Single-engine piston

N12MV

Homebuilt RV-4

Registered No accidents on file
Built
—
Serial
3671
Class
Single-engine piston
Engines
Lycoming O-360-A1D
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Morgan, UT
Registration record

N12MV on the FAA register

Type
Homebuilt RV-4
Serial
3671
Engines
Lycoming O-360-A1D
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Morgan, UT
Certificate issued
2024-10-17
Airworthiness date
2004-04-21
Registration expires
2031-10-31
Airworthiness class
Experimental · amateur-built
Mode S (hex)
A05280
Mode S (octal)
50051200
Seats (type)
2
Weight class
up to 12,499 lb
Kit
Vans Aircraft Inc RV-4
Status
Current as of October 2026
Registry history

Timeline

  • 2031-10-31
    Registration expires (renewal due).
  • 2024-10-17
    Certificate of registration issued as N12MV to the current registrant.
  • 2004-04-21
    Airworthiness date on the current FAA record (experimental category (amateur-built)).
  • 1996-06-14
    N12MV previously assigned to a Homebuilt Rebel 300 (s/n S890022); cancelled.
Overview

About N12MV

N12MV is a Homebuilt RV-4, serial number 3671. It is registered to an individual in Morgan, Utah. The current certificate of registration was issued on October 17, 2024 and expires on October 31, 2031.

The FAA aircraft reference file describes the type as a single-engine piston, one Lycoming O-360-A1D engine and 2 seats. Its airworthiness certificate is experimental category (amateur-built), dated April 21, 2004.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N12MV. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

1994-04-23 Accident · Wonderlake, IL Damage: Destroyed Fatal injury NTSB · CHI94FA140
Reported aircraft: Vavra, Martin A. Rebel 300 — a different aircraft that carried the N12MV registration before this airframe.
Probable cause: FATIGUE AND CATASTROPHIC FAILURE OF THE MAIN WING SPAR RESULTING FROM THE DESIGNER'S EXCESSIVE, UNVERIFIED ESTIMATE OF THE STRENGTH OF THE SPAR CAP MATERIAL AND THE MANUFACTURER'S FAILURE TO ATTAIN THE SPECIFIED STRENGTH DURING THE PRODUCTION PROCESS.

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.