Flight Tracker
N473DA
2007 CIRRUS DESIGN CORP SR20
Fixed wing single engine · Reciprocating · Standard
1 NTSB record for this tail number, including destroyed damage, 14 fatal injuries. See the full record below.

Registration

Registered Owner
AEROSIM ACADEMY INC
Registrant Type
Corporation
Location
SANFORD, FL
Status
Valid
Certificate Issued
Dec 21, 2016
Airworthiness Date
Jun 19, 2007
Expires
Dec 31, 2029
Approved Operations
Normal

Airframe

Manufacturer
CIRRUS DESIGN CORP
Model
SR20
Year
2007
Serial Number
1798
Seats
4
Engines
1
Max Weight
Up to 12,499 lb
Cruise Speed
-
Type Certificate
-

Powerplant

Engine Manufacturer
CONT MOTOR
Engine Model
IO-360-ES
Type
Reciprocating
Power
210 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)
A5CC8B
Mode S Code (Octal)
51346213

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
- - Jul 27, 1989

NTSB Accident & Incident Record

Aug 31, 1988 Accident Destroyed DALLAS/FT WORTH, TX
Injuries14 fatal, 26 serious, 50 minor
Phase of Flight-
ConditionsVMC
OperationFAR 121
Probable Cause

(1) THE CAPTAIN AND FIRST OFFICER'S INADEQUATE COCKPIT DISCIPLINE WHICH RESULTED IN THE FLIGHTCREW'S ATTEMPT TO TAKEOFF WITHOUT THE WING FLAPS AND SLATS PROPERLY CONFIGURED; AND (2) THE FAILURE OF THE TAKEOFF CONFIGURATION WARNING SYSTEM TO ALERT THE CREW THAT THE AIRPLANE WAS NOT PROPERLY CONFIGURED FOR THE TAKEOFF. CONTRIBUTING TO THE ACCIDENT WAS DELTA'S SLOW IMPLEMENTATION OF NECESSARY MODIFICATIONS TO ITS OPERATING PROCEDURES, MANUAL'S, CHECKLISTS, TRAINING, AND CREW CHECKING PROGRAMS WHICH WERE NECESSITATED BY SIGNIFICANT CHANGES IN THE AIRLINE FOLLOWING RAPID GROWTH AND MERGER. ALSO CONTRIBUTING TO THE ACCIDENT WAS THE LACK OF SUFFICIENTLY AGGRESSIVE ACTION BY THE FAA TO HAVE KNOWN DEFICIENCIES CORRECTED BY DELTA AND THE LACK OF SUFFICIENT ACCOUNTABILITY WITHIN THE FAA'S AIR CARRIER INSPECTION PROCESS.

NTSB DCA88MA072