- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0605
- Year built
- 2007
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- November 20, 2007
- Certificate issued
- April 24, 2013
- Expires
- April 30, 2029
- Mode S code
- A02E21
Eurocopter Deutschland EC 135 T2+TCDS H88EUAirframe · Eurocopter Deutschland EC 135 T2+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 · Eurocopter Deutschland EC 135 T2+
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 N110VUMatched 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 T2+ aircraft
FAA incident reports
No FAA accident or incident reports matched to N110VUMatched 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 T2+ aircraft
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2026101375412Frame · gougedDAMAGE WAS FOUND TO THE SURFACE OF THE RH SIDE WINDOW FRAME PN: L533M1207205 IN THE FORM OF MULTIPLE GOUGES AND CRACKS, REQUIRING REPLACEMENT OF THE WINDOW FRAMESDR 2A6R2026100275411Beam · crackedMULTI-CRACKS ARE FOUND ON THE UPPER SHEET OF BEAM FRAME 5, AND OEM OUTER DOUBLER, APPROXIMATELY 1- 2.25” LONG, REF RDAS-EC135-53-2026-3392SDR 2A6R2026100275410Frame · mechanic errorTWO DRILL MARKS ON THE STRUCTURE UNDERNEATH OF THE TRANSMISSION DECK. THE MARK IS 0.129" IN DIAMETER WITH A DEPTH OF 0.016". THE DAMAGE TO THE FRAME IS 0.128" IN DIAMETER WITH A MAX DEPTH OF 0.018"SDR 2A6R2026092975409Bracket · corrodedEC135 S/N 0605 WAS FOUND TO HAVE HEAVY CORROSION ON THE T-CAP P/N L533M1028203 ON TOP OF T-CAP UNDER MAIN CABIN FLOOR AT FS3150MM, LBL100MM – RBL450MM THE DAMAGE REQUIRED REPLACEMENT OF THE T-CAP, AND DUE TO AVAILABILITY, A NEW T-CAP WAS LOCALLY FABRICATEDSDR 2A6R2026092475408Xmsn Deck · dentedA SURFACE DAMAGE (DENT) IS FOUND ON THE TRANSMISSION DECK UPPER SURFACE, UNDER AFT OTBD SECTION OF THE RH XY FITTING, APPROXIMATELY 2.5” LONG, 0.05” WIDE AND 0.032” DEPTH. FOR DETAILS SEE AIRBUS RDAS-EC135-53-2026-3264ASDR 2A6R2026092275407Keelbeam · corrodedDAMAGE TO THE LH KEEL BEAM CAP IN THE FORM OF SEVERAL AREAS OF CORROSION WAS DISCOVERED. THE DAMAGE IS LOCATED ON THE UPPER SURFACE OF THE PART UNDER THE COCKPIT FLOOR, WITH THE LARGEST DAMAGE AREA REPORTED TO BE APPROXIMATELY 0.5” X 0.5” IN SIZE AND 0.018” SDR 2A6R2026091675406Frame · crackedDAMAGE WAS DISCOVERED ON THE CABIN OVERHEAD LONGERON (PN: L533M1017282) IN THE FORM OF TWO CRACKS ON EITHER SIDE OF THE CUTOUT. THE CRACK MEASURES APPROXIMATELY 0.50” LONG (AFT) AND 1.00” LONG (FWD)SDR 2A6R2026091675405Gusset · corrodedEC135 S/N 0605 WAS FOUND TO HAVE CORROSION DAMAGE TO THE BULKHEAD, PN L533M1028221 (APPROX. FS 3150 MM)AND GUSSETS PN: L533M1028227 AND PN: L533M1028228. REPLACEMENTS WERE NOT AVAILABLE WITHIN SCHEDULED RTS AND PARTS WERE FABRICATEDSDR 2A6R2026091675404Angle · corrodedACFT WAS FOUND TO HAVE CORROSION DAMAGE TO THE FRAME 2 ANGLE PN L533M1043427 (APPROX. FS 2675 MM). REPLACEMENT WAS NOT AVAILABLE WITHIN SCHEDULED RTS AND PART WAS FABRICATEDSDR 2A6R2026090375403Frame · corrodedFOUND CORROSION DAMAGE ON FRAME 1, REQUIRING REPLACEMENT OF THE FRAME.SDR 2A6R2026082575402Frame · crackedTWO CRACKS APPROXIMATELY 6MM IN LENGTH EACH WERE DISCOVERED ON THE LH UPPER FRAME 5 MEDICAL INTERIOR MOUNT LOCATION. BOTH CRACKS PROPAGATED FROM THE SAME RIVET HOLE AT APPROXIMATELY FS: 4780, WL: 2400, AND BL: -710. THE CRACKS WERE LESS THAN 1.5” IN LENGTH ANSDR 2A6R2026081675401Attach Angle · corrodedCORROSION DAMAGE OF VARYING DEPTHS WAS FOUND ON THE LOWER LT AND RT BROOM CLOSET ATTACHMENT ANGLES (P/N: L533M1052317), AS WELL AS THE AFT ATTACHMENT ANGLE (P/N: L533M1052318)SDR QMLA2025112520117Circuit Breaker · trippedELECTRICAL BURNING SMELL DURING APPROACH BACK TO BASE. SMELL FADED, INSTRUMENT LIGHTING WAS NO LONGER FUNCTIONING. INSTRUMENT LIGHTS C/B HAD TRIPPED.SDR QMLA2025031920037Probe · malfunctionedAIRCRAFT FUEL INDICATIONS ERRONEOUS. INDICATED 12-20 GALLONS LESS UPON TAKEOFF THAN ASSUMED TO BE IN AIRCRAFT. AFTER 15 MINUTES IN FLIGHT, FUEL INDICATIONS STILL SHOWED MORE FUEL THAN WHEN DEPARTED. REMOVED INSPECTED CLEANED AND REINSTALLED #1 AND #2 SUPPLY SDR QMLA2024020120010Warning Message · false activationNO.2 ENG CHIP DURING CRUISE FLIGHT PRIOR TO BEGINNING APPROACH TO KMRC IN MT. PLEASANT, TN. ENGINE PRESSURES AND TEMPERATURES WERE WITHIN NORMAL LIMITATIONS AND NO ABNORMAL SIGNS OR VIBRATIONS WERE ENCOUNTERED. ENG CHIP WAS SERVICED BY MT. PLEASANT MECHANICS
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.