- Registered owner
- Intermountain Medical Transport LLC
- Location
- Salt Lake City, UT
- Owner type
- LLC
- Serial number
- 22247
- Year built
- 2011
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- November 22, 2011
- Certificate issued
- June 18, 2026
- Expires
- June 30, 2033
- Mode S code
- A28366
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 37
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2009 | 1 |
|---|---|
| 2012 | 1 |
| 2013 | 3 |
| 2014 | 3 |
| 2015 | 3 |
| 2016 | 1 |
| 2018 | 5 |
| 2019 | 1 |
| 2020 | 3 |
| 2021 | 6 |
| 2022 | 6 |
| 2023 | 2 |
| 2024 | 2 |
| 2025 | 4 |
| 2026 | 2 |
See all 43 ADs
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Agusta AW109SP
SAIB SW-18-13Main Transmission Plate FittingNTSB investigations
No NTSB investigations matched to N261HCMatched 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 Agusta AW109SP aircraft
FAA incident reports
No FAA accident or incident reports matched to N261HCMatched 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 Agusta AW109SP aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2023FA0000426Bolt · groovedIT WAS REPORTED AS THE AIRCRAFT WAS COMING IN FOR A 200-HOUR INSPECTION. A SLIGHT BUMP COULD BE FELT IN FLIGHT; DURING THE INSPECTION, ALL PC LINK ROD ENDS, AND BOLTS WERE INSPECTED, AND THE BLUE UPPER BOLT WAS FOUND TO HAVE A STEP WORN INTO IT, THE BOLT WAS RSDR 2014FA0000562Blade · crackedDURING A DAILY INSPECTION , A ONE INCH CRACK ON ONE OF THE TWO TAIL ROTOR BLADES WAS DETECTED. INITAL INSPECTION WAS VISUAL A 10X GLASS WAS USED TO VARIFY. AIRCRAFT WAS REMOVED FROM SERVICE AND WILL RETURN TO SERVICE AFTER A SERVICEABLE TAIL ROTOR BLADE IS I
STCs that may be installed · 32
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 32 STCs