- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0704
- Year built
- 2008
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- September 12, 2008
- Certificate issued
- January 20, 2016
- Expires
- January 31, 2029
- Mode S code
- A0157E
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 N104VUMatched 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 N104VUMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2A6R2025103074503Floorbeam · corrodedDURING INSPECTION, HEAVY CORROSION WAS DISCOVERED ON T-CAP P/N L533M1028203 ON TOP OF T-CAP UNDER MAIN CABIN FLOOR AT FS3150MM, LBL500MM - RBL500MM. THE T-CAP IS NOT AVAILABLE FOR PURCHASE.; THEREFORE, A REPLACEMENT T-CAP WAS FABRICATED AS PER THE INSTRUCTION SDR 2A6R2025103074502Floor Skin · dentedDURING INSPECTION, DAMAGE WAS DISCOVERED TO THE COCKPIT FLOOR UPPER SKIN PANEL (P/N: L533M1014217) IN THE FORM OF MULTIPLE DENTS AND DEBONDED SKIN. THE DENTED AND DEBONDED AREAS ARE REPORTED TO BE FROM 0.50” X 0.50” IN SIZE TO 4.0” X 4.0” IN SIZE. A DETAILED DSDR 2A6R2025103074501Attach Angle · corrodedDURING INSPECTION, CORROSION DAMAGE WAS DISCOVERED ON THE LOWER LH, RH & AFT BROOM CLOSET ATTACHMENT ANGLES (L533M1052317 (X2) & L533M1052318). A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED FABRICATED PROCEDURE IS PROVIDED IN AIR METHODS ENGINEERING AUSDR QMLA2024100120127Unknown · odorSHORTLY AFTER TAKE OFF PILOT AND MEDICAL CREW NOTICED A SMELL OF. HOT ELECTRICAL WIRING/COMPONENTS IN BOTH THE COCKPIT AND CABIN AREAS, WITH NO EVIDENCE OF SMOKE OR FIRE. FOUND HOTDOG SPLICE RESTING AGAINST PILOT PITOT HEATER BREAKER CONTACT. HOTDOG SPLICE ANSDR QMLA2024061020062Engine · warning light#1 ENG CHIP LIGHT ILLUMINATED ENROUTE BACK TO HOME BASE. EMERGENCY PROCEDURES WERE PERFORMED IAW WITH THE RFM. LANDING AT HOME BASE WAS ACCOMPLISHED WITHOUT INCIDENT. APPROPRIATE LOGBOOK ENTRIES AND NOTIFICATIONS WERE MADE.SDR QMLA2024030420027Chin Bubble · damagedBIRD STRIKE IN CRUISE FLIGHT CAUSE DAMAGE TO PILOT WINDSCREEN, CO-PILOT CHIN BUBBLE. POST FLIGHT INSPECTION BY MECHANIC FOUND DAMAGE TO TWO MAIN ROTOR BLADES AND CO-PILOTS KICK/FLOOR PANEL.SDR QMLA2010083110054Wire Harness · burnedA STRONG ELECTRICAL ODOR WAS NOTICED BY THE PILOT AND THE MEDICAL CREW MEMBERS ON A RETURN FLIGHT TO THE BASE. IT WAS BELIEVED TO BE COMING FROM THE AIR CONDITIONING SYS. ONCE ON THE GROUND AND SHUTDOWN, THE ODOR WAS STRONGEST IN THE RT CABIN OVERHEAD LOCATI
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.