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Aircraft record

N455JS1984 Shaffer John Thomas KR-2

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:3 NTSB accidents (substantial damage at worst, latest Sep 2026)No ADs since 1998 matched

Registration
Valid
expires Nov 30, 2027
Based in
Fremont, OH
owner city / state
Engine
CONVERSION · 36 hp
Volkswagen
Owners
1
since 1984
NTSB events
3
substantial, 2026
ADs may apply
0
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Individual owner
City, state
Fremont, OH
Certificate issued
Jul 3, 1984
Expires
Nov 30, 2027
Airworthiness
Experimental · Amateur Built
Airworthiness date
Feb 27, 1985

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Shaffer John Thomas
Model
KR-2
Year
1984
Serial number
8009
Aircraft type
Fixed wing single engine
Category
Land
Certification
Not Type Certificated
Seats
2
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A58588

Engine

Make and model
Volkswagen Conversion
Type
Reciprocating
Power
36 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 1984 – nowIndividual ownerFremont, OH · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (3)

Accident · substantial damage

Feb 24, 2008 · Fremont, OH

The loss of engine power for undetermined reasons during takeoff.

Damage
Substantial
Injuries
None
Report
CHI08CA088

From NTSB records; matched by N-number.Read NTSB report (search CAROL for CHI08CA088)

Accident · substantial damage

Mar 15, 1986 · Mobile, AL

THE PILOT LOST CONTROL OF THE AIRCRAFT DURING CRUISE FLIGHT WHILE ATTEMPTING TO CLOSE THE COCKPIT CANOPY WHICH INADVERTENTLY UNLATCHED. THE AIRCRAFT ENTERED A SPIN AND THE PILOT WAS UNABLE TO RECOVER PRIOR TO GROUND IMPACT. THE AIRCRAFT WAS AN EXPERIMENTAL HOMEBUILT WHICH WAS ASSEMBLED BY THE PILOT. THE CANOPY LATCH WAS A MODIFICATION TO THE ORIGINAL PLANS WHICH WAS DESIGNED AND CONSTRUCTED BY…

Damage
Substantial
Injuries
Serious
Report
ATL86LA094

From NTSB records; matched by N-number.Read NTSB report (search CAROL for ATL86LA094)

ADs published since 1998 that may apply (0)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

No ADs published since 1998 matched this airframe or engine model.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (0)

No Service Difficulty Reports found for this airframe since 1995.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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