N927DS

Substantial
None

CIRRUS DESIGN CORP SR22S/N: 0497

Accident Details

Date
Wednesday, March 23, 2016
NTSB Number
CEN16LA143
Location
Alexandria, LA
Event ID
20160406X31404
Coordinates
31.480556, -92.731666
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The partial loss of engine power for reasons that could not be determined based on the available information.

Aircraft Information

Registration
N927DS
Make
CIRRUS DESIGN CORP
Serial Number
0497
Engine Type
Reciprocating
Year Built
2003
Model / ICAO
SR22SR22
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
RUCKS AVIATION LLC
Address
C/O CLINTON M RUCKS
2240 NW 144TH DR
Status
Deregistered
City
OKEECHOBEE
State / Zip Code
FL 34972-0926
Country
United States

Analysis

On March 23, 2016, about 1600 central daylight time, a Cirrus SR22 airplane, N927DS, impacted terrain following the deployment of the ballistic recovery system (BRS) parachute near Alexandria International Airport (AEX), Alexandria, Louisiana. The pilot and flight instructor were not injured. The airplane was registered to Rucks Aviation, LLC and operated by a private individual under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight.

According to the pilot, he and the flight instructor departed Dallas Executive Airport, Dallas, Texas, and were en route to AEX. The flight was uneventful until the descent into AEX. During the descent, he reduced the engine throttle and noticed some "shaking from the engine." After some brief troubleshooting, he realized the engine would not make sufficient power for a landing at AEX. Due to the unsuitable terrain for an off-airport landing, the pilot elected to activate the BRS. The airplane descended to the ground under the parachute canopy sustained substantial damage to the fuselage during the impact.

Seven gallons of fuel were drained from the right wing fuel tank, and 23 gallons of fuel were drained from the left wing fuel tank. The fuel selector was found in the right fuel tank position.

The engine was placed in a manufacturer's test cell for a functional test. According to the manufacturer, the engine experienced a normal start on the first attempt without hesitation or stumbling in observed RPM. The engine was tested at various power settings for about 25 minutes including rapid throttle applications. Throughout the test phase, the engine accelerated normally without any hesitation, stumbling, or interruption in power and demonstrated the ability to produced rated horsepower. Postaccident examination revealed no airframe or engine anomalies that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN16LA143