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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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April 27, 2024 · Beech F35 · N3880B

Mcalpin, FL

Overview

Report Status
Probable Cause
Event Type
Accident
Date
April 27, 2024
Injury Outcomes
No injuries (2 uninjured)
Location
Mcalpin, FL
Aircraft
Beech F35 (1955)
Tail Number
N3880B
Injuries
None
Aircraft Damage
Destroyed
NTSB Number
ERA24LA197

The pilot and his passenger were preparing for a cross-country flight. After a routine preflight inspection and engine start, the pilot taxied to runway 27, which was 2,644 ft-long and comprised of turf. The grass was “mid height” and wet from the morning dew. The pilot commonly used a “hump” in the runway as a go/no-go decision point, which was about midfield. During the takeoff roll, he scanned his tablet device for speed and noted 47 knots; 52 knots was stall speed, configured. As the takeoff roll continued, he tried to “pop” the airplane off the ground and into ground effect; this attempt was unsuccessful. He realized that the airplane would not become airborne and it departed the end of the runway, collided with a berm, and spun around to a stop. A postaccident fire ensued and the pilot and passenger egressed the airplane without injuries. Despite attempts to extinguish the fire, it progressed and eventually consumed the fuselage. An inspector with the Federal Aviation Administration reported that the airplane was destroyed. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. He also reported that performing the “no go” decision at the hump in the runway would have prevented the accident.

NTSB Probable Cause

The pilot’s inadequate preflight planning and failure to abort the takeoff at the predetermined decision point.

Full Narrative

The pilot and his passenger were preparing for a cross-country flight. After a routine preflight inspection and engine start, the pilot taxied to runway 27, which was 2,644 ft-long and comprised of turf. The grass was “mid height” and wet from the morning dew. The pilot commonly used a “hump” in the runway as a go/no-go decision point, which was about midfield. During the takeoff roll, he scanned his tablet device for speed and noted 47 knots; 52 knots was stall speed, configured. As the takeoff roll continued, he tried to “pop” the airplane off the ground and into ground effect; this attempt was unsuccessful. He realized that the airplane would not become airborne and it departed the end of the runway, collided with a berm, and spun around to a stop. A postaccident fire ensued and the pilot and passenger egressed the airplane without injuries. Despite attempts to extinguish the fire, it progressed and eventually consumed the fuselage. An inspector with the Federal Aviation Administration reported that the airplane was destroyed. The pilot reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. He also reported that performing the “no go” decision at the hump in the runway would have prevented the accident.

Flight

Event TypeAccident
Event Time09:35 EDT
Nearest AirportLittle River (0.2nm W)
Runway27
Runway Length2668 ft
Runway Width50 ft
Flight Plan FiledVfif
Flight Plan ActivatedNo
Aircraft FireGrd
Aircraft ExplosionNo

Aircraft

AircraftBeech F35
Tail NumberN3880B
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · E-225-8 · Reciprocating · 225
Seats4

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 2Age 74 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind90° @ 6 kt
Visibility9 sm
CeilingNone
Temperature / Dew Point63 F
Altimeter30.22 inHg
Observation Time09:35
Weather SourceWFAC

Appendix: Source Data