CEN21FA252

NTSB accident investigation · Diamond Aircraft Ind DA 40 NG · Darlington, IN · June 6, 2021

Accident · FatalClass 3 · FieldFinal report
Date
June 6, 2021, 10:20 local (14:20 UTC)
Place
Darlington, IN
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N853LDiamond Aircraft Ind DA 40 NG
Defining event
Maneuvering: Aerodynamic stall/spin
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 3
NTSB office
Central Region
Parties
Austrian Federal Safety Investigative authority, Lift Training Academy, FAA FSDO, TSB, Diamond Aircraft
FAA report
20210606003809A
Case key
103216

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

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

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The flight instructor and student pilot were conducting a training flight. automatic dependent surveillance – broadcast (ADS-B) and onboard data revealed heading, engine power, and altitude changes consistent with maneuvering. Just before the accident, the airplane entered a power-off stall from an altitude of about 4,000 ft mean sea level (msl). The right wing dropped, the pitch attitude decreased, and the airplane entered a descent consistent with a spin. Ground scars and the orientation of the wreckage were consistent with an impact with terrain in a slight right-wing-low, nose-down attitude. The wreckage was highly fragmented with scattered debris that extended for about 75 yards. There were no mechanical malfunctions or anomalies that would have precluded normal operation of the airplane. Review of engine data indicated nominal engine performance before the accident. The airplane was not approved for spin maneuvers; however, the airplane’s flight manual provided a recovery procedure in the event of an unintentional spin. The circumstances of the accident are consistent with an inadvertent spin and loss of control while practicing an aerodynamic stall. Because the airplane was not approved for intentional spins, it is unlikely that the flight instructor had ever experienced a spin in the accident airplane make/model and was therefore likely unfamiliar with its spin and recovery characteristics.

Factual narrative

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

Aircraft

Registration
N853L
Reported as
Diamond Aircraft Ind DA 40 NG
Category
Airplane
Serial number
40.NC055
Built
2019
Airframe hours
1,432.5
Engine
Austro E4-A, reciprocating
Damage
Destroyed
Flight
Instructional · Part 91
Operator
Lift Training Academy
Registered owner
Lift Aircraft LLC
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 25, 2021
Departed
KIND · Indianapolis, IN
Airport
N/A
Equipment
Electronic primary flight display, Electronic multifunction display, ADS-B

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
28
Injuries
Fatal
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Without waivers/limitations
Seat
Right
Flight hours
329 total · 312.2 in this make and model · 251.9 as pilot in command · 79.3 in the last 90 days · 51.6 in the last 30 days · 1.7 in the last 24 hours
Role
Student pilot
Age
21
Injuries
Fatal
Medical
Class 1, With waivers/limitations
Seat
Left
Flight hours
16 total · 16 in this make and model · 16 in the last 90 days · 16 in the last 30 days · 1.7 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 10 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
77 °F, dew point 63 °F
Altimeter
30.05 inHg
Observed at
KCFJ
METAR
KCFJ 061415Z AUTO 18010KT 10SM SCT045 SCT090 24/17 A3005 RMK AO2 T0238017

Docket · 14

The files NTSB released with the investigation on April 28, 2022, on NTSB’s docket system: statements, records, photos and specialists’ reports. 107 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.