- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0416
- Year built
- 2005
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 29, 2005
- Certificate issued
- March 3, 2026
- Expires
- March 31, 2033
- Mode S code
- AC9C2B
Airbus Helicopters Deutschland EC135T2+TCDS H88EUAirframe · Airbus Helicopters Deutschland EC135T2+TCDS E34NEEngine · Turbomeca ARRIUS-2B2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2005 | 1 |
|---|---|
| 2007 | 1 |
| 2008 | 2 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2019 | 3 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 3 |
| 2025 | 4 |
| 2026 | 6 |
Airframe · Airbus Helicopters Deutschland EC135T2+
AD 2026-20-06Main rotor gearboxAD 2026-17-05Cabin Equipment/FurnishingsAD 2026-08-10Passenger compartment equipmentInformation bulletins that may apply · 3
Advisory, not mandatory.
Airframe · Airbus Helicopters Deutschland EC135T2+
SAIB SW-12-45Garmin Model 400W/500W Series GPS-WAAS Navigation SystemSAIB SW-09-26Operation with Emergency Flotation System ARMEDSAIB SW-08-42Emergency Float with Liferaft Kits (kits)NTSB investigations
No NTSB investigations matched to N911UGMatched 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 Airbus Helicopters Deutschland EC135T2+ aircraft
FAA incident reports
No FAA accident or incident reports matched to N911UGMatched 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 Airbus Helicopters Deutschland EC135T2+ aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2025022020022Engine · making metalABOUT 1-2 MILES OUT FROM PATIENT PICKUP THE #1 ENG CHIP LIGHT ILLUMINATED. POWER WAS DECREASED AND THE LIGHT EXTINGUISHED. POWER WAS SLIGHTLY BROUGHT BACK IN TO SEE IF IT RETRIGGERED THE ANOMALY, WHICH IT DID. THE CHIP BURN SWITCH WAS IDENTIFIED AND THE PROCEDSDR 2A6R2022101103Deck Plate · delaminatedDURING 1000 HOUR INSPECTION, DELAMINATION DAMAGE WAS DISCOVERED ON THE AFT CABIN FLOOR (PN: L533M1015104) ON THE LOWER SKIN PANEL (PN: L533M1416234) MEASURING APPROXIMATELY 8.5” X 7.75” AT THE FORWARD SIDE OF THE FLOOR. A DETAILED DESCRIPTION OF THE DAMAGE ANSDR 2A6R2022101165202Frame · crackedDURING A SCHEDULED INSPECTION ASB21-01, DAMAGE WAS DISCOVERED AT FRAME 5 AT APPROXIMATELY FS 4,709MM RELATING TO THE STC SR00566DE, DRAWING 739-1600, WALL. THE DAMAGE IS ADJACENT TO THE MEDICAL WALL ATTACH FITTING LOCATIONS. PERFORMED THE ALERT SERVICE BULSDR 2A6R2022101165201Deck Plate · corrodedDURING 1000 HOUR INSPECTION, CORROSION DAMAGE WAS DISCOVERED ON THE COCKPIT FLOOR (PN: L533M1013108) AT THE RH FORWARD GROUNDING POINT. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDA
STCs that may be installed · 71
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.