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Aircraft record

N528WG1979 Beechcraft 200

DeregisteredNot yet verified by ownerSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 18, 2010.

Safety record in brief:1 NTSB accident (substantial damage, Oct 2006)6 ADs may apply1 service difficulty report

Registration
Deregistered
Last based in
California, MD
owner city / state
Engine
PT6A-41 · 850 hp
P&W Canada
Owners
1
since 1999
NTSB events
1
substantial, 2006
ADs may apply
6
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Tigress Air III LLC
Owner type
Corporation
City, state
California, MD
Certificate issued
May 5, 1999
Canceled
Nov 18, 2010
Airworthiness
Experimental · Research and Development
Airworthiness date
Nov 4, 2005

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
200
Year
1979
Serial number
BB-151
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Not Type Certificated
Seats
11
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A6A8A1

Engine

Make and model
P&W 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
  1. 1999 – 2010Tigress Air III LLCCalifornia, MD

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 (1)

Accident · substantial damage

Oct 12, 2006 · Leonardtown, MD

The airplane manufacturer's inadequate landing gear downlock plate maintenance orientation information, and the disengaged main landing gear.

Damage
Substantial
Injuries
None
Report
NYC07LA006

From NTSB records; matched by serial number.Read NTSB report (search CAROL for NYC07LA006)

Accident history for this model

ADs published since 1998 that may apply (6)

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
2012-09-10Pratt & Whitney Canada Turboprop EnginesMay 23, 2012Engine (PT6A-41)Only with: Engines with power section maintenance involving first stage sun gear or planet gear replacement since December 22, 2008, and with TAATI PMA first stage sun gears P/N E3028456 or E3037304, or planet gear sets P/N E3101455-02 or E3101525-02 installed.
2004-17-02Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series AirplanesOct 4, 2004Airframe (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; …
2002-23-13Pratt & Whitney Canada PT6A Series Turboprop EnginesDec 31, 2002Engine (PT6A-41)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed.
98-20-38Raytheon Aircraft Company 200 Series AirplanesSep 29, 1998Airframe (200)
97-25-03Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series AirplanesJan 21, 1998Airframe (200)
Show all 6 ADs
ADSubjectEffectiveApplies to
97-23-17Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as…Dec 29, 1997Airframe (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 (1)

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 · lock plate · misinstalledOct 17, 2006

    DURING POST ACCIDENT INSPECTION OF RT AND LT MAIN LANDING GEAR DRAG LEGS, LOCK PLATES WERE FOUND MOUNTED WITH THE BEVEL AT THE NOSE OF THE PLATE FACING UP. INSPECTION OF 5 OTHER AC FOUND THE BEVEL FACING DOWN. REVIEW OF CURRENT REPS COMPONENT MM IS INCONCLUSIVE. (K)

    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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