Flight Tracker
N612AZ
2025 ROLLING ACRES LLC SLING TSI
Fixed wing single engine · Reciprocating · Experimental
1 NTSB record for this tail number, including destroyed damage, 9 fatal injuries. See the full record below.

Registration

Registered Owner
ROLLING ACRES LLC
Registrant Type
LLC
Location
CASEVILLE, MI
Status
Valid
Certificate Issued
Sep 13, 2024
Airworthiness Date
Apr 29, 2025
Expires
Sep 30, 2031
Approved Operations
Amateur Built

Airframe

Manufacturer
ROLLING ACRES LLC
Model
SLING TSI
Year
2025
Serial Number
545SK
Seats
4
Engines
1
Max Weight
Up to 12,499 lb
Cruise Speed
-
Type Certificate
-
Kit Manufacturer
AIRPLANE FACTORY INC
Kit Model
SLING TSI

Powerplant

Engine Manufacturer
ROTAX
Engine Model
915 ISC3 A
Type
Reciprocating
Power
141 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)
A7F644
Mode S Code (Octal)
51773104

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
CARSON HELICOPTERS INC GRANTS PASS, OR May 23, 2017

NTSB Accident & Incident Record

Aug 6, 2008 Accident Destroyed Weaverville, CA
Injuries9 fatal, 4 serious
Phase of Flight-
ConditionsVMC
OperationFAR PUBU
Probable Cause

The following actions by Carson Helicopters: 1) the intentional understatement of the helicopter's empty weight, 2) the alteration of the power available chart to exaggerate the helicopter's lift capability, and 3) the practice of using unapproved above-minimum specification torque in performance calculations that, collectively, resulted in the pilots relying on performance calculations that significantly overestimated the helicopter's load-carrying capacity and did not provide an adequate performance margin for a successful takeoff; and insufficient oversight by the U.S. Forest Service and the Federal Aviation Administration. Contributing to the accident was the failure of the flight crewmembers to address the fact that the helicopter had approached its maximum performance capability on their two prior departures from the accident site because they were accustomed to operating at the limit of the helicopter’s performance. Contributing to the fatalities were the immediate, intense fire that resulted from the spillage of fuel upon impact from the fuel tanks that were not crash resistant, the separation from the floor of the cabin seats that were not crash resistant, and the use of an inappropriate release mechanism on the cabin seat restraints.

NTSB LAX08PA259