- Registered owner
- Bank Of Utah Trustee
- Location
- Salt Lake City, UT
- Owner type
- Corporation
- Serial number
- BB-258
- Year built
- 1977
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Multiple
- Airworthiness date
- August 31, 2009
- Certificate issued
- December 4, 2020
- Expires
- December 31, 2027
- Mode S code
- AC3C03
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 59
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 1 |
|---|---|
| 1975 | 3 |
| 1976 | 5 |
| 1977 | 4 |
| 1978 | 3 |
| 1979 | 1 |
| 1980 | 3 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 1 |
| 1992 | 2 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 4 |
| 1998 | 4 |
| 2003 | 3 |
| 2004 | 3 |
| 2005 | 5 |
| 2006 | 1 |
| 2008 | 3 |
| 2012 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2025 | 1 |
See all 61 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N888ETMatched 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 Beech 200 aircraft
FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 19861001064479ITakeoff Ground Roll · Milwaukee, WINosewheel fork assembly failed at start of takeoff roll. Assembly was previously cracked but within limits.Incident 19840501027519IRoll-Out (Fixed Wing) · Waukegan, ILLeft main landing gear collapsed while using heavy braking on a fast speed turn off after landing.
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2026FA0000733Actuator · damagedAIRCRAFT NLG ACTUATOR & ATTACHING PARTS DAMAGED DURING RIGGING OPS. ALL LANDING GEAR ACTUATORS WERE BEING REPLACED WITH OVERHAULED UNITS. TO FACILITATE REMOVAL OF THE ACTUATORS, THE LANDING GEAR WAS MOVED TO THE IN-TRANSIT POSITION AND LEFT IN THAT POSITION. SDR 2026FA0000671Eva Tube · blownIN ROUTE OVER KCOU WHEN THE MASTER CAUTION CAME ON AND THE LT BLEED FAIL LIGHT ILLUMINATED. THE PILOTS FOLLOWED THE CHKLIST & CLOSED LT BLEED VALVE. THE CHKLIST INSTRUCTED THEM TO DESCEND BELOW 14K. ASKED ATC, CENTER WAS VERY BUSY & TO GIVE THEM PRIORITY HAND
STCs that may be installed · 422
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 200
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA4175NMInstallation of fully enclosed main landing gear door system for high-flotation- gear-equipped aircraft.STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.