- Registered owner
- Alpine Aviation Inc
- Location
- Provo, UT
- Owner type
- Corporation
- Serial number
- UB-14
- Year built
- 1984
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- July 13, 1984
- Certificate issued
- July 22, 2008
- Expires
- October 31, 2027
- Mode S code
- A1DCDA
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 37
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1987 | 3 |
|---|---|
| 1989 | 1 |
| 1990 | 1 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 2 |
| 1997 | 7 |
| 1998 | 3 |
| 1999 | 4 |
| 2000 | 1 |
| 2001 | 2 |
| 2003 | 3 |
| 2004 | 4 |
| 2005 | 3 |
| 2006 | 1 |
| 2009 | 2 |
| 2011 | 1 |
| 2012 | 1 |
| 2014 | 2 |
| 2023 | 1 |
See all 45 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
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 · 2
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20210603005949ALanding: Touchdown · Denver, COOn 06/02/2021 at approximately (2000) hrs (MDT), N219VP, sn UB-14, BE-1900, cargo operator [privacy data omitted], during landing runway 17R at Denver International Airport (dia). Reported aircraft landing gear collapsed. Preliminary damage: both engine #1…Incident 20101130051159ITaxi · Greatfalls, MTPilot stated he departed holman aviation on taxiway 'a' between A1 and A2 at kgtf, he was running the checklist, looking inside the cockpit and veried off the left side of the taxiway. The left main gear and nose gear became stuck in a snow bank.
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR TIMA2019103024001Switch · intermittentLANDING GEAR DID NOT EXTEND WHEN SELECTED. PILOT FLEW BY THE TOWER TO VERIFY THAT THE GEAR DID NOT EXTEND. AFTER DEPARTING THE PATTERN TO MANUALLY EXTEND THE GEAR, SUDDENLY THE GEAR OPERATED AND EXTENDED NORMALLY. MAINTENANCE DETERMINED THAT THE ELECTRIC SWSDR TIMA20121003010Door Frame · crackedA CRACK WAS DISCOVERED IN THE AIRSTAIR DOOR FRAME DURING A FUSELAGE "C" STRUCTURAL INSPECTION. THE CRACK WAS LOCATED IN THE LOWER AFT SECTION OF DOOR FRAME AT FS 168. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH BEECH 1900C STRUCTURAL REPAIR MANUAL 53-90-08 &
STCs that may be installed · 120
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 1900
STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light ControllerSTC SA04837NYInstallation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights