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Aircraft record

N899CA1969 Beechcraft 99A

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19822 ADs may apply12 service difficulty reports

Registration
Valid
expires Feb 28, 2030
Based in
Provo, UT
owner city / state
Engine
PT6 SER 578HP · 550 hp
U/A Canada
Owners
1
since 2011
NTSB events
None
since 1982
ADs may apply
2
confirm with A&P
Service reports
12
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Alpine Aviation INC
Owner type
Corporation
City, state
Provo, UT
Certificate issued
Feb 14, 2011
Expires
Feb 28, 2030
Airworthiness
Standard · Normal
Airworthiness date
Jun 30, 1970

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
99A
Year
1969
Serial number
U-104
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
17
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
AC66F6

Engine

Make and model
U/A Canada Pt6 Ser 578hp
Type
Turbo-prop
Power
550 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. 2011 – 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, 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 (2)

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
2004-17-02Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series AirplanesOct 4, 2004Airframe (99A)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; …
97-25-03Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series AirplanesJan 21, 1998Airframe (99A)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (12)

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.

  • Landing gear · none · noneSep 30, 2022

    WE WERE SCHEDULED FOR AN AIRCRAFT SWAP IN KBTM. I TOOK OFF OUT OF KRXE AT 10AM ON OUR IFR FLIGHT PLAN. ON THE WAY INTO KBTM WE ENCOUNTED SOME WEATHER, WE DID THE ILS 15 INTO KBTM. INBOUND ON THE ILS WE PUT THE GEAR DOWN AND NOTICED WE DIDN'T HAVE THE RIGHT GEAR INDICTION SO WE WENT MISSED AND FLEW…

    From FAA Service Difficulty Reports; matched by N-number.
  • Landing gear · handle · shortedAug 20, 2018

    WITH LANDING GEAR HANDLE SELECTED DOWN, NO GREEN DOWN AND LOCKED INDICATION ALONG WITH RED HANDLE WARNING. PILOT NOTED LANDING GEAR CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER WHICH RESULTED IN NORMAL OPERATION. INVESTIGATION FOUND LANDING GEAR SELECTOR HANDLE HAD A METAL ID PLATE SEPARATED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · circuit breaker · defectiveNov 28, 2016

    AFTER TAKEOFF THE LANDING GEAR FAILED TO RETRACT. LANDING GEAR CB WAS POPPED. PILOT ELECTED TO RETURN TO THE AIRFIELD AND LANDED UNEVENTFULLY. SUBSEQUENT INVESTIGATION FOUND THE LANDING GEAR REMOTE CIRCUIT BREAKER HAD VERY HIGH RESISTANCE IN THE CLOSED POSITION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Landing gear · flasher · faultyNov 11, 2015

    GEAR IN TRANSIT WARNING STAYED ON AFTER GEAR SELECTED UP, FOLLOWING TAKEOFF. PILOT RETURNED TO TAKEOFF AIRFIELD FOR UNEVENTFUL LANDING. SUBSEQUENT INSPECTION DETERMINED ALL GEAR FUNCTIONS WERE NORMAL. ERRONEOUS IN TRANSIT WARNING DETERMINED TO BE CAUSED BY FAULTY LG WARNING HORN FLASHER.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · crackedJun 8, 2012

    A CRACK WAS DISCOVERED IN THE UPPER WING SKIN OUTBOARD OF THE NACELLE AND AFT OF THE MAIN WING SPAR ON THE RIGHT WING. REMOVED THE DAMAGED SECTION OF SKIN. FABRICATED A NEW SECTION OF SKIN USING THE SAME TYPE MATERIAL AND THICKNESS AND INSTALLED USING A SPLICE DOUBLER OF ONE SIZE GREATER THICKNESS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · cam · damagedDec 22, 2011

    WHEN THE PILOT SELECTED GEAR UP AFTER DEPARTURE FROM BIL, THE GREEN LIGHTS EXTINGUISHED BUT THE RED IN-TRANSIT LIGHT DID NOT EXTINGUISHED. EXTENDED THE GEAR AND GOT 3 GREEN, RETRACTED THEM AGAIN AND STILL HAD THE IN TRANSIT LIGHT STAY ON. AT THIS POINT RETURNED AND LANDED WITHOUT INCIDENT.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · switch · inoperativeOct 31, 2007

    GEAR-IN-TRANSIT LIGHT DID NOT EXTINGUISH AFTER TAKE-OFF AND GEAR UP. PILOT CYCLED GEAR AGAIN WITH SAME RESULT. PILOT RETURNED TO DEPARTURE AND LANDED. MECHANIC FOUND THAT THE LT POWER LEVER SWITCH HAD FAILED. REPLACING THE SWITCH RESOLVED THE PROBLEM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · failedNov 18, 2005

    AIRCRAFT IN FLIGHT AT 13000 FT OIL PRESSURE AND TORQUE STARTS TO FLUCTUATED SLIGHTLY, MOMENTS LATER THE ENGINE FAILED. NO CAUSE FOR FAILURE HAS BEEN FOUND AT THIS TIME. THE ENGINE HAS BEEN TAGGED. THE ENGINE HAS 87.5 HOURS SINCE REPAIRS TO THE ENGINE AT AN ENGINE SHOP. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · collar · crackedFeb 5, 2002

    DURING AN INSPECTION OF THE ELEVATOR, IT WAS FOUND THAT THE OUTBOARD ELEVATOR COLLAR WAS CRACKED AT THE TAPER PIN. THE DEFECTIVE TORQUE TUBE WAS REPLACED AND THE NEW TUBE (SERVICEABLE) WAS RIGGED IAW MM. INSPECTION OF THE CRACKED COLLAR WAS INCONCLUSIVE AS TO WHETHER THE CRACK WAS CAUSED BY NORMAL…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · mount · chafedJan 22, 2001

    IT WAS DISCOVERED DURING AN ENGINE CHANGE, THAT THE TUBE MOUNT HAD CHAFE MARKS BEYOND LIMITS. THE TUBE MOUNT WAS REPLACED WITH A SERVICABLE TUBE MOUNT. THE CAUSE OF THE CHAFING WAS DUE TO INDEQUATE CLEARANCE BETWEEN MOUNT AND BAFFLING AND FUEL LINES.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 12 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

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