- Registered owner
- Alpine Aviation Inc
- Location
- Provo, UT
- Owner type
- Corporation
- Serial number
- UB-7
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- March 30, 1984
- Certificate issued
- July 23, 2010
- Expires
- October 31, 2027
- Mode S code
- A06DCD
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 35
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 | 6 |
| 1998 | 3 |
| 1999 | 4 |
| 2000 | 1 |
| 2001 | 2 |
| 2003 | 3 |
| 2004 | 4 |
| 2005 | 2 |
| 2006 | 1 |
| 2009 | 2 |
| 2011 | 1 |
| 2012 | 1 |
| 2014 | 2 |
| 2023 | 1 |
See all 43 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N127BAMatched 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 1900 aircraft
FAA incident reports
No FAA accident or incident reports matched to N127BAMatched 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 Beech 1900 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 TIMA20170321006Seat Track · corrodedDURING A SCHEDULED STRUCTURAL INSPECTION OF THE FUSELAGE, THE RT AFT SEAT TRACK WAS FOUND TO BE CORRODED IN SEVERAL AREAS.SDR TIMA20170321005Seat Track · corrodedDURING A SCHEDULED STRUCTURAL INSPECTION OF THE FUSELAGE, THE LT AFT SEAT TRACK WAS FOUND TO BE CORRODED.SDR TIMA20160326006Bearing · failedPILOT EXPERIENCED AN UNCOMMANDED AILERON INPUT WHEN FLAPS WERE LOWERED FROM TAKEOFF TO APPROACH POSITION, DURING APPROACH. PILOT RETRACTED THE FLAPS TO TAKEOFF POSITION & THE INTERFERENCE WITH THE AILERON WAS ELIMINATED. ACFT WAS LANDED UNEVENTFULLY WITH FLASDR TIMA20160108001Pressure Switch · faultyIMMEDIATELY AFTER ROTATION THE LT PROPELLER AUTO FEATHERED. PILOT REDUCED POWER & IMMEDIATELY LANDED, ABORTING THE TAKEOFF. THE PROBLEM WAS DISCOVERED TO BE A FAULTY AUTO FEATHER LOW PRESS SWITCH.SDR TIMA20130430002Tee Fitting · crackedDURING A SCHEDULED STRUCTURAL INSP A CRACK IN THE LT HORIZONTAL STABILIZER LOWER TEE EXTRUSION WAS DISCOVERED. REPAIRED THE CRACKED TEE EXTRUSION BY SPLICING IN A NEW SECTION OF TEE EXTRUSION IAW FR-CO-02598. 2 REPAIR ANGLES WERE FABRICATED USING A SECTION SDR TIM2005F00003Skin · corrodedCORROSION FOUND ON LT AND RT ELEVATOR: AFT LOWER SPAR CAP LT SIDE, AFT LOWER SPAR CAP RT SIDE, LT OB HINGE, RT OB HINGE, RT CENTER HINGE, LT ELEVATOR TRIM TAB PUSH ROD, RT ELEVATOR TRIM TAB HORN. (K)SDR TIM2005F00002Skin · corrodedCORROSION FOUND ON SKIN FS243-FS273 AND STRINGERS 14L-15R. (K)
STCs that may be installed · 113
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