N3698C

Substantial
None

CESSNA 180R S/N: 31197

Accident Details

Date
Sunday, October 15, 1995
NTSB Number
CHI96LA009
Location
SEATTLE, WA
Event ID
20001207X04663
Coordinates
47.610572, -122.329757
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the pilot's failure to maintain control of the airplane during the landing roll. A factor in the accident was the gusty wind conditions.

Aircraft Information

Registration
Make
CESSNA
Serial Number
31197
Engine Type
Reciprocating
Year Built
1954
Model / ICAO
180R C180
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
180

Registered Owner (Current)

Name
TOMLINSON JOHN J
Address
17635 SE 297TH PL
City
KENT
State / Zip Code
WA 98042-5713
Country
United States

Analysis

On October 15, 1995, at 1540 pacific daylight time (pdt), a Cessna 180R, N3698C, was substantially damaged while landing at Boeing Field, Seattle, Washington. The pilot reported no injuries. The 14 CFR Part 91 flight originated from Camas, Washington, at 1440 pdt. Visual meteorological conditions existed at the time of the accident and a VFR flight plan was on file.

In a detailed written statement, the pilot reported the approach to landing on runway 13R was normal with correction inputs to maintain runway centerline. The pilot stated that while the airplane was on final approach, ATIS was reporting the winds from 170 degrees at 8 knots. He had also heard a wind check transmission from the control tower reporting the winds from 170 variable to 270 degrees at 14 knots. The control tower also reported the winds as gusting, but the remainder of this transmission was cut off by another airplane transmitting on the same frequency.

The pilot stated that approximately 100 feet AGL, the airplane's VSI went full scale down. He immediately applied full power but a high sink rate began. The pilot stated directional control was maintained, but touchdown was unavoidable. The airplane touched down with full aileron and full rudder correction to stop the drift. The pilot reported that he decided that a go around would not be possible without loosing directional control of the airplane because the rudder was at its limit. The pilot stated that as the airplane slowed during the landing roll, the horizontal stabilizer lost authority at full travel. The airplane's tail dropped and the left wing impacted the runway.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI96LA009