Single-engine piston

N706C

2009 Cub Crafters CC18-180

Registered No accidents on file
Built
2009
Serial
CC18-0039
Class
Single-engine piston
Engines
Lycoming O-360-C4P
Status
Current as of October 2026
Registered owner
Usda Aphis Ws (Government)
Based
Cedar City, UT
Registration record

N706C on the FAA register

Type
2009 Cub Crafters CC18-180
Serial
CC18-0039
Engines
Lycoming O-360-C4P
Registered owner
Usda Aphis Ws
Cedar City, UT
Certificate issued
2009-12-04
Airworthiness date
2009-11-06
Registration expires
2029-01-31
Airworthiness class
Standard · normal
Mode S (hex)
A96B0A
Mode S (octal)
52265412
Seats (type)
2
Weight class
up to 12,499 lb
Status
Current as of October 2026
Registry history

Timeline

  • 2029-01-31
    Registration expires (renewal due).
  • 2009-12-04
    Certificate of registration issued as N706C to the current registrant.
  • 2009-11-06
    Airworthiness date on the current FAA record (standard category (normal)).
  • 2005-01-12
    N706C previously assigned to a Homebuilt Glasair II RG (s/n 307); cancelled.
  • 1995-07-05
    N706C previously assigned to a Swearingen SA-227AC Metro III (s/n AC689); cancelled.
Overview

About N706C

N706C is a 2009 Cub Crafters CC18-180, serial number CC18-0039. The FAA register lists Usda Aphis Ws as the registrant in Cedar City, Utah. The current certificate of registration was issued on December 4, 2009 and expires on January 31, 2029.

The FAA aircraft reference file describes the type as a single-engine piston, one Lycoming O-360-C4P engine and 2 seats. Its airworthiness certificate is standard category (normal), dated November 6, 2009.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N706C. 1 earlier record involves a different aircraft that carried the same N-number.

Safety record

Accident & incident history

2004-10-14 Accident · Hermiston, OR Damage: Destroyed Fatal injury NTSB · SEA05LA006
Reported aircraft: Caldwell Glasair II — a different aircraft that carried the N706C registration before this airframe.
Probable cause: The pilot's failure to maintain an airspeed above stall speed while executing a wingover maneuver at the top of a vertical climb, leading to an inadvertent spin, and the pilot's inadequate remedial action in attempting to recover from the spin. Factors include performing aerobatic maneuvers close to the terrain.

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.