# N24BH: 1985 Beech 99, registration cancelled 2026-06-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 18, 2026 - Exported to: Bahamas - Status when cancelled: Valid registration - Airframe: [Beech 99](https://openairdocs.org/model/beech-99) (registry code 1154002) - Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032) - Data sheets: [TCDS A14CE](https://openairdocs.org/tcds/A14CE) (OpenAirDocs) - Serial number: U-67 - Year built: 1985 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, normal - Airworthiness date: June 2, 1994 - Certificate issued: July 27, 2010 - Last registry action: March 24, 2023 - Mode S code: A22DC7 - Owner when cancelled: [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC) - Location: [Provo, UT](https://openairdocs.org/faa-place/UT/Provo) - Owner type: Corporation - Owner's area on the map: 40.2272° N, 111.6958° W: Placed by OpenAirDocs at the center of ZIP code 84601, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N24BH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=24BH - Page: https://openairdocs.org/deregistered/N24BH-2026-06-18 From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Beech 99: https://openairdocs.org/model/beech-99.md ## Service difficulty reports (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR TIMA20251226004](https://openairdocs.org/sdr/TIMA20251226004), Dec 23, 2025: ELECTRICAL BOX. CONTAMINATED. WHILE IN CRUISE FLIGHT THE CIRCUIT BREAKER PANEL STARTED SMOKING. PILOT REQUESTED APPROACH FOR PRIORITY IN HELENA, MT. PILOT SAID THE SMOKE SHORTLY STOPPED AFTE - [SDR TIMA20151015006](https://openairdocs.org/sdr/TIMA20151015006), Oct 15, 2015: GEAR SET. STRIPPED. DURING CRUISE CLIMB AT APPROX 9000 FT, THE LT ENG SUDDENLY LOST ALL POWER. ACFT RETURNED TO DEPARTURE LOCATION & LANDED WITHOUT INCIDENT. INSPECTION REVEALED TH - [SDR TIMA20140213005](https://openairdocs.org/sdr/TIMA20140213005), Feb 13, 2014: RIB. CRACKED. INSPECTION REVEALED A CRACK IN THE RT ELEVATOR LE RIB. THE RIB WAS REPLACED WITH A NEW RIB. - [SDR TIMA201000002](https://openairdocs.org/sdr/TIMA201000002), Jan 14, 2010: COWLING. OPEN. COWL OPENED AFTER TAKEOFF. PILOT STATED THAT HE LATCHED THE COWL, BUT THERE IS NO WAY TO VISUALLY CONFIRM THAT THE LATCHES WERE CONNECTED. COWL WAS SUBSTANTIALL - [SDR TIM2006F00001](https://openairdocs.org/sdr/TIM2006F00001), Jan 6, 2006: SKIN. CORRODED. THE SKIN ON THE UPPER LEADING EDGE OF THE RT AILERON WAS FOUND TO BE TEARING AFT. INVESTIGATION DETERMINED THAT THERE WAS SIGNIFICANT CORROSION ON THE INSIDE OF - [SDR TIM2005F00011](https://openairdocs.org/sdr/TIM2005F00011), Nov 8, 2005: GROUND WIRE. CORRODED. LANDING GEAR FAILED TO EXTEND. INSPECTION FOUND A CORRODED GROUND WIRE. THE FAILURE WAS INTERMITTENT THIS CAUSED CONSIDERABLE TROUBLE IN THE TROUBLESHOOTING AND - [SDR 2004F00035](https://openairdocs.org/sdr/2004F00035), Oct 27, 2003: DOOR. DEPARTED. LEFT ENGINE COWLING SIDE DOOR DEPARTED FROM AIRCRAFT DURING FLIGHT. INSPECTION REVEALED THAT THE CAUSE WAS MOST LIKELY, FAILURE TO SECURE DOOR PANEL PRIOR TO FL - [SDR 20000913SH020](https://openairdocs.org/sdr/20000913SH020), Aug 28, 2000: TURBINE. LIGHTNING STRIKE. THE AIRCRAFT WAS BROUGHT INTO MAINTENANCE FOR A SCHEDULED INSPECTION. UPON INSPECTION OF THE LEFT ENGINE, A HOLE WAS FOUND IN THE POWER SECTION CASE. THE HOLE C - [SDR 20000808SH032](https://openairdocs.org/sdr/20000808SH032), Jul 7, 2000: ARM. WORN. NOSE STEERING WAS REPORTED TO BE LOOSE. INSPECTION REVEALED RUDDER PEDAL ARM PIVOT HOLES ELONGATED. REPLACED RUDDER ARM ASSY WITH NEW COMPONENT AND NEW HARDWARE - [SDR 20000808SH031](https://openairdocs.org/sdr/20000808SH031), Jul 7, 2000: ARM. LOOSE. NOSE STEERING REPORTED LOOSE AND INSPECTION REVEALED NOSE STEERING TORQUE ARM HOLE TO ACTUATOR ELONGATED. REPLACED NOSE STEERING TORQUE ARM WITH SERVICEABLE ARM - [SDR 20000803SH010](https://openairdocs.org/sdr/20000803SH010), Jul 7, 2000: VANE. INACCURATE. A TREND HAS DEVELOPED INDICATING PROCEDURES, TECHNIQUES, OR WORKMANSHIP OF OVERHAULED VANE RINGS IS RESULTING IN PREMATURE FAILURE OF PN 3032651 WHICH RESULTS I - [SDR 20000426SH027](https://openairdocs.org/sdr/20000426SH027), Mar 17, 2000: FUEL LINE. CRACKED. DISCOVERED FUEL LEAKING FROM LOWER COWL ON THE LEFT ENGINE ON A POST-FLIGHT INSP. INSP REVEALED THE FUEL LEAK SOURCE TO BE A HIGH PRESSURE FUEL LINE FROM THE FC - [SDR 99ZZZX4113](https://openairdocs.org/sdr/99ZZZX4113), Oct 1, 1999: PUMP. INOPERABLE. FUEL BOOST PUMP INOPERABLE. - [SDR 99ZZZX4175](https://openairdocs.org/sdr/99ZZZX4175), Sep 13, 1999: TIRE. DAMAGED. A NEW TIRE WITH 151 CYCLES INSTALLED ON 9-13-99. DURING INSPECTION, FOUND TIRE TREAD SPLIT AND SEPARATED THE SAME DIRECTION AS TIRE GROOVES. - [SDR 99ZZZX3387](https://openairdocs.org/sdr/99ZZZX3387), Aug 10, 1999: HINGE. BENT. CREW DOOR LEAKS AIR IN-FLIGHT DUE TO SLIGHT MIS-ALIGNMENT ON FORWARD EDGE. PROBLEM FOUND TO BE BENT HINGE ON UPPER FORWARD SIDE. REPLACED HINGE AND INSPECTED AR - [SDR 99ZZZX3006](https://openairdocs.org/sdr/99ZZZX3006), Jul 20, 1999: FUEL CELL. LEAKING. PILOT REPORTED FUEL LEAKING FROM AREA OTHER THAN THE FUEL SUMPS IN THE VICINITY OF THE NACELLE. INSPECTION REVEALED VARIOUS SMALL LEAKS IN THE BLADDER OF THE CE - [SDR 99ZZZX2219](https://openairdocs.org/sdr/99ZZZX2219), May 17, 1999: MOTOR. FAILED. FLAPS WERE INOPERATIVE. MOTOR WINDINGS COOKED (BRUSHES WORN). REPLACED FLAP MOTOR AND GEARBOX AS AN ASSEMBLY. VERIFIED RIGGING OK. MOTOR INOPERATIVE DUE TO NORM - [SDR 99ZZZX794](https://openairdocs.org/sdr/99ZZZX794), Jan 29, 1999: FUEL CELL. LEAKING. PILOT REPORTS RM FUEL LEAK, FUEL DRIPPING FROM GEAR DOOR. FUEL CELL REMOVED AND TESTED. REPLACED CELL. - [SDR 99ZZZX4](https://openairdocs.org/sdr/99ZZZX4), Nov 18, 1998: DEICER. CONTAMINATED. PILOT REPORTED TO MAINTENANCE ICE REMAINING ON TAIL AFTER LANDING. (SPECIFICALLY, BOTH HORIZONTAL SURFACE DEICERS.) OPERATIONAL CHECK OF BOOTS BROKE ICE FORM SU ## FAA accident and incident reports (3) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20060612019569I](https://openairdocs.org/incident/20060612019569I), Jun 12, 2006: Beech 99 (N24BH), Kaunakakai, HI, Minor damage. (-23) Pilot reported gear collapsed on landing. Aircraft skidded off right side of runway. - [Incident 19970305017999I](https://openairdocs.org/incident/19970305017999I), Mar 5, 1997: Beech 99 (N24BH), Billings, MT. Narrative: alpine flight 5001, a BE-99 cargo flight, departed hln for bil on 03-05-97. While enroute, the forward baggage pod door opened allowing some U.S.… - [Incident 19870302017879I](https://openairdocs.org/incident/19870302017879I), Mar 2, 1987: Beech 99 (N24BH), Portland, ME. After liftoff, flaps extended fully and could not be retracted. Returned for landing. Cause undetermined. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.