Flight Tracker
N2417T
2003 SADLER TERRY RANS S-7 COURIER
Fixed wing single engine · Reciprocating · Experimental
2 NTSB records for this tail number, including substantial damage. See the full record below.

Registration

Registered Owner
MARMIC LLC
Registrant Type
LLC
Location
RUSSELL, KS
Status
Valid
Certificate Issued
Jul 13, 2023
Airworthiness Date
Aug 19, 2003
Expires
Jul 31, 2030
Approved Operations
Amateur Built

Airframe

Manufacturer
SADLER TERRY
Model
RANS S-7 COURIER
Year
2003
Serial Number
0496185
Seats
2
Engines
1
Max Weight
Up to 12,499 lb
Cruise Speed
-
Type Certificate
-
Kit Manufacturer
RANS INC
Kit Model
S-7 COURIER

Powerplant

Engine Manufacturer
ROTAX
Engine Model
SEE BOMBADIER
Type
Reciprocating
Power
-

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)
A23715
Mode S Code (Octal)
50433425

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: 1 prior registration

RegistrantLocationCancelled
MATARESE WILLIAM LOUIS HOBE SOUND, FL Nov 30, 2000

NTSB Accident & Incident Record

Oct 1, 2011 Accident Substantial Riley, KS
Injuries1 serious, 1 minor
Phase of Flight-
ConditionsVMC
OperationFAR 091
Probable Cause

A total loss of engine power during takeoff due to fuel starvation as a result of the pilot’s inadequate preflight inspection and failure to ensure that the fuel shutoff valve was turned on before departure.

NTSB CEN12CA003
Jan 24, 1997 Accident Substantial INDIANTOWN, FL
Injuries2 serious
Phase of Flight-
ConditionsVMC
OperationFAR 091
Probable Cause

Total loss of engine power due to undetermined reasons. Contributing to the accident was the unsuitable terrain encountered during the forced landing. Findings of the follow-up investigation were 1) The airplane had not been operated and no annual inspections were performed between the effective date of Airworthiness Directive 93-16-15 and the date of the last annual inspection (May 1996), 2) AD 93-16-15 requiring replacement of the installed fuel pump drive coupling was not complied with by the IA at the last annual inspection and no entry was made in the maintenance records indicating compliance required within 30 hours time in service, 3) the pilot unknowingly operated the airplane approximately 8 hours past the 30 hour compliance time specified by the AD, and 4) the reason for the AD (mechanical damage to the fuel pump drive coupling), was not present in the accident fuel pump drive coupling.

NTSB MIA97LA072