Single-engine piston

N11TP

1992 Homebuilt SH2

Registered No accidents on file
Built
1992
Serial
1017
Class
Single-engine piston
Engines
Lycoming O&VO-360 series
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Newton, NJ
Registration record

N11TP on the FAA register

Type
1992 Homebuilt SH2
Serial
1017
Engines
Lycoming O&VO-360 series
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Newton, NJ
Certificate issued
2020-09-14
Airworthiness date
1992-06-15
Registration expires
2027-09-30
Airworthiness class
Experimental · amateur-built
Mode S (hex)
A02B91
Mode S (octal)
50025621
Seats (type)
2
Weight class
up to 12,499 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2027-09-30
    Registration expires (renewal due).
  • 2020-09-14
    Certificate of registration issued as N11TP to the current registrant.
  • 1992-06-15
    Airworthiness date on the current FAA record (experimental category (amateur-built)).
  • 1990-06-18
    N11TP previously assigned to a Beechcraft 70 (s/n LB12); cancelled.
Overview

About N11TP

N11TP is a 1992 Homebuilt SH2, serial number 1017. It is registered to an individual in Newton, New Jersey. The current certificate of registration was issued on September 14, 2020 and expires on September 30, 2027.

The FAA aircraft reference file describes the type as a single-engine piston, one Lycoming O&VO-360 series engine and 2 seats. Its airworthiness certificate is experimental category (amateur-built), dated June 15, 1992.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N11TP. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

1989-08-02 Accident · Albany, GA Damage: Destroyed Fatal injury NTSB · ATL89FA188
Reported aircraft: Beechcraft 70 — a different aircraft that carried the N11TP registration before this airframe.
Probable cause: THE FATIGUE FAILURE OF THE SUPERCHARGER INTERMEDIATE DRIVE GEAR SHAFT (GEAR TOOTH), WHICH RESULTED IN A PARTIAL LOSS OF POWER, AND THE PILOT'S INITIATION OF LIFT-OFF BEFORE REACHING VMC AIRSPEED. FACTORS RELATED TO THE ACCIDENT WERE: THE WORN INTERMEDIATE DRIVE GEAR SHAFT, THE PILOT'S OPERATION OF THE AIRCRAFT ABOVE ITS MAXIMUM CERTIFIED GROSS WEIGHT LIMIT, AND THE HIGH DENSITY ALTITUDE.

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.