- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0781
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- April 29, 2009
- Certificate issued
- June 18, 2019
- Expires
- June 30, 2029
- Mode S code
- AB2BCB
Eurocopter Deutschland EC 135 P2+TCDS H88EUAirframe · Eurocopter Deutschland EC 135 P2+TCDS E42NEEngine · Pratt & Whitney Canada PW206B2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 50
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2000 | 1 |
|---|---|
| 2008 | 2 |
| 2009 | 2 |
| 2012 | 4 |
| 2013 | 7 |
| 2014 | 6 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 11 |
| 2022 | 7 |
| 2024 | 4 |
| 2025 | 3 |
| 2026 | 5 |
Airframe · Eurocopter Deutschland EC 135 P2+
AD 2026-20-06Main rotor gearboxAD 2026-17-05Cabin Equipment/FurnishingsAD 2026-08-10Passenger compartment equipmentInformation bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N819LFMatched 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 Deutschland EC 135 P2+ aircraft
FAA incident reports
No FAA accident or incident reports matched to N819LFMatched 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 Deutschland EC 135 P2+ 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 2A6R2026061575901Floor Panel · damagedDAMAGE WAS FOUND ON THE COCKPIT FLOOR PANEL IN THE FORM OF IMPACT DAMAGE AND CORROSION. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2026-24444A DATED 16 JUL 2026, AIR MSDR QMLA2026032720024Warning Message · illuminatedTRANSMISSION CHIP CAUTION ILLUMINATED MULTIPLE TIMES WHILE IN CRUISE FLIGHT. CAUTION REMAINED ON FOR LAST 3 MINUTES OF FLIGHT.SDR QMLA2026021320012Unknown · odorAFTER SHUTTING DOWN, CREW INDICATED A BURNING ODOR COMING FROM THE AFT NR 2 ENGINE AREA. CREW DESCRIBED THE ODOR AS ACRID AND ELECTRICAL IN NATURE. PILOT NOTED UNBURNT JET FUEL ODOR BUT COULD NOT IDENTIFY AN ELECTRICAL ODOR OR SEE
ANY EVIDENCE OF FIRE OR BURNSDR QMLA2025022320025Unknown · odorCREW REPORTED ABNORMAL SMELL IN THE REAR CABIN DURING OPERATING OF THE BLEED HEATING. TURNED THE HEATING OFF AND CONTINUED ON RTB LEG. LANDED WITHOUT INCIDENT, CALLED MAINTENANCE TO INVESTIGATE.SDR QMLA202305060031Unknown · unknownCORRECTION TO PREVIOUS SUBMISSION. THIS WAS INCORRECTLY SUBMITTED UNDER CONTROL NUMBER QMLA202305050031. (THIS CONTROL # WAS PREVIOUSLY USED) NEW SDR SUBMITTED AS QMLA2023050520036 N819LF 0781SDR QMLA2023050520036Warning Unit · unserviceableINFLIGHT ON AN AIR AMBULANCE FLIGHT. RECEIVED A #2 FUEL VALVE CL CAUTION FOLLOWED BY #2 FUEL PRESSURE AND THEN AND ENGINE FAIL LIGHT. I MADE AN EMERGENCY LANDING AT THE NEAREST AIRPORT. AFTER LANDING AND COMPLETE SHUTDOWN FOR TEN MINUTES. THIS WAS INCORRECTLY SDR QMLA2023050520031Warning Unit · unserviceableINFLIGHT ON AN AIR AMBULANCE FLIGHT. RECEIVED A #2 FUEL VALVE CL CAUTION FOLLOWED BY #2 FUEL PRESSURE AND THEN AND ENGINE FAIL LIGHT. I MADE AN EMERGENCY LANDING AT THE NEAREST AIRPORT. AFTER LANDING AND COMPLETE SHUTDOWN FOR TEN MINUTES. SDR SUBMITTED LATSDR QMLA2022082920058None · damagedCOMPLETION OF 23-5300-EO-3820 PART 1. REPAIRED FRAME 5 IAW REFERENCED EA BY INSTALLING DOUBLERS AS DIRECTED.
ISSUED 337 FOR REPAIR. EO CONTAINS FIGURES OF REPAIRS. MORE DETAILS FOUND ON UNIFLIGHT AVIATION WORK ORDER. AIRCRAFT OOS AT HEAVY MAINTENANCE EVENT SDR QMLA2020062220028Wire · unsecureAC EQUIPPED WITH AN FDC IBF SYSTEM, WHICH INVOLVES AN ADDITIONAL COWLING ACROSS THE FORWARD PART OF THE TRANSMISSION DECK. THIS COWLING INCLUDES, ON EACH SIDE, TWO PIECES OF HARD PLASTIC DUCTING CONNECTED BY A PIECE OF FLEXIBLE ORANGE DUCTING WITH A METAL WIR
STCs that may be installed · 74
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.