Single-engine piston

N556BW

2010 Homebuilt Rans S6 ES Coyote II

Registered No accidents on file
Built
2010
Serial
1092369
Class
Single-engine piston
Engines
Rotax 582SER
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Key Largo, FL
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Registration record

N556BW on the FAA register

Type
2010 Homebuilt Rans S6 ES Coyote II
Serial
1092369
Engines
Rotax 582SER
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Key Largo, FL
Certificate issued
2026-10-16
Airworthiness date
2010-07-08
Registration expires
2033-10-31
Airworthiness class
Experimental · amateur-built
Mode S (hex)
A715E3
Mode S (octal)
51612743
Seats (type)
2
Weight class
up to 12,499 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2033-10-31
    Registration expires (renewal due).
  • 2026-10-16
    Certificate of registration issued as N556BW to the current registrant.
  • 2010-07-08
    Airworthiness date on the current FAA record (experimental category (amateur-built)).
  • 1998-09-01
    N556BW previously assigned to a Aero Commander 500B (s/n 1625215); cancelled.
Overview

About N556BW

N556BW is a 2010 Homebuilt Rans S6 ES Coyote II, serial number 1092369. It is registered to an individual in Key Largo, Florida. The current certificate of registration was issued on October 16, 2026 and expires on October 31, 2033.

The FAA aircraft reference file describes the type as a single-engine piston, one Rotax 582SER engine and 2 seats. Its airworthiness certificate is experimental category (amateur-built), dated July 8, 2010.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N556BW. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

1998-01-10 Accident · Ennis, TX Damage: Destroyed Fatal injury NTSB · FTW98FA092
Reported aircraft: Aero Commander 500-B — a different aircraft that carried the N556BW registration before this airframe.
Probable cause: failure of the flight crew to maintain minimum control speed (Vmc) during go-around from a single-engine approach, which resulted in loss of control and collision with power lines and the ground. Related factors were: a ruptured diaphragm in the distributor valve (flow divider) of the right engine's fuel injector system, which resulted in loss of power in the right engine; inadequate maintenance; a failure to comply with Bendix Service Bulletin RS-76; the airplane's excessive gross weight and forward center-of-gravity (CG); and both pilots' lack of experience in this make and model of airplane.

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.