N853L

Destroyed
Fatal

DIAMOND AIRCRAFT IND INC DA 40 NGS/N: 40.NC055

Accident Details

Date
Sunday, June 6, 2021
NTSB Number
CEN21FA252
Location
Darlington, IN
Event ID
20210606103216
Coordinates
40.114244, -86.754150
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
2
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

A loss of control while practicing an aerodynamic stall, which resulted in a spin and impact with terrain.

Aircraft Information

Registration
N853L
Make
DIAMOND AIRCRAFT IND INC
Serial Number
40.NC055
Engine Type
Reciprocating
Year Built
2019
Model / ICAO
DA 40 NGDA40
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
LIFT AIRCRAFT LLC
Address
8909 PURDUE RD STE 300
Status
Deregistered
City
INDIANAPOLIS
State / Zip Code
IN 46268-3152
Country
United States

Analysis

On June 6, 2021, about 1020 eastern daylight time, a Diamond Aircraft DA 40 NG airplane, N853L, was destroyed when it was involved in an accident near Darlington, Indiana. The pilot and flight instructor were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 141 instructional flight.

A review of automatic dependent surveillance – broadcast (ADS-B) data revealed that the airplane departed and flew northwest about 4,000 ft mean sea level (msl). At the time of the accident, the flight was not in radio contact with air traffic control. A witness heard the airplane, looked up, and saw it in a “nose down, left spin” before it disappeared behind a tree line. He added that it sounded like the propeller was at a high rpm before impact.

Ground scars and the orientation of the wreckage were consistent with an impact in a slight right-wing-low, nose-down attitude. The main wreckage was oriented on a heading of about 037°. The wreckage was highly fragmented with scattered debris that extended about 75 yards. All major components of the airplane were accounted for at the accident site. A slight odor of fuel was present, along with fuel blight on vegetation along the debris path. Control continuity was established for all flight controls; separations were consistent with overload or impact damage.

A data card was removed from the flight display and the engine’s electronic engine control unit (EECU), which was damaged in the accident, was also secured for later examination. The EECU was shipped to the engine manufacturer for data download. The exam noted no preimpact abnormalities that would affect engine operation. The engine was running normally and appeared to respond to the power lever requests.

A review of the airplane’s Garmin G1000 data revealed several turns and engine power and altitude changes, consistent with airplane maneuvering. The data revealed that the airplane was about 4,000 ft msl when engine power was reduced; as the airspeed decreased, the airplane’s pitch attitude increased. The airplane’s pitch then decreased to a nose-down attitude, and the airplane made a right, spiraling turn consistent with a stall and spin entry.

The flight instructor was a graduate of the flight school’s training academy and had earned her flight certificate on March 30, 2021. She had about 329 total hours of flight experience and 44 hours as a flight instructor.

The student pilot had about 16 total hours of flight experience.

The airplane was not approved for spins. The aircraft flight manual noted the following procedure for recovery from an unintentional spin (see figure).

Figure. Flight manual excerpt

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN21FA252