20200312001399I

Incident · Minor damage

FAA incident report · Beech A36 · Sanford, FL · March 12, 2020

Date
March 12, 2020 · 17:11 local
Place
Sanford, FL
Airport
Orlando Sanford
Phase of flight
Cruise/Level Flight
Operating rules
Air taxi and commuter (Part 135)
Operator
XGNA
Damage
Minor damage
Aircraft
N75AT
Reported as
Beech A36
Reported engine
Continental IO-520 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
3,470 total111 in this make and model176 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 3/12/2020, at approximately 22:11Z, N75AT (GTA505) a BE36, s/n E-597 while enroute at 7000? From opf-sfb, reported a bird strike (cormorant) to the center of the passenger side of the windshield 7 miles west of sfb. The bird penetrated the windshield striking the glare shield , instrument panel, compass and the pilots right shoulder/arm (no injuries). Also the right wing outboard leading edge was impacted and dented (1?x 2? Area). The lower vertical stab leading edge was also damaged. (1.5? Hole). A light gun was used to clear the aircraft to land runway 9L without incident.

As the FAA filed it

ON 3/12/2020, AT APPROXIMATELY 22:11Z, N75AT (GTA505) A BE36, S/N E-597 WHILE ENROUTE AT 7000? FROM OPF-SFB, REPORTED A BIRD STRIKE (CORMORANT) TO THE CENTER OF THE PASSENGER SIDE OF THE WINDSHIELD 7 MILES WEST OF SFB. THE BIRD PENETRATED THE WINDSHIELD STRIKING THE GLARE SHIELD , INSTRUMENT PANEL, COMPASS AND THE PILOTS RIGHT SHOULDER/ARM (NO INJURIES). ALSO THE RIGHT WING OUTBOARD LEADING EDGE WAS IMPACTED AND DENTED (1?X 2? AREA). THE LOWER VERTICAL STAB LEADING EDGE WAS ALSO DAMAGED. (1.5? HOLE). A LIGHT GUN WAS USED TO CLEAR THE AIRCRAFT TO LAND RUNWAY 9L WITHOUT INCIDENT.

Other reports on N75AT · 2

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