Weight-shift trike

N5074J

2002 Homebuilt Jet Star II

Registered No accidents on file
Built
2002
Serial
070702
Class
Weight-shift trike
Engines
Rotax 503 DCDI
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Imler, PA
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Registration record

N5074J on the FAA register

Type
2002 Homebuilt Jet Star II
Serial
070702
Engines
Rotax 503 DCDI
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Imler, PA
Certificate issued
2022-11-09
Airworthiness date
2007-09-26
Registration expires
2029-11-30
Airworthiness class
Experimental · light-sport
Mode S (hex)
A656DE
Mode S (octal)
51453336
Seats (type)
2
Weight class
up to 12,499 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2029-11-30
    Registration expires (renewal due).
  • 2022-11-09
    Certificate of registration issued as N5074J to the current registrant.
  • 2007-09-26
    Airworthiness date on the current FAA record (experimental category (light-sport)).
  • 2002
    Manufactured (2002).
  • 1994-02-04
    N5074J previously assigned to a Cessna 310R (s/n 310R0194); cancelled.
Overview

About N5074J

N5074J is a 2002 Homebuilt Jet Star II, serial number 070702. It is registered to an individual in Imler, Pennsylvania. The current certificate of registration was issued on November 9, 2022 and expires on November 30, 2029.

The FAA aircraft reference file describes the type as a weight-shift trike, one Rotax 503 DCDI engine and 2 seats. Its airworthiness certificate is experimental category (light-sport), dated September 26, 2007.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N5074J. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

1992-10-28 Accident · Saipan Damage: Destroyed Fatal injury NTSB · LAX93LA019
Reported aircraft: Cessna 310R — a different aircraft that carried the N5074J registration before this airframe.
Probable cause: THE PILOT NOT FOLLOWING WAKE TURBULENCE (VOTEX) AVOIDANCE PROCEDURES, WHICH ARE DETAILED IN FAA PUBLICATIONS, RESULTING IN THE AIRPLANE ENCOUNTERING WAKE TURBULENCE. FACTORS IN THIS ACCIDENT WERE: 1) THE PILOT'S INABILITY TO CONTROL THE AIRPLANE AFTER ENCOUNTERING WAKE TURBULENCE, AND 2) INADEQUATE ALTITUDE TO EFFECT A RECOVERY FROM THE UNCONTROLLED DESCENT.

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.