20151226022229A

Accident · Substantial damage

FAA accident report · Cessna 172N · Punta Gorda, FL · December 26, 2015

Date
December 26, 2015 · 17:05 local
Place
Punta Gorda, FL
Airport
Puntagorda Airport
Phase of flight
Ground/Ramp/Ma
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4776E
NTSB investigation
NTSBGAA16CA096
Reported as
Cessna 172N
Reported engine
Lycoming 0-320 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Student
Pilot’s flight hours
47 total31 in this make and model19 in the last 90 days

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 26 December 2015, at 1705 EST, a Cessna 172, N4776E, struck concrete light pole with its left wing. Visual meteorological conditions prevailed at the time. The aircraft was taxiing to a parking spot and struck the light pole with the left wing leading edge approx. 2.5' from the wingtip. The pilot was uninjured. The aircraft suffered substantial damage. The strike caused an approx. 2" deep dent in the leading edge, and caused the aft top side skin of the wing, between the fuselage and flaps, to wrinkle and buckle up in several places in an approx. 2' x 2' area. Subsequent inspection by maintenance personnel revealed that the aft wing spar was buckled which necessitated a re-wing of the aircraft.

As the FAA filed it

ON 26 DECEMBER 2015, AT 1705 EST, A CESSNA 172, N4776E, STRUCK CONCRETE LIGHT POLE WITH ITS LEFT WING. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME. THE AIRCRAFT WAS TAXIING TO A PARKING SPOT AND STRUCK THE LIGHT POLE WITH THE LEFT WING LEADING EDGE APPROX. 2.5' FROM THE WINGTIP. THE PILOT WAS UNINJURED. THE AIRCRAFT SUFFERED SUBSTANTIAL DAMAGE. THE STRIKE CAUSED AN APPROX. 2" DEEP DENT IN THE LEADING EDGE, AND CAUSED THE AFT TOP SIDE SKIN OF THE WING, BETWEEN THE FUSELAGE AND FLAPS, TO WRINKLE AND BUCKLE UP IN SEVERAL PLACES IN AN APPROX. 2' X 2' AREA. SUBSEQUENT INSPECTION BY MAINTENANCE PERSONNEL REVEALED THAT THE AFT WING SPAR WAS BUCKLED WHICH NECESSITATED A RE-WING OF THE AIRCRAFT.

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 N4776E · 2

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