N28831976 Beechcraft 200
This N-number isn't registered right now. Below is its last known registration, canceled Apr 10, 2019.
Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply4 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Twa International INC
- Owner type
- Corporation
- City, state
- Cheyenne, WY
- Certificate issued
- Jan 28, 2019
- Canceled
- Apr 10, 2019
- Airworthiness
- Standard · Normal
- Airworthiness date
- Apr 30, 1976
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
- 200
- Year
- 1976
- Serial number
- BB-144
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 11
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Mode S code
- A2EE74
Engine
- Make and model
- U/A Canada Pt6a-41
- Type
- Turbo-prop
- Power
- 850 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2019Twa International INCCheyenne, WY
- 1927Wyoming Airways CorpCasper, WY · different airframe: Alexander Long Wing Eaglerock S/N 160
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 (4)
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 |
|---|---|---|---|
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (200)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; … |
| 98-20-38 | Raytheon Aircraft Company 200 Series Airplanes | Sep 29, 1998 | Airframe (200) |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (200) |
| 97-23-17 | Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as… | Dec 29, 1997 | Airframe (200)Certain serial numbers: C90 LJ-683–LJ-1463; C90A LJ-683–LJ-1463; E90 LW-177–LW-347; F90 LA-1–LA-236; H90 LL-1–LL-61; A100 B-228–B-247; … |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (4)
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 · actuator · failedApr 26, 1999
LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. REPLACED MOTOR, SEVERAL CYCLES CARRIED OUT ON JACK, PROPER OPS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · detector · corrodedApr 9, 1999
FALSE FIRE WARNING, RT ENGINE. POSSIBLY CAUSED BY AGE OF THE UNIT, OR MOISTURE AND SOAP CREEPING INSIDE. SUBMITTER SUGGESTED BETTER SEALING OF DETECTOR.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · bolt · brokenMay 22, 1998
DURING LANDING, RT MAIN LANDING GEAR LEG PIVOT BOLT BROKE ALLOWING GEAR TO FOLD AFT INTO NACELLE AND RT INBOARD FLAP. PROPELLER REPEATEDLY STRUCK RUNWAY DURING LANDING ROLL-OUT AND ENGINE WAS RUNNING PART OF THE TIME DURING ROLL-OUT. BOTH REMOVED FOR REPAIR AS REQUIRED.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reportsShow fewer reports
- Engine fuel and control · lever · jamsJul 25, 1995
LEFT POWER LEVER WOULD INTERMITTENTLY STOP BEFORE FULL TRAVEL IN QUADRANT, LIMITING ENGINE SPEED TO APPROXIMATELY 80 PERCENT N1. ENGINE WAS NEWLY OVERHAULED, AND FCU LEVER, PN 311458-01, WAS INSTALLED DURING C/W SB 3304. FCU LEVER FOUND JAMMING ON PROPELLER REVERSE CONTROL FOLLOWING LEVER.…
From FAA Service Difficulty Reports; matched by N-number and serial number.
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