N197GA1984 Beechcraft 1900C
Safety record in brief:No NTSB accidents or incidents since 198223 ADs may apply22 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Alpine Aviation INC
- Owner type
- Corporation
- City, state
- Provo, UT
- Certificate issued
- Aug 4, 2010
- Expires
- Jan 31, 2028
- Airworthiness
- Standard · Normal
- Airworthiness date
- Aug 3, 1984
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
- 1984
- Serial number
- UB-16
- 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
- A182C3
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- 2010 – 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 (22)
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.
- Windows · windshield · crackedDec 9, 2019
CLIMBED TO 15,000 FT AND HEARD A NOISE THEN NOTICED A CRACK IN WINDSHIELD. CRACK COULD NOT BE FELT ON THE INSIDE. AIRCRAFT RETURNED TO BASE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine oil · hose · chafedOct 30, 2018
ENGINE WAS SHUTDOWN IN FLIGHT AFTER TORQUE AND OIL PRESSURE FLUCTUATIONS. INSPECTION REVEALED THAT THE OIL HOSE CONNECTED BETWEEN THE ENGINE AND OIL COOLER HAD CHAFED THROUGH THE INSULATION AND SHIELDING WHERE THE HOSE RESTED ON THE AFT NACELLE STRUCTURE TO THE POINT OF LEAKING OIL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · doubler · crackedNov 25, 2016
DURING A SCHEDULED SIM CHECK, CRACKS WERE DISCOVERED IN THE DOUBLERS OF THE HORIZONTAL STABILIZER FORWARD ATTACHMENT TO THE VERTICAL STABILIZER. TWO, ONE INCH CRACKS WERE FOUND IN THE LT DOUBLER AND ONE, ONE1 INCH CRACK WAS FOUND IN THE RT DOUBLER. BOTH DOUBLERS WERE REPLACED.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Engine controls · fastener · missingOct 4, 2015
DURING TAKEOFF ROLL, THE RT POWER LEVER DID NOT PROVIDE FULL TRAVEL. TAKEOFF TORQUE COULD NOT BE ACHIEVED ON THE RT ENG & THE TAKEOFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED A MISSING FASTENER IN THE POWER LEVER CLAMP BRACKET UNDER THE PEDESTAL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support · corrodedAug 11, 2014
DURING MX INSPECTION THE LT SIDE SEAT SUPPORT RAIL WAS FOUND TO BE CORRODED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · support · corrodedAug 11, 2014
DURING MX INSPECTION THE RT SIDE SEAT SUPPORT RAIL WAS FOUND TO BE CORRODED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedJul 8, 2011
DISCOVERED CORROSION DAMAGE ON THE FUSELAGE BELLY SKINS DURING VISUAL INSPECTION. REPAIRED SKINS USING COVER PATCH METHOD IAW BEECH SRM 51-70-6.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedJul 8, 2011
DISCOVERED CORROSION DAMAGE ON THE FUSELAGE BELLY SKINS DURING VISUAL INSPECTION. REPAIRED SKINS USING COVER PATCH METHOD IAW BEECH SRM 51-70-6.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · limit switch · brokenOct 28, 2008
THE LANDING GEAR DID NOT EXTEND WHEN SELECTED. THE PILOT MANUALLY PUMPED THE GEAR DOWN AND LANDED. INVESTIGATION REVEALED THAT THE LT UP-LIMIT ELECTRICAL SWITCH HAD PHYSICALLY BROKEN, OPENING THE CIRCUIT TO THE LANDING GEAR CONTROL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · relay · failedJan 17, 2006
LANDING GEAR DID NOT EXTEND WHEN SELECTED. PILOT EXTENDED GEAR MANUALLY AND LANDED WITHOUT INCIDENT. MAINTENANCE DETERMINED THAT THE HYDRAULIC POWER PACK MOTOR RELAY HAD WELDED IN THE CLOSED POSITION RESULTING IN THE MOTOR RUNNING CONTINOUSLY UNTIL IT FAILED. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 22 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