Single-engine piston

N802TC

2012 Homebuilt Highlander

Registered No accidents on file
Built
2012
Serial
JA7-10-08
Class
Single-engine piston
Engines
Rotax 912S
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Royston, GA
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Registration record

N802TC on the FAA register

Type
2012 Homebuilt Highlander
Serial
JA7-10-08
Engines
Rotax 912S
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Royston, GA
Certificate issued
2016-11-28
Airworthiness date
2012-11-09
Registration expires
2029-11-30
Airworthiness class
Experimental · amateur-built
Mode S (hex)
AAEAF7
Mode S (octal)
52565367
Seats (type)
2
Weight class
up to 12,499 lb
Kit
Just Aircraft Llc HIGHLANDER
Status
Current as of October 2026
Registry history

Timeline

  • 2029-11-30
    Registration expires (renewal due).
  • 2016-11-28
    Certificate of registration issued as N802TC to the current registrant.
  • 2012-11-09
    Airworthiness date on the current FAA record (experimental category (amateur-built)).
  • 2003-11-06
    N802TC previously assigned to a Aero Commander 500B (s/n 1015-38); cancelled.
Overview

About N802TC

N802TC is a 2012 Homebuilt Highlander, serial number JA7-10-08. It is registered to an individual in Royston, Georgia. The current certificate of registration was issued on November 28, 2016 and expires on November 30, 2029.

The FAA aircraft reference file describes the type as a single-engine piston, one Rotax 912S engine and 2 seats. Its airworthiness certificate is experimental category (amateur-built), dated November 9, 2012.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N802TC. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

1997-07-08 Accident · Dallas, TX Damage: Substantial Serious injury NTSB · FTW97LA258
Reported aircraft: Aero Commander 500-B — a different aircraft that carried the N802TC registration before this airframe.
Probable cause: The pilot-in-command's failure to follow emergency procedures to reduce drag and maintain best climb airspeed. Factors were the partial loss of engine power due to the cracks in the #1 and #4 cylinders as the result of an unapproved modification of their intake ports, the separation of the magneto lead plate due to its improper installation by the pilot-in-command, the dark night light conditions and the lack of suitable terrain for the forced landing.

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.