20240422004689A

Accident · Substantial damage

FAA accident report · Beech B24R · Lumberton, NJ · April 22, 2024

Date
April 22, 2024 · 17:15 local
Place
Lumberton, NJ
Airport
Flying W
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N53EM
NTSB investigation
NTSBERA24LA190
Reported as
Beech B24R
Reported engine
Lycoming I0360 series
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Private pilot
Pilot’s flight hours
267 total19 in this make and model

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On April 22, 2024, the pilot of a Beech aircraft corporation B24R was observed taking off at a slow rate of speed with popping and sputtering sounds eminating from the aircraft. The aircraft was observed climbing at a low angle and attempting a left bank, then impacted the ground in a field approximately 1500 feet north of the departure end of the runway. The aircraft incurred substantial damage to the landing gear, fuselage, and primary flight control surafces, and the pilot was transported to the hospitalized with injuries.

Post-accident investigation of the aircraft revealed low #2 cylinder compression (intake valve), with evidence of corrosion on the #2 cylinder wall and left magneto impulse coupling.

This report may be amended if further information is received.

As the FAA filed it

ON APRIL 22, 2024, THE PILOT OF A BEECH AIRCRAFT CORPORATION B24R WAS OBSERVED TAKING OFF AT A SLOW RATE OF SPEED WITH POPPING AND SPUTTERING SOUNDS EMINATING FROM THE AIRCRAFT. THE AIRCRAFT WAS OBSERVED CLIMBING AT A LOW ANGLE AND ATTEMPTING A LEFT BANK, THEN IMPACTED THE GROUND IN A FIELD APPROXIMATELY 1500 FEET NORTH OF THE DEPARTURE END OF THE RUNWAY. THE AIRCRAFT INCURRED SUBSTANTIAL DAMAGE TO THE LANDING GEAR, FUSELAGE, AND PRIMARY FLIGHT CONTROL SURAFCES, AND THE PILOT WAS TRANSPORTED TO THE HOSPITALIZED WITH INJURIES.

POST-ACCIDENT INVESTIGATION OF THE AIRCRAFT REVEALED LOW #2 CYLINDER COMPRESSION (INTAKE VALVE), WITH EVIDENCE OF CORROSION ON THE #2 CYLINDER WALL AND LEFT MAGNETO IMPULSE COUPLING.

THIS REPORT MAY BE AMENDED IF FURTHER INFORMATION IS RECEIVED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.