- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- 45389
- Year built
- 1980
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Restricted, aerial surveying
- Airworthiness date
- March 20, 1981
- Certificate issued
- May 21, 2025
- Expires
- May 31, 2032
- Mode S code
- A02232
Bell Helicopter Textron 206L-1TCDS H2SWAirframe · Bell Helicopter Textron 206L-1Engine modelAllison 250 SER 317HP
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 64
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1980 | 3 |
|---|---|
| 1981 | 3 |
| 1982 | 1 |
| 1983 | 1 |
| 1985 | 2 |
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 2 |
| 1989 | 2 |
| 1991 | 4 |
| 1992 | 2 |
| 1994 | 3 |
| 1995 | 3 |
| 1996 | 2 |
| 1999 | 2 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 1 |
| 2007 | 2 |
| 2008 | 2 |
| 2009 | 2 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 3 |
| 2014 | 2 |
| 2015 | 1 |
| 2017 | 1 |
| 2019 | 2 |
| 2021 | 4 |
| 2022 | 4 |
| 2023 | 2 |
| 2024 | 1 |
Airframe · Bell Helicopter Textron 206L-1
AD 2024-20-07Emergency Equipment; Emergency Flotation SectionAD 2023-11-07Ground Proximity SystemAD 2023-06-05Tail Rotor Drive ShaftInformation bulletins that may apply · 7
Advisory, not mandatory.
Airframe · Bell Helicopter Textron 206L-1
SAIB SW-19-05Tail Rotor Drive System, Spline DamageSAIB SW-18-02Loss of Hardware Tail Rotor Drive Shaft CouplingsSAIB SW-12-45Garmin Model 400W/500W Series GPS-WAAS Navigation SystemSAIB SW-10-42R1Emergency Float KitsSAIB SW-08-42Emergency Float with Liferaft Kits (kits)SAIB SW-05-24SAIB SW-04-92Historical bulletins · 1
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 19901120060889IPower On Descent (Rotorcraft) · Gulf Of Mexico, LAPilot struck tv antenna with tail rotor on short final to offshore heliport. Landed safely.Accident 19840516024819APwr Off Run Land (Autorotation · Mt Mckinley Vil, AKEngine flamed out. Made a hard auto rotation landing to reach the strip. Both fuel line poppet valves jammed closedAccident 19831229075519APwr Off Run Land (Autorotation · Wasilla, AKEngine failed on climbout. Hard landing severed tailboom. First stage turbine wheel had failed from hot starts.
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ALG2005F00054Switch · failedDURING RUN UP THE FLOAT WOULD NOT ARM, THE PILOT SHUT THE AC DOWN AND NOTIFIED MAINTENANCE. THE MECHANIC REMOVED AND REPLACED THE FLOAT ARM SWITCH AND THE AC WAS RETURNED TO SERVICE UPON COMPLETION OF THE FUNCTION CHECKS. (K)SDR 2004F00285Structure · vibrationTRANSITION INTO CRUISE FLT PRODUCED A LATERAL LOW FREQUENCY VIBRATION, RETURNED TO ICY. MAINTENANCE VISUALLY INSPECTED AIRCRAFT FOR DISCREPANCY, NO DEFECTS NOTED THAT WOULD CAUSE A LATERAL VIBRATION, COMPLIED WITH A OPS CHECK FLIGHT AND NO LATERAL VIBRATION WSDR ALG2003F00086Starter Gen · failedCOMING TO A HOVER FOR TAKE OFF. N2 DROOPED TO 94 PERCENT AT 50 PERCENT TORQUE AND STAYED THERE FOR 15 SECONDS. ABLE TO RECOVER BY BEEPING. BEFORE HOVER, N2 WAS STABILIZED AT 100 PERCENT. MAINTENANCE REPLACED STARTER GENERATOR.SDR ALG2003F00082Governor · malfunctionedUPON COMING TO A HOVER. NR 2 DROPPED TO 92 PERCENT AND TOOK UP TO 15 SECONDS TO RECOVER AT HIGH TORQUE SETTING (ABOVE 80 PERCENT) N2, WOULD NOT DROOP AT LOW TORQUE SETTING. MAINTENANCE CHANGED GOVERNOR, LINER ACTUATOR, AND CHECKED NR2 RIGGING, CHECKED GOOD.SDR ALG2003F00021Fuel Control · failedDURING START, NR 1 ENGINE DID NOT EXCEED 30 PERCENT, PILOT ABORTED THE START AND USED BATTERY CART TO START THE AIRCRAFT. NO POWER FROM BATTERY CART, APU CIRCUIT BREAKER POPPED, UPON RESET THE PILOT OBSERVED A SPARK FROM THE OVERHEAD CIRCUIT BREAKER PANEL. TSDR 97ZZZX934Blade · debondedDURING A LIGHTNING STRIKE INSPECTION, FOUND CORROSION AND DEBONDING OVER SPAR AT TIP (SKIN).SDR 97ZZZX933Blade · debondedLIGHTNING STRIKE INSPECTION FOUND M/R BLADE CORRODED AND DEBONDED AT TIP OF BLADE.SDR 96ZZZX5508Lever Idler · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. SUBMITTESDR 96ZZZX5507Link Assy · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. SUBMITTESDR 96ZZZX289Link Idler · wornDURING DAILY INSPECTION, FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. SDR 96ZZZX288Lever Assy · wornDURING DAILY INSPECTION, FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. SDR 95ZZZX2780Bulkhead · crackedAFTER REMOVAL OF SHIMS IN ORDER TO COMPLY WITH TB 206L-94-169. FORWARD RING WAS FOUND CRACKED UNDER SHIM AT LT LOWER ATTACH POINT. APPARENTLY, THIS IS A STRESS CRACK CAUSED BY WORKING RIVETS IN THE INTERCOSTAL ASSEMBLY.SDR 95ZZZX1235Link Idler · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 2 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH NAS6605D64 BOLTS. NORMAL OPERATION CAUSES PARTS TO WEAR OUT TOO SOON. SPACERS, BEARINGS, ANSDR 95ZZZX1234Lever Assy · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 2 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH NAS6605D64 BOLTS. NORMAL OPERATION CAUSES PARTS TO WEAR OUT TOO SOON. SPACERS, BEARINGS, AN
STCs that may be installed · 459
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.