N900AM

MINR
None

PIPER PA-23-250S/N: 27-7954014

Accident Details

Date
Thursday, August 27, 2015
NTSB Number
CEN15IA385
Location
Joliet, IL
Event ID
20150827X82014
Coordinates
41.577777, -88.173057
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A bird strike.

Aircraft Information

Registration
Make
PIPER
Serial Number
27-7954014
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
PA-23-250PA27
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
6
FAA Model
PA-23-250

Registered Owner (Current)

Name
GIMLI SON LLC
Address
1525 NW 56TH ST HNGR G
City
FORT LAUDERDALE
State / Zip Code
FL 33309-2811
Country
United States

Analysis

On August 27, 2015, about 1110 central daylight time, a Piper PA-23-250, N900AM, sustained minor damage when it was struck by an unknown object while in cruise flight at 2,500 ft above mean sea level (1,920 ft above ground level) about 4 nm north of the Joliet Regional Airport (JOT), Joliet, Illinois. The commercial pilot was not injured. The airplane was registered to and operated by Aerial Imaging Inc. under the provisions of the 14 Code of Federal Regulations Part 91 as a positioning flight. Visual meteorological conditions prevailed at the time of the incident, and no flight plan was filed. The airplane departed the Aurora Municipal Airport (AAR), Aurora, Illinois, about 1100 and landed without incident at the South Bend International Airport (SBN), South Bend, Indiana.

The pilot reported that he heard a "bang" and felt a jolt in the flight controls while he was completing the cruise checklist. He did not see any objects before the noise, and he did not see any damage to the airplane. The engines were operating normally, the flight controls felt normal, the landing gear indicated up and locked, and the cargo did not appear to have shifted. He continued the flight to SBN. No abnormal flight characteristics were noted during the flight. After landing, damage to the leading edge of the left horizontal stabilizer was observed. The damage included about four dents spanning approximately 13 inches from left to right with the inboard dent piercing the aluminum skin. The damage also included multiple scratches and cuts in the deicing boot that overlies the leading edge of the left horizontal stabilizer.

The damaged section of the deicing boot was removed from the leading edge of the left horizontal stabilizer and shipped to the National Transportation Safety Board's Materials Laboratory for examination. The NTSB examination using an ultraviolet light indicated that insects impacted the deicing boot, but there was no widespread area that fluoresced under exposure to ultraviolet light consistent with an exposure to larger volumes of biological materials. The tears in the deicing boot revealed exhibited features consistent with failure from overstress.

The deicing boot was subsequently examined at the Feather Identification Laboratory, Division of Birds, Smithsonian Institution National Museum of Natural History. Several feather barbs were removed from the tears in the boot during the microscopic examinations that were consistent with remnants from the Columbidae bird family (doves and pigeons).

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN15IA385