Skip to content

N528WG

Cancelled 2010

Deregistered aircraft · 1979 Raytheon 200 · Pratt & Whitney Canada PT6A-41

Open in FAA registry

© OpenStreetMap

Cancelled: November 18, 2010
Status when cancelled: Triennial form not returned
Serial number: BB-151
Year built: 1979
Type: Fixed wing multi engine
Engine: Turbo-prop
Airworthiness: Experimental, research and development
Airworthiness date: November 4, 2005
Certificate issued: May 5, 1999
Last registry action: June 16, 2009
Mode S code: A6A8A1
Owner when cancelled: Tigress Air III LLC
Location: California, MD
Owner type: Corporation

Airframe modelRaytheon 200TCDS A24CE · ADs, bulletins and aircraft registered now Engine modelPratt & Whitney Canada PT6A-41TCDS E4EA · Turbo-prop

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 1

Matched to this aircraft by N528WG and the event date: up to this one’s cancellation.

NTSB NYC07LA006Accident · No injuriesLimited investigationFinal reportLeonardtown, MDThe airplane manufacturer's inadequate landing gear downlock plate maintenance orientation information, and the disengaged main landing gear.Oct 12, 2006 · Substantial damage

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N528WG and the event date: up to this one’s cancellation.

Accident 20061012031249ARoll-Out (Fixed Wing) · Leonardtown, MD(-23) After landing, the right hand main gear slowly retracted during roll out. The aircraft stopped and caught fire, destroying the right wing and most of the right side of the fuselage. The right main gear actuator part number 99-810057-651 appears to have…Oct 12, 2006 · Destroyed

Service difficulty reports · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2006FA0001150Lock Plate · misinstalledDURING 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 INCONCLUSOct 17, 2006 · N528WG · Beech 200BEECH · Landing Gear Retraction/Extension System