N2162C

Substantial
None

Cessna 207 S/N: 20700575

Accident Details

Date
Thursday, June 18, 1998
NTSB Number
ANC98LA104
Location
BETHEL, AK
Event ID
20001211X10225
Coordinates
60.809616, -161.849090
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

An in-flight collision with a large bird.

Aircraft Information

Registration
N2162C
Make
CESSNA
Serial Number
20700575
Engine Type
Turbo-shaft
Year Built
1980
Model / ICAO
207 C07T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
COPPER RIVER AIRMOTIVE LLC
Address
MILE 10 EDGERTON HWY
HC 60 BOX 251B
Status
Deregistered
City
COPPER CENTER
State / Zip Code
AK 99573-9704
Country
United States

Analysis

On June 17, 1998, about 1730 Alaska daylight time, a wheel equipped Cessna 207 airplane, N2162C, sustained substantial damage as a result of a bird strike during approach to the Bethel Airport, Bethel, Alaska. The airplane was being operated as a visual flight rules (VFR) on-demand passenger flight under Title 14, CFR Part 135, when the accident occurred. The airplane is registered to and operated by Kusko Aviation, Inc., Bethel, Alaska. The certificated commercial pilot, and the three passengers aboard, were not injured. Visual meteorological conditions prevailed, and VFR company flight following procedures were in effect. The flight originated at the Quinhagak Airport, Quinhagak, Alaska, about 1655.

During a telephone conversation with the National Transportation Safety Board investigator-in-charge, on July 20, 1998, the pilot stated that while on a left downwind for landing on runway 18, he noticed a brown object pass in front of the windshield, from left to right, striking the right wing. The pilot said he was able to continue the approach, and made a normal landing. Company maintenance personnel performed a postflight inspection and reported substantial damage to the right wing's leading edge and rib assemblies. They noted what appeared to be goose feathers imbedded in the damaged portion of the wing.

In the pilot/operator report (NTSB form 6120.1/2) submitted by the pilot, and dated August 7, 1998, he reported that right wing leading edge skin was crushed back to the forward portion of the spar. The entire leading edge was replaced between the tip cap, and outboard of the attach point of the wing strut.

The pilot noted that there were no preaccident mechanical anomalies with the airplane.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC98LA104