Single-engine piston

N82BW

2005 Homebuilt Kimball ET PITTS M12

Registered No accidents on file
Built
2005
Serial
106
Class
Single-engine piston
Engines
Ama/Expr UNKNOWN ENG
Status
Current as of October 2026
Registered owner
Helm Aviation LLC (LLC)
Based
Dover, DE
Registration record

N82BW on the FAA register

Type
2005 Homebuilt Kimball ET PITTS M12
Serial
106
Engines
Ama/Expr UNKNOWN ENG
Registered owner
Helm Aviation LLC
Dover, DE
Certificate issued
2017-01-30
Airworthiness date
2005-12-22
Registration expires
2030-01-31
Airworthiness class
Experimental · amateur-built
Mode S (hex)
AB2EB0
Mode S (octal)
52627260
Seats (type)
2
Weight class
up to 12,499 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2030-01-31
    Registration expires (renewal due).
  • 2017-01-30
    Certificate of registration issued as N82BW to the current registrant.
  • 2005-12-22
    Airworthiness date on the current FAA record (experimental category (amateur-built)).
  • 2000-11-02
    N82BW previously assigned to a Avions Mudry Et Cie Cap 10B (s/n 142); cancelled.
Overview

About N82BW

N82BW is a 2005 Homebuilt Kimball ET PITTS M12, serial number 106. The FAA register lists Helm Aviation LLC as the registrant in Dover, Delaware. The current certificate of registration was issued on January 30, 2017 and expires on January 31, 2030.

The FAA aircraft reference file describes the type as a single-engine piston, one Ama/Expr UNKNOWN ENG engine and 2 seats. Its airworthiness certificate is experimental category (amateur-built), dated December 22, 2005.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N82BW. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

2000-05-27 Accident · Bunnell, FL Damage: Destroyed Fatal injury NTSB · MIA00FA172A
Reported aircraft: Avions Mudry Et Cie Cap 10B — a different aircraft that carried the N82BW registration before this airframe.
Probable cause: A midair collision due to the failure of the wingman to maintain proper clearance between his aircraft and the lead aircraft while conducting formation aerobatics and the subsequent loss of control of both aircraft resulting in an uncontrolled descent and collision of both aircraft with the terrain. A factor in the accident was the faulty design of the belly-to-belly maneuver that required the wingman to discontinue continuous observation of the lead aircraft.

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.