Single-engine piston

N313RS

1999 Homebuilt Minimax RS

Registered No accidents on file
Built
1999
Serial
P-701
Class
Single-engine piston
Engines
Rotax SEE BOMBADIER
Status
Current as of October 2026
Registered owner
Individual · sign in to see
Based
Snow Hill, NC
Registration record

N313RS on the FAA register

Type
1999 Homebuilt Minimax RS
Serial
P-701
Engines
Rotax SEE BOMBADIER
Registered owner
Individual — the name of an individual registrant is shown to signed-in users. Sign in
Snow Hill, NC
Certificate issued
2001-06-08
Airworthiness date
2001-06-26
Registration expires
2027-07-31
Airworthiness class
Experimental · amateur-built
Mode S (hex)
A3537E
Mode S (octal)
50651576
Seats (type)
1
Weight class
up to 12,499 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2027-07-31
    Registration expires (renewal due).
  • 2001-06-26
    Airworthiness date on the current FAA record (experimental category (amateur-built)).
  • 2001-06-08
    Certificate of registration issued as N313RS to the current registrant.
  • 1999
    Manufactured (1999).
  • 1997-03-10
    N313RS previously assigned to a Homebuilt C-118 (s/n 533292); cancelled.
Overview

About N313RS

N313RS is a 1999 Homebuilt Minimax RS, serial number P-701. It is registered to an individual in Snow Hill, North Carolina. The current certificate of registration was issued on June 8, 2001 and expires on July 31, 2027.

The FAA aircraft reference file describes the type as a single-engine piston, one Rotax SEE BOMBADIER engine and 1 seats. Its airworthiness certificate is experimental category (amateur-built), dated June 26, 2001.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N313RS. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

1996-07-20 Accident · Russian Mission, AK Damage: Destroyed Fatal injury NTSB · ANC96FA102
Reported aircraft: Douglas DC-6A — a different aircraft that carried the N313RS registration before this airframe.
Probable cause: fatigue failure of the master connecting rod, which originated from corrosion pitting, subsequently compromised the engine crankcase, and resulted in a fire; and failure of the flight crew to follow emergency procedures by pulling the fire handle before feathering the propeller, which diminished the effectiveness of the fire suppression system.

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.