Flight Tracker
N216PB
2025 CIRRUS DESIGN CORP SR22
Fixed wing single engine · Reciprocating · Standard
2 NTSB records for this tail number, including destroyed damage, 4 fatal injuries. See the full record below.

Registration

Registered Owner
DIVINE AIR LLC
Registrant Type
LLC
Location
BROOKSHIRE, TX
Status
Valid
Certificate Issued
Nov 3, 2025
Airworthiness Date
Sep 12, 2025
Expires
Nov 30, 2032
Approved Operations
Normal

Airframe

Manufacturer
CIRRUS DESIGN CORP
Model
SR22
Year
2025
Serial Number
10924
Seats
4
Engines
1
Max Weight
Up to 12,499 lb
Cruise Speed
-
Type Certificate
A00009CH

Powerplant

Engine Manufacturer
CONT MOTOR
Engine Model
IO-550-N
Type
Reciprocating
Power
310 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)
A1D113
Mode S Code (Octal)
50350423

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
BERNDT SCOTT J CHICO, CA Jul 2, 2013

NTSB Accident & Incident Record

Apr 28, 2000 Accident Destroyed CHESTER, CA
Injuries4 fatal
Phase of Flight-
ConditionsVMC
OperationFAR 091
Probable Cause

The pilot's encounter with a wind shear at low altitude, which resulted in a loss of control and a stall/spin. Factors in the accident were the high density altitude and the pilot's lack of experience and training in high density altitude operations. The pilot's decision to takeoff downwind, while reasonable given the nature of the obstacles and terrain on the other runways, set up a situation where decreased safety margins existed and is considered a factor.

NTSB LAX00FA178
Jun 9, 1990 Accident Substantial REDDING, CA
InjuriesNone
Phase of Flight-
ConditionsVMC
OperationFAR 091
Probable Cause

THE FAILURE OF THE PILOT IN COMMAND TO MAINTAIN DIRECTION CONTROL. FACTORS IN THE ACCIDENT WERE THE PILOT IN COMMAND'S PREMATURE ROTATION DURING THE TAKEOFF AND THE FAILURE TO TAKE THE NECESSARY REMEDIAL ACTION.

NTSB LAX90LA216