- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0346
- Year built
- 2004
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 11, 2004
- Certificate issued
- January 16, 2023
- Expires
- January 31, 2030
- Mode S code
- ACF83F
Eurocopter Deutschland EC 135 P2TCDS H88EUAirframe · Eurocopter Deutschland EC 135 P2TCDS E42NEEngine · Pratt & Whitney Canada PW206B series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada PW206B model are included below.
On this page
Airworthiness directives that may apply · 51
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 |
|---|---|
| 2004 | 2 |
| 2008 | 2 |
| 2009 | 2 |
| 2012 | 4 |
| 2013 | 8 |
| 2014 | 5 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 11 |
| 2022 | 6 |
| 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 N935ACMatched 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 N935ACMatched 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 2A6R202412050001Floor Skin · dentedDURING 1000 HOUR INSPECTION, DENT / DEBOND DAMAGE WAS DISCOVERED ON THE REAR CABIN FLOOR UPPER SKIN PANEL (PN: L533M1016237). A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-5SDR 2A6R2024101771708Tee Fitting · corrodedDURING 1000 HOUR INSPECTION, FOUND CORROSION ON T CAP PN L533M1028203 AT THE CABIN FLOOR RAIL ATTACHMENT. FABRICATED REPLACEMENT PART IAW EC 135 MTC AND AIR METHODS ENGINEERING AUTHORIZATION 23-5300-EA-4882 REV. - DATED 09-05-2024.SDR 2A6R2024101771707Deck Plate · crackedWHILE CHANGING THE L/H XY FITTING FOUND CRACKS UNDERNEATH ON THE TRANSMISSION DECK SKIN PANEL THE CRACKS ARE 1.80 AND 0.65 INCHES LONGSDR 2A6R2024101771706Keelbeam · corrodedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND CORROSION ON THE LEFT AND RIGHT KEEL BEAMS. L/H P/N L533M1009203, R/H P/N L533M1010203SDR 2A6R2024101771705Rib · chafedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND CHAFING IN THE UPPER FENESTRON CLOSE OUT RIB.SDR 2A6R2024101771704Frame · crackedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND FRAME 5 CRACKED ON THE RIGHT AND LEFT BEAM NEAR THE UPPER AND LOWER MOST POINTS WHERE THE MEDICAL INTERIOR BEAM ATTACHES. THE CRACKS ARE NE MORE THAN 1.50 INCHES IN LENGTH.SDR 2A6R2024101771703Frame · corrodedDURING A 1000 HOUR AIRFRAME INSPECTION FRAME 1 HAS EXTENSIVE CORROSION ON THE LOWER FLANGE OF THE FRAME ON THE LEFT AND RIGHT SIDE AS WELL AS CORROSION IN THE WEB OF THE FRAME.SDR 2A6R2024101771702Floorbeam · corrodedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND HEAVY CORROSION ON THE T CAP AT THE CABIN FLOOR RAIL ATTACHMENT.SDR 2A6R2024082871701Frame · crackedDURING A 1000 HOUR INSPECTION, FOUND A 0.25MM CRACK ON THE TAIL CONE UPPER FRAME 7
STCs that may be installed · 72
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.