Piper PA28 N4890L

Summary

On 13 April 2019 at about 05:15 local time, a Piper PA28 registered N4890L was involved in an accident near Lake, Mississippi, United States. One person was on board and one died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

13 April 2019 at 05:15

Classification

Accident

Location

Lake, Mississippi, United States

Coordinates

32.3402, -89.3645

Aircraft

Piper PA28

Registration

N4890L

Category

Airplane

Year built

1967

Engines

1

Operator

Not recorded

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

Picayune → Ackerman

Aircraft damage

Destroyed

Weather

IMC

Light

Night

NTSB number

CEN19FA120

1 person died.

The noninstrument-rated pilot’s loss of control while flying in dark night instrument meteorological weather conditions with convective activity, which resulted in the airplane exceeding its structural limitations and experiencing an in-flight breakup. Contributing to the accident was the pilot’s lack of preflight planning and impairment from drugs.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The noninstrument-rated pilot was operating the airplane on a cross-country flight in dark night instrument meteorological conditions. There was no record of the pilot obtaining a weather briefing, filing a flight plan, or making any radio transmissions. Primary radar data and weather data showed the airplane entering an area of thunderstorms and convective activity. The radar track ended when the airplane was about 8,400 ft mean sea level. A resident near the accident area heard the sound of an airplane and a loud “bang” and noted strong wind, rain, and thunderstorms at the time. Examination of the main wreckage revealed that the airplane impacted the ground in a high-speed, near-vertical condition, and the accident site encompassed a linear area about 1,500 ft long. The main wreckage was destroyed by impact forces, and the engine and propeller assembly were buried in a 4-ft-deep crater. The left aileron, outboard sections of the left and right wings, and the left and right horizontal stabilizers were located about 1,500, 1,000, and 900 ft from the main wreckage, respectively. Fractured areas of the left and right wings and the horizontal stabilizers were consistent with overload separation before ground impact. The debris path and separated sections of the wings and empennage were consistent with an in-flight breakup. Examinations of the engine and airframe did not reveal evidence of any pre-existing anomalies that would have precluded normal operation. Flight control continuity was established, and the propeller blades showed evidence of rotation at impact. The pilot did not have an instrument rating, and his instrument proficiency could not be verified. Based on toxicological and operational evidence, it is likely that impairing effects from the pilot’s use of methamphetamine contributed to the accident. Whether effects from his use of buprenorphine also contributed to the accident cannot be determined.

Quoted verbatim from the NTSB record.