N575F1990 Beechcraft 1900C
Safety record in brief:No NTSB accidents or incidents since 198223 ADs may apply7 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Alpine Aviation INC
- Owner type
- Corporation
- City, state
- Provo, UT
- Certificate issued
- Jan 21, 2015
- Expires
- Jan 31, 2028
- Airworthiness
- Standard · Normal
- Airworthiness date
- Jan 3, 2002
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
- 1990
- Serial number
- UC-99
- 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
- A76179
Engine
- Make and model
- P&W Canada Pt6a-65b
- Type
- Turbo-prop
- Power
- 1173 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2015 – nowAlpine Aviation INCProvo, UT · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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-65B)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 (7)
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.
- Engine air · bleed air sys · smokeDec 3, 2015
ENROUTE, THE LT BLEED FAIL WARNING ILLUMINATED. WHILE FINISHING THE CHECKLIST FOR THE FAILURE SMOKE ENTERED THE CABIN OF THE AIRCRAFT. ELECTED TO CONDUCT A LANDING. UPON LANDING, THE SMOKE DISSIPATED FROM THE CABIN OF THE AIRCRAFT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · motor · failedJul 6, 2011
REPORTED THAT AT APPROX 0130 IN THE MORNING PILOT HAD TO MANUALLY EXTEND THE LANDING GEAR PRIOR TO LANDING. THE PILOT SELECTED GEAR DOWN AND IT DID NOTHING. HE FOUND THE LANDING GEAR RELAY CIRCUIT BREAKER HAD POPPED. HE THEN MANUALLY PUMPED THE GEAR DOWN AND IT INDICATED DOWN AND LOCKED, SO HE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Ice and rain protection · terminal · meltedNov 19, 2009
SHORTLY AFTER TAKEOFF, SMOKE WAS OBSERVED COMING OUT OF F/OS GLARE SHIELD. ACFT RETURNED FOR LANDING. FOUND TERMINAL BLOCK AND RING TERMINAL INSULATION FOR CO-PILOT WINDSHIELD LOW HEAT PWR LEAD MELTED AND CRACKED. THE TERMINAL APPEARED TO BE LOOSE CAUSING A HIGH RESISTANCE CONNECTION LEADING TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reportsShow fewer reports
- Ice and rain protection · terminal · meltedMar 24, 2009
SHORTLY AFTER TAKE OFF, SMOKE WAS OBSERVED COMING OUT OF FIRST OFFICER’S GLARE SHIELD. AIRCRAFT RETURNED FOR LANDING. FOUND TERMINAL BLOCK AND RING TERMINAL INSULATION FOR CO-PILOT WINDSHIELD LOW HEAT POWER LEAD MELTED AND CRACKED. THE TERMINAL APPEARED TO BE LOOSE CAUSING A HIGH RESISTANCE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · bellcrank · mismanufacturedMay 5, 2005
IN ATTEMPTING TO RIG THE ELEVATOR SYSTEM, IT WAS DISCOVERED THE RIGGING HOLE FOR THE FORWARD ELEVATOR BELLCRANK WAS DAMAGED IN THE UPPER ELEVATOR BELLCRANK SUPPORT. IT APPEARED THAT THE HOLE HAD BEEN TORN BY MOVEMENT OF THE BELLCRANK WITH THE RIG PIN INSTALLED. ADDITIONALLY IT WAS DISCOVERED THAT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · seat track · corrodedMay 2, 2005
THE LT FORWARD SEAT TRACK WAS CORRODED THROUGH THE SIDE OF THE TRACK AND THE TRACK AND THE FLANGE THAT SUPPORTS THE FLOORBOARD. CORROSION WAS PARTICULARLY EVIDENT AT FUSELAGE STA 158.5 - 170.5. THE LOCATION OF THE CORROSION, JUST INSIDE THE AIRSTAIR DOOR, SUGGESTS THAT IT MAY BE THE RESULT OF…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · latch · brokenSep 7, 2004
THE AFT UPPER CAMLOCK LATCH WAS BROKEN. THE SHAFT ROTATED PROPERLY AS THE DOOR HANDLE WAS ROTATED TO THE LOCK POSITION, BUT APPROXIMATELY HALF OF THE LIP OF THE CAMLOCK WAS MISSING MAKING IT UNABLE TO CAPTURE THE LATCH POST. TOTAL TIME ON PART UNKNOWN.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026