- Registered owner
- Intermountain Medical Transport LLC
- Location
- Salt Lake City, UT
- Owner type
- LLC
- Serial number
- 22313
- Year built
- 2013
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- October 9, 2014
- Certificate issued
- June 19, 2026
- Expires
- June 30, 2033
- Mode S code
- A2F9E3
Agustawestland AW109SPTCDS H7EUAirframe · Agustawestland AW109SPTCDS E42NEEngine · Pratt & Whitney Canada PW207C
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 |
Airframe · Agustawestland AW109SP
AD 2026-17-07Main rotor mast/swashplateAD 2026-17-05Cabin Equipment/FurnishingsAD 2025-18-01Main Rotor HeadInformation bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Agustawestland AW109SP
SAIB SW-18-13Main Transmission Plate FittingNTSB investigations
No NTSB investigations matched to N291HCMatched 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 Agustawestland AW109SP aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2019FA0000414Trunnion · scoredPILOT REPORTED A MAIN ROTOR VIBRATION. UPON TRACK AND BALANCE OF THE MAIN ROTOR IT WAS DISCOVERED THAT THE VIBRATION WAS FROM THE TAIL ROTOR. THIS WAS NOT A COMMON OCCURRENCE AS THE TAIL ROTOR UNDERGOES A DETAILED INSPECTION EVERY 200-HOURS. IT IS VERY UNCOMMOSDR I7LA2018081800125Oil Cooler · wornPILOT NOTED A SLIGHT INCREASE, WITHING LIMITS IN THE NR 1 ENGINE OIL TEMP DURING FLIGHT. DURING FINAL APPROACH, THE OIL TEMP STARTING INCREASING, THE PILOT ABORTED THE APPROACH, SECURED THE NR 1 ENGINE IAW THE RFM AND SUCCESSFULLY COMPLETED A RUN ON LANDINGSDR I7LA201705110103Attach Fitting · crackedDURING A 1200 HOUR INSPECTION, A CRACK WAS FOUND IN THE LOWER LT TAIL BOOM ATTACH FITTING. AFTER REMOVING THE TAIL BOOM, FOUND A CRACK IN THE BULKHEAD & FRAME ASSEMBLY.
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.