- Registered owners
- Ihc Health Services Inc DBAIhc Life Flight
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 10033
- Year built
- 1988
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- May 2, 2018
- Certificate issued
- August 26, 2003
- Expires
- April 30, 2028
- Mode S code
- AC7395
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 46
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1978 | 1 |
|---|---|
| 1998 | 2 |
| 1999 | 3 |
| 2000 | 3 |
| 2002 | 2 |
| 2003 | 4 |
| 2004 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 1 |
| 2013 | 6 |
| 2014 | 6 |
| 2015 | 3 |
| 2016 | 2 |
| 2017 | 2 |
| 2018 | 2 |
| 2020 | 1 |
| 2021 | 5 |
| 2022 | 2 |
| 2023 | 3 |
| 2024 | 1 |
| 2025 | 3 |
| 2026 | 1 |
Airframe · Agusta S P A A109K2
AD 2026-17-07Main rotor mast/swashplateAD 2025-17-10Main Rotor ControlAD 2025-07-01Air Data ComputerInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N901HCMatched 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 S P A A109K2 aircraft
FAA incident reports
No FAA accident or incident reports matched to N901HCMatched 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 S P A A109K2 aircraft
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR I7LA0002746Trunnion · overheatedSEPT 5, 2004. AIRCRAFT TT: 3518.7 UPON 25 HOUR INSPECTION, TAIL ROTOR TRUNION ENAMEL PAINT DISCOLORED. SIGNS OF EXCESSIVE HEAT.SDR I7AL0002748Trunnion · overheatedUPON DAILY INSPECTION, MECHANIC FOUND ABNORMAL PLAY IN TAIL ROTOR ASSEMBLY. TRUNION- FURTHER INSPECTION FOUND SIGNS OF EXCESSIVE HEAT TO TRUNION ENAMEL PAINT DISCOLORED (BROWN).SDR I7LA0002736Trunnion · looseUPON DAILY INSPECTION, MECHANIC NOTED EXCESSIVE PLAY IN TAIL ROTOR HUB AT TRUNION AREA. TAIL ROTOR HUB WAS REMOVED FOR INSPECTION A SOFT FACE MALLET WAS REQUIRED TO FREE THE TRUNION FROM TAIL ROTOR GEARBOX OUTPUT SHAFT. REMOVAL OF TRUNION NOTED SIGNS OF EXCESDR I7LA0002739Gearbox · damagedREMOVAL OF TAIL ROTOR HUB AND BLADE ASSY. FOUND TAIL ROTOR GEARBOX OUTPUT SHAFT TO HAVE METAL TRANSFER TYPE DAMAGE TO SPLINE AREA. HEAT GENERATED FROM THE TAIL ROTOR TRUNION WAS ALSO EVIDENT.SDR I7LA0002728Trunnion · overheatedUPON 25 HOUR INSPECTION, SIGNS OF HEAT NOTED. ENAMEL PAINT WAS BROWN-DISCOLORED.
STCs that may be installed · 40
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 40 STCs