Single-engine piston

N59412

1998 Homebuilt Velocity Fge

Registered No accidents on file
Built
1998
Serial
DMO365
Class
Single-engine piston
Engines
Ama/Expr UNKNOWN ENG
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Clinton, TN
Registration record

N59412 on the FAA register

Type
1998 Homebuilt Velocity Fge
Serial
DMO365
Engines
Ama/Expr UNKNOWN ENG
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Clinton, TN
Certificate issued
2013-01-29
Airworthiness date
2004-12-16
Registration expires
2029-01-31
Airworthiness class
Experimental · amateur-built
Mode S (hex)
A7AED9
Mode S (octal)
51727331
Seats (type)
2
Weight class
up to 12,499 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2029-01-31
    Registration expires (renewal due).
  • 2013-01-29
    Certificate of registration issued as N59412 to the current registrant.
  • 2004-12-16
    Airworthiness date on the current FAA record (experimental category (amateur-built)).
  • 1998
    Manufactured (1998).
  • 1965-05-22
    N59412 previously assigned to a Cessna T-50 (s/n 5209); cancelled.
Overview

About N59412

N59412 is a 1998 Homebuilt Velocity Fge, serial number DMO365. It is registered to an individual in Clinton, Tennessee. The current certificate of registration was issued on January 29, 2013 and expires on January 31, 2029.

The FAA aircraft reference file describes the type as a single-engine piston, one Ama/Expr UNKNOWN ENG engine and 2 seats. Its airworthiness certificate is experimental category (amateur-built), dated December 16, 2004.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N59412. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

1994-04-02 Incident · Orlando, FL Damage: Minor NTSB · MIA94IA110
Reported aircraft: Boeing 727-243 — a different aircraft that carried the N59412 registration before this airframe.
Probable cause: The total failure of the left main landing gear door actuator fitting due to fatigue cracking in the fitting. Contributing to the accident was inadequate written inspection procedures by the aircraft manufacturer.

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.