- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 28114
- Year built
- 1982
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- January 2, 1998
- Certificate issued
- September 8, 2022
- Expires
- September 30, 2029
- Mode S code
- A48A42
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 N392ALMatched 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 N392ALMatched 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 ALG2006F00035Current Limiter · inoperativeIN FLIGHT, EN ROUTE, THE FOLLOWING INDICATION WENT TO (0). NR 1 NG, NR 1 ENG PRESS, TEMP, C-BOX PRESS, NR 1 HYD PRESS, NR 2 HYD TEMP. NO CAUTION LIGHTS ILLUMINATED. AC DIVERTED, MAINTENANCE REMOVED AND REPLACED NR 1 CURRENT LIMITER, (PN 209-375-096-103). (SDR ALG2004F00059Warning Light · activatedFIVE MINUTES AFTER TAKEOFF, AC815 TRANSMISSION CHIP LIGHT ILLUMINATED, PILOT RETURNED TO RIG. MECHANIC REMOVED, CLEANED, AND INSPECTED ALL TRANSMISSION CHIP PLUGS, NO CONTAMINANTS NOTED. CONNECTOR PLUGS WERE EXAMINED AND FOUND SERVICEABLE. AC WAS RETURNED TSDR ALGA084114Rotor Head · wornTAIL ROTOR HEAD REMOVED DUE TO YOKE FEATHERING, BEARING BORE WORN BEYOND LIMITS.SDR 2002F00900Light · contaminatedDURING PREFLIGHT CHECK, NR 1 FIRE LIGHT WOULD NOT TEST, WATER CONDUCTOR. AFTER BEING DRIED OUT SYSTEM OPERATED PROPERLY. (M)SDR 20010502CW007Relay · malfunctionedDURING COOL DOWN AFTER LANDING, AN ELECTRICAL SMELL WAS NOTED. SEARCH LIGHT RELAY WAS FOUND TO BE THE CAUSE OF THE SMELL.SDR 20010314CW003Bolt · brokenDURING DAILY INSPECTION, FOUND UPPER RETAINER BOLT, PN NAS6606D70, ON THE FWD NODAL BEAM ASSY HELPER SPRING BROKE, CRACKING THE HELPER SPRING SIDE PLATE AND CAUSING CONTACT DAMAGE TO THE RIGHT TORSION ARM ASSEMBLY. NEED SCHEDULED INSPECTION OR RETIREMENT OF BSDR 99ZZZX514Blade · crackedDURING DAILY INSPECTION, FOUND OUTER SKIN CRACK ON BLADE.
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