20250418003719A

Accident · Substantial damage

FAA accident report · Grumman G-164A · Danevang, TX · April 18, 2025

Date
April 18, 2025 · 10:47 local
Place
Danevang, TX
Phase of flight
Cruise/Level Flight
Operating rules
Agricultural (Part 137)
Operator
NEOG
Damage
Substantial damage
Aircraft
N5416
NTSB investigation
NTSBCEN25LA160
Reported as
Grumman G-164A
Reported engine
Pratt And Whitney R-985-AN-14B
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
1,183 total

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.

Event description:

During a warmup flight, the aircraft experienced an unexpected engine failure shortly after takeoff. The pilot initiated a return to the departure airport but was unable to reach the runway, necessitating an emergency landing in a cornfield.

Landing details:

Aircraft touched down and rolled approximately 50–75 feet before spinning to the right.

Left main landing gear collapsed upon or shortly after touchdown.

The engine and propeller contacted the ground during or following the collapse.

The propeller damage and absence of ground scarring are consistent with the propeller not rotating at the time of impact (I.e., the engine was not producing power).

Aircraft structural damage:

The top wing sheared from its mounts, shifting forward during impact and making contact with the nose of the aircraft, just before the engine.

Engine inspection:

A visual inspection of the engine at the accident site revealed no immediate evidence of mechanical failure or the specific cause of the engine stoppage.

As the FAA filed it

EVENT DESCRIPTION:

DURING A WARMUP FLIGHT, THE AIRCRAFT EXPERIENCED AN UNEXPECTED ENGINE FAILURE SHORTLY AFTER TAKEOFF. THE PILOT INITIATED A RETURN TO THE DEPARTURE AIRPORT BUT WAS UNABLE TO REACH THE RUNWAY, NECESSITATING AN EMERGENCY LANDING IN A CORNFIELD.

LANDING DETAILS:

AIRCRAFT TOUCHED DOWN AND ROLLED APPROXIMATELY 50–75 FEET BEFORE SPINNING TO THE RIGHT.

LEFT MAIN LANDING GEAR COLLAPSED UPON OR SHORTLY AFTER TOUCHDOWN.

THE ENGINE AND PROPELLER CONTACTED THE GROUND DURING OR FOLLOWING THE COLLAPSE.

THE PROPELLER DAMAGE AND ABSENCE OF GROUND SCARRING ARE CONSISTENT WITH THE PROPELLER NOT ROTATING AT THE TIME OF IMPACT (I.E., THE ENGINE WAS NOT PRODUCING POWER).

AIRCRAFT STRUCTURAL DAMAGE:

THE TOP WING SHEARED FROM ITS MOUNTS, SHIFTING FORWARD DURING IMPACT AND MAKING CONTACT WITH THE NOSE OF THE AIRCRAFT, JUST BEFORE THE ENGINE.

ENGINE INSPECTION:

A VISUAL INSPECTION OF THE ENGINE AT THE ACCIDENT SITE REVEALED NO IMMEDIATE EVIDENCE OF MECHANICAL FAILURE OR THE SPECIFIC CAUSE OF THE ENGINE STOPPAGE.

NTSB investigation

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

Other reports on N5416 · 2

Matched to the same aircraft by N-number and date.