20260502010509I

Incident · Minor damage

FAA incident report · Cessna T210N · Punta Gorda, FL · May 2, 2026

Date
May 2, 2026 · 17:12 local
Place
Punta Gorda, FL
Airport
Punta Gorda
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N4951Y
Reported as
Cessna T210N
Reported engine
Continental TSIO-520 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
974 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.

Pilot on arrival into Punta Gorda (pgd), obtained current weather information and planned the approach with consideration for reported wind conditions.

The approach was stabilized on final. Touchdown initially occurred on the main landing gear with slight aft elevator input as the nose was being lowered. Immediately after touchdown, a gust of wind caused the aircraft to become airborne again, reaching an estimated 15-20 feet AGL. Upon becoming airborne, pilot applied full power to initiate a go-around.

Before full power was achieved and a positive climb established, the aircraft descended back to the runway.

The aircraft contacted the runway nose gear first, followed by the main landing gear. Directional control was maintained throughout the event.

The engine continued to operate normally following the impact. Pilot elected to continue the landing rollout, exited the runway normally,

And taxied to the FBO where the aircraft was shut down.

During post-flight inspection, deformation of the propeller blades was observed, consistent with a propeller strike. Further inspection revealed collapse of the nose landing gear strut, consistent with a firm nose gear contact.

As the FAA filed it

PILOT ON ARRIVAL INTO PUNTA GORDA (PGD), OBTAINED CURRENT WEATHER INFORMATION AND PLANNED THE APPROACH WITH CONSIDERATION FOR REPORTED WIND CONDITIONS.

THE APPROACH WAS STABILIZED ON FINAL. TOUCHDOWN INITIALLY OCCURRED ON THE MAIN LANDING GEAR WITH SLIGHT AFT ELEVATOR INPUT AS THE NOSE WAS BEING LOWERED. IMMEDIATELY AFTER TOUCHDOWN, A GUST OF WIND CAUSED THE AIRCRAFT TO BECOME AIRBORNE AGAIN, REACHING AN ESTIMATED 15-20 FEET AGL. UPON BECOMING AIRBORNE, PILOT APPLIED FULL POWER TO INITIATE A GO-AROUND.

BEFORE FULL POWER WAS ACHIEVED AND A POSITIVE CLIMB ESTABLISHED, THE AIRCRAFT DESCENDED BACK TO THE RUNWAY.

THE AIRCRAFT CONTACTED THE RUNWAY NOSE GEAR FIRST, FOLLOWED BY THE MAIN LANDING GEAR. DIRECTIONAL CONTROL WAS MAINTAINED THROUGHOUT THE EVENT.

THE ENGINE CONTINUED TO OPERATE NORMALLY FOLLOWING THE IMPACT. PILOT ELECTED TO CONTINUE THE LANDING ROLLOUT, EXITED THE RUNWAY NORMALLY,

AND TAXIED TO THE FBO WHERE THE AIRCRAFT WAS SHUT DOWN.

DURING POST-FLIGHT INSPECTION, DEFORMATION OF THE PROPELLER BLADES WAS OBSERVED, CONSISTENT WITH A PROPELLER STRIKE.FURTHER INSPECTION REVEALED COLLAPSE OF THE NOSE LANDING GEAR STRUT, CONSISTENT WITH A FIRM NOSE GEAR CONTACT.

Other reports on N4951Y · 1

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