N153GA1985 Beechcraft 1900C
Safety record in brief:No NTSB accidents or incidents since 198223 ADs may apply29 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Alpine Aviation INC
- Owner type
- Corporation
- City, state
- Provo, UT
- Certificate issued
- Sep 17, 2013
- Expires
- Sep 30, 2029
- Airworthiness
- Standard · Normal
- Airworthiness date
- Mar 1, 1985
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Beechcraft
- Model
- 1900C
- Year
- 1985
- Serial number
- UB-34
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 19
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Mode S code
- A0D5EB
Engine
- Make and model
- P&W Canada Pt6a-60a
- Type
- Turbo-prop
- Power
- 1050 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2013 – nowAlpine Aviation INCProvo, UT · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (23)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2014-02-03 | Flight Controls | Mar 7, 2014 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439 |
| 2013-24-03 | Stabilizers | Jan 13, 2014 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439 |
| 2009-23-03 | Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft… | Dec 14, 2009 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439 |
| 2009-23-01 | Hawker Beechcraft Corporation Model 1900, 1900C, and 1900D Airplanes | Dec 8, 2009 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439. Only with: Equipped with Hawker Beechcraft MLG actuator P/N 114-380041-11, -13, -15, or -15OVH (or FAA-approved equivalent, including Frisby P/N 1FA10043-3). |
| 2006-18-51 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Sep 8, 2006 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439 |
Show all 23 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2005-18-21 | Raytheon Aircraft Company Models 1900, 1900C, 1900C (C-12J), and 1900D Airplanes | Sep 13, 2005 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-439 |
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (1900C)Certain serial numbers: 65-A90, B90, C90, C90A LJ-76; 65-A90, B90, C90, C90A LJ-114–LJ-1691; E90 LW-1–LW-347; F90 LA-2–LA-236; 99, 99A, A99A, B99, C99 U-1–U-239; 100, A100 B-1–B-94; … |
| 2004-09-30 | Raytheon Aircraft Company Model 1900C Airplanes | Jun 18, 2004 | Airframe (1900C)Certain serial numbers: 1900C UB-1–UB-35 |
| 2004-09-07 | Raytheon Aircraft Company Model 1900, 1900C, 1900C (C-12J), and 1900D Airplanes | Jun 14, 2004 | Airframe (1900C)Certain serial numbers: 1900 UA-1–UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-113. Only with: Applies to airplanes that do not have canted bulkhead Kit No. 129-4005-1 incorporated. |
| 2004-01-13 | Raytheon Aircraft Company Model 1900, 1900C, and 1900D Airplanes | Feb 19, 2004 | Airframe (1900C)Certain serial numbers: 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900 UD-1–UD-6; 1900D UE-1–UE-427. Only with: Equipped with vent blower assembly P/N 114-380028-1, 114-380028-3, 114-380028-5, or 114-380028-7. |
| 2003-20-10 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | Oct 15, 2003 | Airframe (1900C) |
| 2003-03-18 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | Feb 5, 2003 | Airframe (1900C) |
| 2002-23-13 | Pratt & Whitney Canada PT6A Series Turboprop Engines | Dec 31, 2002 | Engine (PT6A-60A)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed. |
| 2001-22-16 | Raytheon Aircraft Company Beech Models 1900, 1900C (C-12J), and 1900D Airplanes | Dec 17, 2001 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-302 |
| 2001-18-07 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | Oct 12, 2001 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-345; … |
| 2000-20-07 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | Nov 22, 2000 | Airframe (1900C)Certain serial numbers: 1900D UE-1–UE-376. Only with: Airplanes required to have a cockpit voice recorder (CVR) installed; for 1900 and 1900C, all serials with RAC Kit No. 114-3020 (-1, -3, -7, or -9), 114-3032-1, or 114-3008-1 incorporated, or where RAC installed the CVR. |
| 97-15-13 R2 | Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D Airplanes | May 28, 1999 | Airframe (1900C)Certain serial numbers: 1900 UA-1–UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-157 |
| 99-04-08 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Mar 26, 1999 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-299 |
| 99-01-03 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Feb 8, 1999 | Airframe (1900C)Certain serial numbers: 1900 UA-1; 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; … |
| 98-26-16 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Feb 5, 1999 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-271 |
| 98-21-20 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Nov 20, 1998 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-268 |
| 97-26-15 | Raytheon Aircraft Company Models 1900, 1900C, and 1900D Airplanes | Jan 25, 1998 | Airframe (1900C)Certain serial numbers: 1900 UA-2; 1900 UA-3; 1900C UB-1–UB-74; 1900C UC-1–UC-174; 1900C UD-1–UD-6; 1900D UE-1–UE-249; …. Only with: Equipped with at least one P/N 114-380041-11 (or FAA-approved equivalent) main landing gear actuator. |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (1900C) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (29)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Power plant · engine · shutdownJul 12, 2022
PS NORMAL THROUGH 10,000 FT. CLIMBING THROUGH ABOUT 10500 FT THE PILOT NOTICED THE RH TORQUE GAUGE BEGIN TO FALL, THEN THE RH OIL PRESSURE LIGHT CAME ON. PILOT FELT A YAW, WAITED ABOUT THIRTY SECONDS TO CONFIRM FAILURE, SECURED THE ENGINE AND RETURNED BACK TO BIL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · unknown · unknownDec 7, 2021
GOT SMOKE/HAZE IN THE COCKPIT ONCE LEVELED IN CRUISE. TURNED BACK TO BIL AND SHUT OFF THE BLEED VALVES. ONCE BLEED VALVES WERE OFF THE COCKPIT CLEARED. LANDED AND TAXIED WITH NO ISSUES.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Windows · windshield · crackedDec 13, 2016
THE PILOT’S SIDE WINDSHIELD CRACKED DURING FLIGHT. THERE WAS A 3 INCH WIDE BAND OF SHATTERING OF THE OUTER LAYER THAT RAN FROM THE TOP TO THE BOTTOM OF THE WINDSHIELD ON THE INBOARD EDGE NEXT TO THE CENTER POST.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · skin · corrodedAug 30, 2013
CORROSION FOUND ON BELLY OF ACFT UNDER ADF ANTENNA BS 183.25. REPAIRED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · seat track · corrodedMar 10, 2010
LEFT SIDE SEAT RAIL CORRODED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · blade · brokenDec 28, 2004
AIRCRAFT DEPARTED, AT CRUISE, THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LEFT ENGINE SEIZED. PRE INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · blade · brokenDec 28, 2004
AIRCRAFT DEPARTED AT CRUISE. THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LT ENGINE SEIZED. PRE-INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · cable · brokenNov 16, 2004
ON CLIMBOUT THE AIRSTAIR DOOR OPENED. AC RETURNED, WHEN AIRSTAIR DOOR OPENED IN FLIGHT, DOOR DAMPER BROKE AND SUPPORT CHAINS BROKE. CHAIN HIT PROPELLER AND CAUSED NOTICEABLE DAMAGE. DOOR ANNUNCIATOR LIGHT WAS NOT ILLUMINATED SO NO INDICATION OF ANY PROBLEM WAS EVIDENT. CAUSE FOR DOOR FAILURE WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Power plant · bulkhead · crackedOct 15, 2001
THE RIGHT ENGINE COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS CRACKED ON THE RIGHT LOWER SIDE. THIS LOCATION IS WERE ONE OF THE FOUR BOLTS SECURE THE LOWER COWL TO THE BULKHEAD. (PICTURES INCLUDED)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · shaft · damagedOct 4, 2001
INSPECTION OF THE FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE CABLES DIAGONAL WRAP TO BE UNWINDING. CONTINUED INSPECTION REVEALED THAT THREE OF THE FOUR CABLES TO BE UNWINDING. THE CABLES WERE INSTALLED IN THE CORRECT FASHION. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 29 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026