- Registered owner
- Mercy Hospital Springfield
- Location
- Springfield, MO
- Owner type
- Corporation
- Serial number
- 0817
- Year built
- 2009
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- October 12, 2009
- Certificate issued
- November 12, 2013
- Expires
- November 30, 2029
- Mode S code
- A6C405
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 22, 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 N535LLMatched 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 N535LLMatched 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 HDNA2018070940817Blade · crackedMAIN ROTOR BLADE HAS CRACK LOCATED ON BOTTOM SIDE 15 INCHES INBOARD OF THE TIP THAT IS BEYOND FIELD REPAIR CRITERIA GIVEN IN THE REPAIR MANUALS.SDR HDNA2018070930817Blade · crackedMAIN ROTOR BLADE HAS CRACK LOCATED ON THE TOP SIDE 35.5 INCHES OUTBOARD OF THE CUFF THAT IS BEYOND FIELD REPAIR CRITERIA GIVEN IN THE REPAIR MANUALS.SDR HDNA2018070920817Blade · crackedMAIN ROTOR BLADE HAS CRACK LOCATED ON BOTTOM SIDE 48 INCHES OUTBOARD OF THE CUFF THAT IS BEYOND FIELD REPAIR CRITERIA GIVEN IN THE REPAIR MANUALS.SDR HDNA2018070910817Blade · crackedMAIN ROTOR BLADE HAS CRACK LOCATED ON THE TOP SIDE, 104 1/8 INCHES OUTBOARD OF THE BLADE CUFF THAT IS BEYOND FIELD REPAIR CRITERIA GIVEN IN THE REPAIR MANUALS.SDR HDNA2018070900817Skin Panel · corrodedCORROSION DETECTED BEYOND LIMITS PUBLISHED IN REPAIR MANUALS AROUND RIGHT AFT FOOT STEP ON SIDE OF FUSELAGE.SDR HDNA201807090817Skin Panel · corrodedCORROSION BEYOND LIMITS PUBLISHED IN REPAIR MANUALS AROUND LEFT AFT FOOT STEPS ON SIDE OF FUSELAGE.SDR HDNA201660823008Thermal Bypass · failedTHERMAL BYPASS VALVE FAILED IN CLOSED POSITION NOT ALLOWING OIL TO OIL COOLER.SDR HDNA20151012004Fire Detector · defectiveDURING CRUISE FLIGHT, AUDIBLE WARNING GOING FOR FIRE DETECTION, SOUNDED WITH NO WARNING, LIGHT ILLUMINATION. MADE PRECAUTIONARY LANDING & UPON LANDING SAW FAINT FIRE WARNING LIGHT ILLUMINATION.
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.