Single-engine piston

N301DW

Homebuilt Quicksilver GT

Registered No accidents on file
Built
—
Serial
GT2801093
Class
Single-engine piston
Engines
Rotax 447
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Meridian, ID
Registration record

N301DW on the FAA register

Type
Homebuilt Quicksilver GT
Serial
GT2801093
Engines
Rotax 447
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Meridian, ID
Certificate issued
2020-10-21
Airworthiness date
2007-04-24
Registration expires
2027-10-31
Airworthiness class
Experimental · light-sport
Mode S (hex)
A32369
Mode S (octal)
50621551
Seats (type)
1
Weight class
up to 12,499 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2027-10-31
    Registration expires (renewal due).
  • 2020-10-21
    Certificate of registration issued as N301DW to the current registrant.
  • 2007-04-24
    Airworthiness date on the current FAA record (experimental category (light-sport)).
  • 1995-05-11
    N301DW previously assigned to a Cessna 152 (s/n 15285319); cancelled.
Overview

About N301DW

N301DW is a Homebuilt Quicksilver GT, serial number GT2801093. It is registered to an individual in Meridian, Idaho. The current certificate of registration was issued on October 21, 2020 and expires on October 31, 2027.

The FAA aircraft reference file describes the type as a single-engine piston, one Rotax 447 engine and 1 seats. Its airworthiness certificate is experimental category (light-sport), dated April 24, 2007.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N301DW. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

1992-10-05 Accident · Milford, NH Damage: Substantial NTSB · NYC93LA008
Reported aircraft: Cessna 152 II — a different aircraft that carried the N301DW registration before this airframe.
Probable cause: THE INSTRUCTOR PILOTS IMPROPER IN-FLIGHT PLANNING, AND HIS FAILURE TO MAINTAIN A PROPER GLIDE PATH TO THE FORCED LANDING AREA. A FACTOR IN THIS ACCIDENT WAS THE INSTRUCTOR'S DECISION TO SHUT DOWN THE ENGINE DURING A 'SIMULATED' ENGINE FAILURE .

Sources: NTSB aviation accident database and CAROL case system, FAA preliminary accident & incident notices. Search accident records

Same state

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Data: FAA Aircraft Registry (October 2026), including deregistered aircraft; NTSB and FAA accident data; fyiAero listing history. Individual owners' names are shown to signed-in users and street addresses are never shown. Type figures are published specifications, not this aircraft's.