Single-engine piston

N3176G

Homebuilt GT-400

Registered No accidents on file
Built
—
Serial
GT2801474
Class
Single-engine piston
Engines
Rotax 503 DCDI
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Georgetown, TX
Registration record

N3176G on the FAA register

Type
Homebuilt GT-400
Serial
GT2801474
Engines
Rotax 503 DCDI
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Georgetown, TX
Certificate issued
2020-06-08
Airworthiness date
2007-07-03
Registration expires
2027-06-30
Airworthiness class
Experimental · light-sport
Mode S (hex)
A36403
Mode S (octal)
50662003
Seats (type)
1
Weight class
up to 12,499 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2027-06-30
    Registration expires (renewal due).
  • 2020-06-08
    Certificate of registration issued as N3176G to the current registrant.
  • 2007-07-03
    Airworthiness date on the current FAA record (experimental category (light-sport)).
  • 1997-03-25
    N3176G previously assigned to a Beechcraft F33A Bonanza (s/n CE1271); cancelled.
Overview

About N3176G

N3176G is a Homebuilt GT-400, serial number GT2801474. It is registered to an individual in Georgetown, Texas. The current certificate of registration was issued on June 8, 2020 and expires on June 30, 2027.

The FAA aircraft reference file describes the type as a single-engine piston, one Rotax 503 DCDI engine and 1 seats. Its airworthiness certificate is experimental category (light-sport), dated July 3, 2007.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N3176G. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

1995-09-24 Accident · Farmingdale, NY Damage: Destroyed Fatal injury NTSB · BFO95FA097
Reported aircraft: Beechcraft F33A — a different aircraft that carried the N3176G registration before this airframe.
Probable cause: failure of the pilot to maintain pitch control of the airplane during the initial climb after lift-off, which resulted in a steep climb, loss of airspeed, and a resultant stall/spin and subsequent crash. A factor relating to the accident was: failure of the pilot to properly set the elevator trim before takeoff.

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

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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.