N819LFEurocopter Deutschland Gmbh EC 135 P2+
Safety record in brief:No NTSB accidents or incidents since 198216 ADs may apply9 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Air Methods LLC
- Owner type
- LLC
- City, state
- Greenwood Village, CO
- Certificate issued
- Jun 18, 2019
- Expires
- Jun 30, 2029
- Airworthiness
- Standard · Normal
- Airworthiness date
- Apr 29, 2009
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Eurocopter Deutschland Gmbh
- Model
- EC 135 P2+
- Serial number
- 0781
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 7
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Type certificate data sheet
- H88EU
- Mode S code
- AB2BCB
Engine
- Make and model
- P&W Canada Pw206b2
- Type
- Turbo-shaft
- Power
- 447 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2019 – nowAir Methods LLCGreenwood Village, CO · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (16)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2014-05-06 R1 | Airbus Helicopters Deutschland GmbH Helicopters (Type Certificate Previously Held by… | Jan 22, 2019 | Airframe (EC 135 P2+)Certain serial numbers: EC135 P1 0005–00829; EC135 P2 0005–00829; EC135 P2+ 0005–00829; EC135 T1 0005–00829; EC135 T2 0005–00829; EC135 T2+ 0005–00829; …. Only with: EC135: tail rotor control lever P/N L672M2802205 or L672M1012212, cyclic control lever P/N L671M1005250, collective control lever assembly P/N L671M2020108, or collective control plate P/N L671M5040207 installed; MBB-BK 117C-2: tail rotor control lever assembly P/N B672M1007101 or B672M1807101, tail rotor control lever P/N B672M1002202 or L672M2802205, or lateral control lever assembly P/N B670M1008101 installed. |
| 2018-07-01 | Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter… | May 3, 2018 | Airframe (EC 135 P2+)Serial numbers per Table 1 of Airbus Helicopters Alert Service Bulletin EC135-63A-017, Revision 2, dated December 5, 2016. Only with: Main transmission FS108 housing upper part P/N 4649 301 034, 4649 301 067, or 4649 301 088 installed, with a serial number listed in Table 1 of ASB EC135-63A-017. |
| 2017-03-01 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) Helicopters | Mar 31, 2017 | Airframe (EC 135 P2+)Certain serial numbers: EC135 0005–00829; MBB-BK 117 C-2 9004–9310. Only with: EC135: with tail rotor control lever P/N L672M2802205 or L672M1012212, cyclic control lever P/N L671M1005250, collective control lever assembly P/N L671M2020108, or collective control plate P/N L671M5040207 installed; MBB-BK 117 C-2: with tail rotor control lever assembly P/N B672M1007101 or B672M1807101, tail rotor control lever P/N B672M1002202 or L672M2802205, or lateral control lever assembly P/N B670M1008101 installed. |
| 2016-11-21 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus… | Jul 11, 2016 | Airframe (EC 135 P2+) |
| 2015-12-09 R1 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GmbH) (Airbus… | Feb 25, 2016 | Airframe (EC 135 P2+) |
Show all 16 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2014-16-24 | Airbus Helicopters Deutschland GmbH (Previously Eurocopter Deutschland GbmH) (Airbus… | Sep 25, 2014 | Airframe (EC 135 P2+)Only with: Main rotor hub shaft P/N L623M1006101, L623M1206101, L623M1006102, L623M1206102, L623M1006103, or L623M1206103 installed. |
| 2014-13-09 | Airbus Helicopters Deutschland GmbH (Type Certificate Previously Held by Eurocopter… | Jul 30, 2014 | Airframe (EC 135 P2+)Only with: Mounting ring frame X9227 P/N L535H2120301, L535H2120303, or L535H2120304 installed, except those with frame reinforcement P/N L535H2100201 installed. |
| 2014-05-01 | Eurocopter Deutschland GmbH Helicopters | Apr 14, 2014 | Airframe (EC 135 P2+)Only with: Main gearbox (MGB) P/N 4649 010 003, 4649 010 005, 4649 010 006, 4649 010 006X, 4649 010 008, 4649 010 008X, 4649 001 007, 4649 010 010, or 4649 010 013 installed. |
| 2014-01-02 | Eurocopter Deutschland GmbH Helicopters | Mar 3, 2014 | Airframe (EC 135 P2+)Certain serial numbers: 870; 872; 873; 879; 883; 884; …. Only with: Mechanical air conditioning system compressor bearing block upper bearing P/N L210M1872105 installed. |
| 2013-21-06 | Eurocopter Deutschland GmbH Helicopters | Jan 31, 2014 | Airframe (EC 135 P2+)Only with: Goodrich external mounted hoist with boom support assembly P/N 44301-500, 44307-500, or 44307-500-1 installed (EC135); boom P/N 44307-500 installed (MBB-BK 117 C-2). |
| 2013-21-05 | Eurocopter Deutschland GmbH Helicopters | Dec 5, 2013 | Airframe (EC 135 P2+)Only with: With bearing P/N LN9367GE6N2, rod P/N L671M5040205, lever P/N L671M5040101, and floor P/N L533M1014101 through L533M1014106 installed. |
| 2013-18-05 | Eurocopter Deutschland GmbH Helicopters | Oct 18, 2013 | Airframe (EC 135 P2+)Only with: Fire extinguishing system P/N L262M1808101, L262M1812101, or L262M1812102 installed. |
| 2013-11-15 | Eurocopter Deutschland GmbH Helicopters | Jul 26, 2013 | Airframe (EC 135 P2+)Certain serial numbers: EC135 P1 0005–0699; EC135 P2 0005–0699; EC135 P2+ 0005–0699; EC135 T1 0005–0699; EC135 T2 0005–0699; EC135 T2+ 0005–0699; …. Only with: BO-105A/C/S/LS A-1 with cantilever assembly P/N 105-40132 or 105-40139; BO 105 LS A-3 with cantilever assembly P/N 105-40139; EC135 (excluding S/Ns 0076, 0093, 0098, 0099, 0102, 0104, 0106, 0108, 0110, 0111, 0113, 0114, 0116, 0117, 0119) with cyclic stick locking device P/N L670M1045101/-102/-104/-105/-106/-107 and pin P/N L311M1038205 or L311M1099205; MBB-BK117 A-1 through C-1 with cyclic stick holder assembly P/N 117-41140-01, 117-41230-01 or 117-41230-03; MBB-BK117 C-2 with cyclic stick locking device P/N B856M1011101 and pin P/N L311M1038205 or L311M1099205 installed. |
| 2013-03-21 | Pratt & Whitney Canada Corp. Turboshaft Engines | Mar 26, 2013 | Engine (PW206B2) |
| 2009-03-05 | Pratt & Whitney Canada PW206A, PW206B, PW206B2, PW206C, PW206E, PW207C, PW207D, and… | Mar 27, 2009 | Engine (PW206B2) |
| 2004-22-11 | Eurocopter Deutschland GmbH Model EC135 P1, P2, T1, and T2 Helicopters | Dec 7, 2004 | Airframe (EC 135 P2+)Only with: Main rotor drive aluminum torque strut assembly P/N L633M1001 103 or L633M1001 105 installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (9)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Fuselage · floor panel · damagedJun 15, 2026
DAMAGE 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 METHODS ENGINEERING AUTHORIZATION…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor drive · warning message · illuminatedMar 27, 2026
TRANSMISSION CHIP CAUTION ILLUMINATED MULTIPLE TIMES WHILE IN CRUISE FLIGHT. CAUTION REMAINED ON FOR LAST 3 MINUTES OF FLIGHT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · unknown · odorFeb 13, 2026
AFTER 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 BURNING.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 9 reportsShow fewer reports
- Air conditioning and pressurization · unknown · odorFeb 26, 2025
CREW 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.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · warning unit · unserviceableApr 30, 2023
INFLIGHT 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 LATE FROM THE FIELD
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · warning unit · unserviceableApr 30, 2023
INFLIGHT 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 SUBMITTED UNDER SDR #…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · unknown · unknownApr 30, 2023
CORRECTION TO PREVIOUS SUBMISSION. THIS WAS INCORRECTLY SUBMITTED UNDER CONTROL NUMBER QMLA202305050031. (THIS CONTROL # WAS PREVIOUSLY USED) NEW SDR SUBMITTED AS QMLA2023050520036 N819LF 0781
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · none · damagedMay 2, 2022
COMPLETION 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 STARTING 03/30/2022, EXPECTED RTS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Power plant · wire · unsecureJun 19, 2020
AC 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 WIRE WOUND THROUGH THE INTERIOR FOR…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026