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Aircraft record

N575F1990 Beechcraft 1900C

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 198223 ADs may apply7 service difficulty reports

Registration
Valid
expires Jan 31, 2028
Based in
Provo, UT
owner city / state
Engine
PT6A-65B · 1173 hp
P&W Canada
Owners
1
since 2015
NTSB events
None
since 1982
ADs may apply
23
confirm with A&P
Service reports
7
since 1995

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 data

Airframe

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
  1. 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, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs 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.

ADSubjectEffectiveApplies to
2014-02-03Flight ControlsMar 7, 2014Airframe (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
2013-24-03StabilizersJan 13, 2014Airframe (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
2009-23-03Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft…Dec 14, 2009Airframe (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
2009-23-01Hawker Beechcraft Corporation Model 1900, 1900C, and 1900D AirplanesDec 8, 2009Airframe (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).
2006-18-51Raytheon Aircraft Company Models 1900, 1900C, and 1900D AirplanesSep 8, 2006Airframe (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 ADs
ADSubjectEffectiveApplies to
2005-18-21Raytheon Aircraft Company Models 1900, 1900C, 1900C (C-12J), and 1900D AirplanesSep 13, 2005Airframe (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
2004-17-02Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series AirplanesOct 4, 2004Airframe (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; …
2004-09-30Raytheon Aircraft Company Model 1900C AirplanesJun 18, 2004Airframe (1900C)Certain serial numbers: 1900C UB-1–UB-35
2004-09-07Raytheon Aircraft Company Model 1900, 1900C, 1900C (C-12J), and 1900D AirplanesJun 14, 2004Airframe (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.
2004-01-13Raytheon Aircraft Company Model 1900, 1900C, and 1900D AirplanesFeb 19, 2004Airframe (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.
2003-20-10Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D AirplanesOct 15, 2003Airframe (1900C)
2003-03-18Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D AirplanesFeb 5, 2003Airframe (1900C)
2002-23-13Pratt & Whitney Canada PT6A Series Turboprop EnginesDec 31, 2002Engine (PT6A-65B)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed.
2001-22-16Raytheon Aircraft Company Beech Models 1900, 1900C (C-12J), and 1900D AirplanesDec 17, 2001Airframe (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
2001-18-07Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D AirplanesOct 12, 2001Airframe (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; …
2000-20-07Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D AirplanesNov 22, 2000Airframe (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 R2Raytheon Aircraft Company Beech Models 1900, 1900C, and 1900D AirplanesMay 28, 1999Airframe (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
99-04-08Raytheon Aircraft Company Models 1900, 1900C, and 1900D AirplanesMar 26, 1999Airframe (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
99-01-03Raytheon Aircraft Company Models 1900, 1900C, and 1900D AirplanesFeb 8, 1999Airframe (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; …
98-26-16Raytheon Aircraft Company Models 1900, 1900C, and 1900D AirplanesFeb 5, 1999Airframe (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
98-21-20Raytheon Aircraft Company Models 1900, 1900C, and 1900D AirplanesNov 20, 1998Airframe (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
97-26-15Raytheon Aircraft Company Models 1900, 1900C, and 1900D AirplanesJan 25, 1998Airframe (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.
97-25-03Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series AirplanesJan 21, 1998Airframe (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 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

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