Single-engine piston

N721PT

2016 Homebuilt RV-7A

Registered No accidents on file
Built
2016
Serial
72112
Class
Single-engine piston
Engines
Lycoming YIO-360-M1B
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Bellingham, WA
Registration record

N721PT on the FAA register

Type
2016 Homebuilt RV-7A
Serial
72112
Engines
Lycoming YIO-360-M1B
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Bellingham, WA
Certificate issued
2023-02-19
Airworthiness date
2016-06-18
Registration expires
2030-02-28
Airworthiness class
Experimental · amateur-built
Mode S (hex)
A9A89A
Mode S (octal)
52324232
Seats (type)
2
Weight class
up to 12,499 lb
Kit
Vans Aircraft Inc RV7A
Status
Current as of October 2026
Registry history

Timeline

  • 2030-02-28
    Registration expires (renewal due).
  • 2023-02-19
    Certificate of registration issued as N721PT to the current registrant.
  • 2016-06-18
    Airworthiness date on the current FAA record (experimental category (amateur-built)).
  • 2005-11-29
    N721PT previously assigned to a Homebuilt Zodiac CH 601 HDS (s/n 63423); cancelled.
Overview

About N721PT

N721PT is a 2016 Homebuilt RV-7A, serial number 72112. It is registered to an individual in Bellingham, Washington. The current certificate of registration was issued on February 19, 2023 and expires on February 28, 2030.

The FAA aircraft reference file describes the type as a single-engine piston, one Lycoming YIO-360-M1B engine and 2 seats. Its airworthiness certificate is experimental category (amateur-built), dated June 18, 2016.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N721PT. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

2003-06-16 Accident · Thomson, GA Damage: Substantial NTSB · ATL03LA106
Reported aircraft: Polstra Zodiac CH 601 HDS — a different aircraft that carried the N721PT registration before this airframe.
Probable cause: The total loss of engine power due to the fatigue fracture of the No. 3 cylinder intake valve, which resulted in a forced landing to rough terrain and subsequent collision with small trees and a tree stump.

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.