- Registered owner
- Air Methods LLC
- Location
- Greenwood Village, CO
- Owner type
- LLC
- Serial number
- 0697
- Year built
- 2008
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 13, 2008
- Certificate issued
- January 13, 2009
- Expires
- April 30, 2029
- Mode S code
- A6A30E
Eurocopter Deutschland EC 135 P2+TCDS H88EUAirframe · Eurocopter Deutschland EC 135 P2+TCDS E42NEEngine · Pratt & Whitney Canada PW206B2
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 50
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 |
|---|---|
| 2008 | 2 |
| 2009 | 2 |
| 2012 | 4 |
| 2013 | 7 |
| 2014 | 6 |
| 2015 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 4 |
| 2020 | 1 |
| 2021 | 11 |
| 2022 | 7 |
| 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 N527BFMatched 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 N527BFMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR QMLA2024113020146Cap · crackedCRACK DISCOVERED ON POST FLIGHT. LOCATED ON MR HUB CAP FLANGE.SDR 2A6R2021122262705Unknown · unknownAFTER REMOVAL OF MAIN GEAR BOX FOR OTHER MAINTENANCE. FOUND THE LEFT XY FITTING P/N L533M2001103 AND THE RIGHT XY FITTING P/N L533M2002103 CORRODED. CLEANED CORROSION AND FOUND BOTH OUT OF LIMITS. THE LEFT ONE IS GETTING REPLACE. THE RIGHT WAS JUST OUT OF SDR 2A6R2021121762704None · noneDURING 1000 HOUR AIRFRAME INSPECTION, FOUND SEVERAL CRACKS UNDER THE MAIN TRANSMISSION DECK. LEFT & RIGHT LONGERONS P/N L533M1017281 & P/N L533M1017282 WERE CRACKED IN THE UPPER FLANGES AT X4565 WITH L/H CRACK MEASURING 0.50 LONG AND R/H MEASURING 0.60 LONE. SDR 2A6R2021121762703None · corrodedDURING 1000 HOUR AIRFRAME INSPECTION, FOUND MULTIPLE ISSUES WITH THE MAIN CABIN FLOOR AS FOLLOWS. RIGHT INBOARD IMBEDDED SEAT TRACK @ F.S. 5730MM, RBL 120MM CORROSION WAS FOUND IN THE WEB AREA AT THE VERY END OF THE TRACK. IN THE SAME AREA ON THE UNDERSIDE OSDR 2A6R2021120662702Keelbeam · corrodedDURING A 1000 HOUR INSPECTION FOUND CORROSION ON THE L/H KEEL BEAM TOP CAT AT NUT PLATE APPROX. F.S 2670MM, LBL 500MM CLEANED CORROSION, REMOVED 0.17 MATERIAL.SDR 2A6R2021120162701Tail Boom · corrodedDURING 1000 HOUR AIRFRAME INSPECTION FOUND CORROSION AT THE TAIL BOOM AFT RING FRAME REINFORCEMENT WHERE SERVICE BULLETIN SB EC135-53-030 WAS PERFORMED. THE CORROSION HAS MITIGATED UNDER THE REINFORCEMENT P/N L535H2100202. REPLACING THE TAIL BOOM.SDR QMLA2017051617051Angle · crackedDURING SCHEDULED MAINTENANCE EVENT, A CRACK WAS FOUND IN THE R/H FWD TRANSMISSION DECK. THIS CRACK WAS REPAIRED UTILIZING ABH EC-135 STRUCTURAL REPAIR MANUAL. THIS AIRCRAFT HAS RETURNED TO SERVICE.SDR QMLA2012012312009Seat · corrodedTHE MECHANIC NOTICED SOME "LEVEL 3" CORROSION ON THE F/A CREW SEAT IN THE CABIN WHILE PERFORMING A SCHEDULED INSPECTION. THE CAUSE OF THIS CORROSION IS UNKNOWN AT THIS TIME. THIS ACFT IS CURRENTLY OUT OF SERVICE.
STCs that may be installed · 74
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.