Flight Tracker
N5157T
2003 POWRACHUTE PEGASUS
Powered Parachute · 4 Cycle · Experimental
2 NTSB records for this tail number, including destroyed damage, 4 fatal injuries. See the full record below.

Registration

Registered Owner
MERRILL CHESTER R
Registrant Type
Individual
Location
BENSON, AZ
Status
Valid
Certificate Issued
May 21, 2007
Airworthiness Date
Sep 8, 2007
Expires
Apr 30, 2030
Approved Operations
Light Sport / Reg. prior to 01/31/08

Airframe

Manufacturer
POWRACHUTE
Model
PEGASUS
Year
2003
Serial Number
A127PEG
Seats
2
Engines
1
Max Weight
Up to 12,499 lb
Cruise Speed
-
Type Certificate
-

Powerplant

Engine Manufacturer
ROTAX
Engine Model
582UL
Type
4 Cycle
Power
65 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)
A67761
Mode S Code (Octal)
51473541

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.

Ownership History: 2 prior registrations

RegistrantLocationCancelled
AIR SERVICE CARAVAN CO INC NEW BEDFORD, MA Mar 19, 1974
PROPCO INC MOBILE, AL Jan 11, 2005

NTSB Accident & Incident Record

Sep 23, 2004 Accident Destroyed Milton, FL
Injuries4 fatal
Phase of Flight-
ConditionsVMC
OperationFAR 091
Probable Cause

The pilots operation of the airplane with known deficiencies in the equipment based on witness statements describing an excessive rpm drop and rough running engine after starting, during the engine run-up, and after becoming airborne, his failure to abort the takeoff after an excessive takeoff roll, and his failure to maintain airspeed resulting in an inadvertent stall, uncontrolled descent, and in-flight collision with terrain. A factor in the accident was the loss of engine power due to undetermined reasons.

NTSB MIA04FA128
Dec 9, 1990 Accident Substantial ORLANDO, FL
InjuriesNone
Phase of Flight-
ConditionsVMC
OperationFAR 091
Probable Cause

FAILURE OF THE PILOT TO MAINTAIN DIRECTIONAL CONTROL DURING THE LANDING ROLL.

NTSB MIA91LA041