- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 28117
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Experimental, showing compliance
- Airworthiness date
- April 14, 1997
- Certificate issued
- September 8, 2022
- Expires
- September 30, 2029
- Mode S code
- A48DF9
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CT7 model are included below.
On this page
Airworthiness directives that may apply · 48
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1981 | 1 |
|---|---|
| 1982 | 1 |
| 1984 | 2 |
| 1986 | 2 |
| 1987 | 2 |
| 1988 | 2 |
| 1990 | 1 |
| 1994 | 3 |
| 1996 | 1 |
| 1997 | 6 |
| 1998 | 3 |
| 1999 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 2 |
| 2013 | 3 |
| 2014 | 1 |
| 2017 | 1 |
| 2018 | 1 |
| 2020 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 2 |
| 2025 | 2 |
See all 54 ADs
Information bulletins that may apply · 1
Advisory, not mandatory.
Engine · GE CT7 series
SAIB ANE-98-31NTSB investigations
No NTSB investigations matched to N393ALMatched 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 Bell 214ST aircraft
FAA incident reports
No FAA accident or incident reports matched to N393ALMatched 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 Bell 214ST 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 9EKA2015052019Fuel Filter · restrictedNUMBER 2 ENG FUEL FILTER MASTER CAUTION LIGHT CAME ON WHEN THE ENG WAS AT 60 % TQ , INDICATING A FUEL FLOW RESTRICTION.SDR 9EKA2015040314Plate · tornDURING CRUISE FLIGHT , PILOT REPORTED UNUSUAL VIBRATIONS. DURING INSPECTION, NODAL BEAM PLATES & HELPER SPRING FOUND TO HAVE TORN ELASTOMERIC RUBBER.SDR 9EKA2015010601Pump · wornDURING FLIGHT, NR 1 FUEL TRANSFER PUMP LIGHT FLICKERED. ACFT WAS ON LAST MISSION RETURNING TO BASE.SDR ALG2003F00008Wire · brokenON THE PREFLIGHT CHECK, NR 2 FIRE DETECTION SYSTEM INOPERATIVE. A WIRE WAS FOUND BROKEN AT THE NR 2 FIRE DETECTION AMPLIFIER.SDR ALG2003F3ADPBearing · failedDURING DAILY INSPECTION. BEARINGS OUTER LINER COMING APART DUE TO HIGH VIBRATION, SCRAPPED 4 EACH BEARINGS. CLOSER DAILY INSPECTION OF TAILROTOR ASSEMBLY.SDR ALG2003F00067Bolt · brokenDURING THE DAILY SERVICE CHECK. BROKEN TAIL ROTOR YOKE PLATE BOLT.SDR 20010517CW002Light · inoperativeON PRE-START CHECK, LEFT HAND BAGGAGE FIRE DETECTION SYSTEM WOULD NOT TEST, TEST LAMP BURNED OUT AND WIRE BROKEN ADJACENT TO SMOKE DETECTOR.
STCs that may be installed · 50
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 50 STCs