0A5C
Eurocopter AS 350 B3TCDS H9EUAirframe · Eurocopter AS 350 B3TCDS E00054ENEngine · Turbomeca ARRIEL-2B1
From the FAA registry file of October 24, 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 · Eurocopter AS 350 B3
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 · Eurocopter AS 350 B3
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 N810LFMatched 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 AS 350 B3 aircraft
FAA incident reports
No FAA accident or incident reports matched to N810LFMatched 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 AS 350 B3 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 QMLA2026070520043Outlet · odorFLIGHT CREW REPORTED SMOKE ODOR IN CABIN DURING FLIGHT.SDR 2023FA0000124Unknown · unknownON A FLIGHT FROM SILVER CITY, NM TO MEMORIAL MEDICAL CENTER IN LAS CRUCES. I GOT A YELLOW AND RED GOV LIGHT. I WAS ABOUT 5 MINS FROM KSVC, SO I TURNED AND LANDED AT GRANT COUNTY AIRPORT. AIRCOM WAS ALERTED, AND THEY GOT NATIVE 30 HEADED OVER TO PICK UP OUR PATSDR 2023F00079Unknown · unknownABOUT 30 MINUTES AFTER TAKEOFF FROM GILA REGIONAL WITH A INTERFACILITY TRANSFER THE COCKPIT STARTED TO SMELL STRONGLY LIKE BURNING PLASTIC/RUBBER. NO SMOKE WAS PRESENT AND INSTRUMENTS AND WARNING LIGHT PANEL WAS NORMAL WITH NO INDICATIONS OF A PROBLEM BESIDES SDR 2A6D20220127001Floor Support · corrodedCORROSION WAS NOTED ON THE LH AND RH SIDE OF THE CABIN FLOOR EDGE. THE DAMAGE WAS REPAIRED VIA BLENDING AND TRIMMING OUT THE DAMAGED PORTION(S) OF THE EDGE FRAME, ALONG WITH FABRICATING AND INSTALLING SPLICE DOUBLER(S) AT LH STA 75.19 AND RH STA 73.19 TO REINFSDR 2A6D20220120005None · chafedAC 7015 HAS CHAFE DAMAGE TO THE L/H X-FRAME’S AFT LOWER LEG LOCATED AT APPROXIMATELY STA 3650, WL 2305, AND BL 430L. THE DAMAGE MEASURES .21” LONG AND .2” WIDE WITH A MAX DEPTH OF .019”.SDR 2A6D20220120004None · chafedTHE TRANSMISSION SUPPORT FRAME (PN 350A21-1041-143) HAS CHAFING DAMAGE ON THE LOWER FLANGE FROM AN UNSECURED CABLE. THE DAMAGE IS UNDER THE TRANSMISSION DECK AT THE AFT RH CORNER OF THE TRANSMISSION CUTOUT. THE CHAFING ON THE TRANSMISSION DECK FRAME WITH A LENSDR 2A6D20220120003Bulkhead · gougedTHE L/H LATERAL BAGGAGE COMPARTMENT WE IDENTIFIED THE LANDING GEAR’S L/H VIBRATION DAMPENER FITTING WAS GOUGED. DAMAGE LOCATED AT APROX. STA 2700, WL 2550, BL 600L. THE DAMAGE MEASURES L=0.600”, W=0.300”, D=0.025”.SDR 2A6D20220120002Bulkhead · chafedDAMAGE TO THE 15 DEGREE BULKHEAD LH WEB (PN: 350A21-1032.60 IN THE FORM OF CHAFES. THE FIRST CHAFE DAMAGE AREA WAS FOUND NEAR THE X-FRAME AND WAS MEASURED TO BE APPROXIMATELY 0.40” X 0.39” AND 0.015” DEEP; THE SECOND CHAFE DAMAGE AREA WAS FOUND ON THE STIFFENISDR 2A6D20220120001Bulkhead · chafedAIRCRAFT HAS CHAFE DAMAGE ON THE AFT SIDE OF THE 15 DEGREE BULKHEAD LOCATED IN THE L/H LATERAL BAGGAGE COMPARTMENT IN TWO DIFFERENT LOCATIONS. THE DAMAGE IS LOCATED AT APPROXIMATELY STA 2700, WL 2300, AND BL 500L. THE OB DAMAGE MEASURES.2” LONG AND .11” WIDE WSDR 2022FA0000022Skin Panel · chafedDAMAGE TO THE ENGINE DECK (PN: 350A21-1239.20) IN THE FORM OF CHAFES NEAR THE
SCUPPER DRAIN. THE DAMAGE AT THE SCUPPER DRAIN WAS MEASURED TO BE 3.90” X 7.40” AND 0.014” DEEPSDR QMLA2019121019095Floorbeam · gougedGOUGING FOUND ON RIB UNDERNEATH CABIN FLOOR AT THE RIB BEHIND THE CO PILOTS COLLECTIVE. GOUGING WAS THROUGH THE COMPLETE THICKNESS OF THE RIB. THE DAMAGE WAS APPROXIMATELY 13/32" IN LENGTH AND LOCATED AT THE BEND RADIUS OF THE RIB. ** THIS AIRCRAFT REMAINS OOS
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