- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 6335
- Year built
- 1989
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- October 24, 2001
- Certificate issued
- July 22, 2020
- Expires
- July 31, 2027
- Mode S code
- A45A08
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 78
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1986 | 1 |
|---|---|
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 3 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 8 |
| 2004 | 3 |
| 2005 | 2 |
| 2006 | 2 |
| 2008 | 2 |
| 2010 | 4 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 8 |
| 2014 | 3 |
| 2015 | 4 |
| 2016 | 8 |
| 2017 | 1 |
| 2018 | 2 |
| 2020 | 4 |
| 2021 | 16 |
| 2022 | 8 |
| 2023 | 1 |
| 2024 | 1 |
| 2025 | 5 |
| 2026 | 1 |
Airframe · Eurocopter AS365N3
AD 2026-17-05Cabin Equipment/FurnishingsAD 2025-14-07Fire Detection SystemAD 2025-13-09Main rotor controlInformation bulletins that may apply · 3
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N38MDMatched 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 AS365N3 aircraft
FAA incident reports
No FAA accident or incident reports matched to N38MDMatched 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 AS365N3 aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2011FA0000672Lockwasher · misinstalledINCORRECT APPLICATION OF LOCKING WASHERS ON ROTOR SHAFT NUT RETAINER LOCK (117-12118-01). INCORRECT APPLICATION OCCURRED DURING INSTALLATION OF REPLACEMENT ROTOR SHAFT. DISCOVERED WHILE PERFORMING MAIN GEARBOX LOWER CASING REPAIR. (REMOVAL OF ROTOR SHAFT RESDR 2011FA0000673Bearing · failedFAILURE OF INPUT PINION TAPERED ROLLER BEARING OF TAIL ROTOR GEARBOX. FAILURE OCCURRED DURING GROUND RUN AFTER MX. REPLACEMENT OF TAIL ROTOR GEARBOX. TAIL ROTOR GEARBOX INPUT CASING DISCOLORED DUE TO OVERHEATING OF FAILED BEARING. INPUT PINION SEIZED.SDR 97ZZZX4831Valve · leaksDRAIN VALVE LEAKS AT SEAMS.SDR 96ZZZX207Transmitter · defectiveOIL PRESSURE TRANSMITTER FLUCTUATING AND PEGGING AT 5 BARS.
STCs that may be installed · 47
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.