Flight Tracker
N339T
1953 PIPER PA-18 105
Fixed wing single engine · Reciprocating · Restricted
4 NTSB records for this tail number, including substantial damage. See the full record below.

Registration

Registered Owner
LEROUX TODD C
Registrant Type
Individual
Location
PALMER, AK
Status
Valid
Certificate Issued
Feb 1, 2025
Airworthiness Date
Sep 19, 1990
Expires
Feb 29, 2032
Approved Operations
Other

Airframe

Manufacturer
PIPER
Model
PA-18 105
Year
1953
Serial Number
18-2453
Seats
2
Engines
1
Max Weight
Up to 12,499 lb
Cruise Speed
97 kt
Type Certificate
-

Powerplant

Engine Manufacturer
LYCOMING
Engine Model
0-320 SERIES
Type
Reciprocating
Power
180 hp

Live Flight Status

Checking live traffic…

Coverage depends on ground receiver reception and is not a complete picture of traffic.

Transponder & Tracking

Mode S Code (Hex)
A3B8E7
Mode S Code (Octal)
50734347

The hex code is the aircraft's ICAO 24-bit address, broadcast by its ADS-B transponder. It is the key used to match live position reports to this registration.

NTSB Accident & Incident Record

Apr 14, 2003 Accident Substantial Cantwell, AK
InjuriesNone
Phase of Flight-
ConditionsVMC
OperationFAR 091
Probable Cause

The pilot's selection of an unsuitable landing area in deep snow, which resulted in the nose over of the airplane on touchdown. A factor associated with the accident was a snow-covered airstrip.

NTSB ANC03LA041
Aug 9, 1997 Accident Substantial CIRCLE, AK
InjuriesNone
Phase of Flight-
ConditionsVMC
OperationFAR 091
Probable Cause

The inadequate visual lookout by the pilot, and his selection of a landing area with high vegetation in the landing path. Factors which contributed to the accident were fatigue and the high vegatation.

NTSB ANC97LA118
Aug 4, 1995 Accident Substantial CIRCLE, AK
Injuries2 minor
Phase of Flight-
ConditionsVMC
OperationFAR 091
Probable Cause

THE PILOT'S PREMATURE LIFTOFF DURING TAKEOFF.

NTSB ANC95LA128
Sep 11, 1989 Accident Substantial CIRCLE CITY, AK
InjuriesNone
Phase of Flight-
ConditionsVMC
OperationFAR 091
Probable Cause

PILOT FAILED TO MAINTAIN DIRECTIONAL DURING THE LANDING ROLL.

NTSB ANC89LA166