- Registered owner
- Tvpx Trust Co LLC Trustee
- Location
- North Salt Lake, UT
- Owner type
- LLC
- Serial number
- 920210
- Year built
- 2013
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- July 31, 2013
- Certificate issued
- September 17, 2026
- Expires
- September 30, 2033
- Mode S code
- AD122C
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 42
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2005 | 1 |
|---|---|
| 2006 | 3 |
| 2007 | 1 |
| 2009 | 4 |
| 2010 | 3 |
| 2011 | 4 |
| 2012 | 4 |
| 2013 | 3 |
| 2014 | 3 |
| 2015 | 2 |
| 2016 | 3 |
| 2017 | 7 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 1 |
| 2021 | 5 |
| 2022 | 4 |
| 2023 | 2 |
| 2024 | 2 |
See all 54 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N941PHMatched 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 Sikorsky S-92A aircraft
FAA incident reports
No FAA accident or incident reports matched to N941PHMatched 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 Sikorsky S-92A aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HEEA202405140001Switch · faultedDOOR OPEN LIGHT ILLUMINATED UPON REACHING CRUISE FLIGHT. EMERGENCY PROCEDURE PERFORMED AND LIGHT EXTINGUISHED WHILE SLOWING AIRSPEED TO 80 KNOTS. VERIFIED THE DOOR WAS LATCHED CORRECTLY AND THE PINS WERE IN. AFTER SPEEDING BACK UP TO CRUISE SPEED THE LIGHT CAMSDR HEER20160918235Fire Detector · false indicationINTERMITTENT FIRE LIGHT AND AURAL ON NR 1 ENGINE. TESTED THE NR 1 ENGINE FIRE DETECTION SYSTEM IAW S92A-AMM-000 TASK 26-11-00710-001 REV. 33. CHECKED GOOD. INSPECTED INBOARD AND OUTBOARD DETECTORS WIRING AND CONNECTORS, NO DEFECTS NOTED. FAULT COULD NOT BESDR HEER20160801932Abrasion Strip · departedEROSION STRIP DEPARTED AIRCRAFT. PN FOR ABRASION STRIP IS FOUND IN THE SPECIAL INSTRUCTIONS NN 92-097, PAGE 5. REPLACED MAIN ROTOR BLADE.SDR HEER20160325336Servo · leakingNR 2 HYD LEVEL LOW CAUTION LIGHT IN FLIGHT. FOUND LT MAIN SERVO LEAKING AT PISTON SEAL. REPLACED MAIN ROTOR SERVO.SDR HEER20151001743Wire Harness · damagedPICKED UP TO HOVER, STARTED TAKEOFF. NR 2 ENGINE FIRE LIGHT ILLUMINATED WITH AUDIO FIRE NR 2. REPLACED NR 2 AFT FLAME DETECTOR HARNESS ASSY.SDR HEER20150923716Fire Detector · false activationNR 2 FIRE LIGHT INTERMITTENT IN FLIGHT. REPLACED DETECTOR AND HARNESS, CHECKED GOOD.SDR HEER20141205539Fire Detector · false activationDURING CRUISE FLIGHT NR 2 FIRE LIGHT ILLUMINATED INTERMITTENTLY. REPLACED THE AFT FLAME DETECTOR ON THE NR 2 ENG.
STCs that may be installed · 120
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 120 STCs