20170712014099I

Incident · Minor damage

FAA incident report · Piper PA-44-180 · Raleigh, NC · July 12, 2017

Date
July 12, 2017 · 11:20 local
Place
Raleigh, NC
Airport
Raleigh-Durham International
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Operator
F3CV
Damage
Minor damage
Aircraft
N2236D
Reported as
Piper PA-44-180
Reported engine
Lycoming O&VO-360 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
560 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.

Bird strike approximately 150 feet AGL on short final to runway 32 at rdu. Bird was medium to large size brown hawk. Bird made contact with the left wing just inside of the stall warning tabs. Two small dents near leading edge of wing.

Repair: inspected left wing for bird damage. Found 2 small dents left wing 1 inch inside inner stall vane. Dents measure 1/2 inch circumference and .020 inch deep. Dents negligible per PA-44 -180 maintenance manual chapter 51-70-00. No further repairs needed.

As the FAA filed it

BIRD STRIKE APPROXIMATELY 150 FEET AGL ON SHORT FINAL TO RUNWAY 32 AT RDU. BIRD WAS MEDIUM TO LARGE SIZE BROWN HAWK. BIRD MADE CONTACT WITH THE LEFT WING JUST INSIDE OF THE STALL WARNING TABS. TWO SMALL DENTS NEAR LEADING EDGE OF WING.

REPAIR: INSPECTED LEFT WING FOR BIRD DAMAGE. FOUND 2 SMALL DENTS LEFT WING 1 INCH INSIDE INNER STALL VANE. DENTS MEASURE 1/2 INCH CIRCUMFERENCE AND .020 INCH DEEP. DENTS NEGLIGIBLE PER PA-44 -180 MAINTENANCE MANUAL CHAPTER 51-70-00. NO FURTHER REPAIRS NEEDED.