Single-engine piston

N3UH

2007 Homebuilt Legacy FG

Registered 1 NTSB/FAA record
Built
2007
Serial
LS-223
Class
Single-engine piston
Engines
Aerosport IO-375 series
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Pembroke Pines, FL
Registration record

N3UH on the FAA register

Type
2007 Homebuilt Legacy FG
Serial
LS-223
Engines
Aerosport IO-375 series
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Pembroke Pines, FL
Certificate issued
2017-11-16
Airworthiness date
2010-08-07
Registration expires
2027-11-30
Airworthiness class
Experimental · amateur-built
Mode S (hex)
A31C6A
Mode S (octal)
50616152
Seats (type)
2
Weight class
up to 12,499 lb
Kit
Lancair International Inc LEGACY FG
Status
Current as of October 2026
Registry history

Timeline

  • 2027-11-30
    Registration expires (renewal due).
  • 2020-11-23
    Accident at Hollywood, FL; damage: substantial.
  • 2017-11-16
    Certificate of registration issued as N3UH.
  • 2010-08-07
    Airworthiness date on the current FAA record (experimental category (amateur-built)).
  • 2007
    Manufactured (2007).
Overview

About N3UH

N3UH is a 2007 Homebuilt Legacy FG, serial number LS-223. It is registered to an individual in Pembroke Pines, Florida. The current certificate of registration was issued on November 16, 2017 and expires on November 30, 2027.

The FAA aircraft reference file describes the type as a single-engine piston, one Aerosport IO-375 series engine and 2 seats. Its airworthiness certificate is experimental category (amateur-built), dated August 7, 2010.

N3UH has 1 accident/incident record on file (most serious damage: substantial); details are below.

Safety record

Accident & incident history

2020-11-23 Accident · Hollywood, FL Damage: Substantial Fatal injury NTSB · ERA21LA052
Reported aircraft: Lancair Legacy FG
Probable cause: The pilot/owner s failure to properly reinstall the number 1 cylinder spark plug, which resulted in a partial loss of engine power during the initial climb. Contributing was the pilot's exceedance of the airplane s critical angle of attack during an attempted return to the airport following the partial loss of engine power, which resulted in an aerodynamic stall, loss of control, and impact with terrain.

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.