N4420C

Substantial
Minor

CESSNA 195BS/N: 16005

Accident Details

Date
Sunday, April 28, 2013
NTSB Number
CEN13LA243
Location
Albuquerque, NM
Event ID
20130429X00605
Coordinates
35.145278, -106.795280
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The pilot’s failure to maintain directional control during the landing roll.

Aircraft Information

Registration
Make
CESSNA
Serial Number
16005
Engine Type
Reciprocating
Year Built
1952
Model / ICAO
195BC195
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
5
FAA Model
195B

Registered Owner (Current)

Name
MILTON WILLIAM H
Address
164 HART RD
City
AMSTERDAM
State / Zip Code
NY 12010-8430
Country
United States

Analysis

On April 28, 2013, at 0950 mountain daylight time, a Cessna model 195B airplane, N4420C, was substantially damaged while landing at Double Eagle II Airport (KAEG), Albuquerque, New Mexico. The private pilot and passenger sustained minor injuries. The airplane was registered to and operated by a private individual, under the provisions of 14 Code of Federal Regulations Part 91, without a flight plan. Day visual meteorological conditions prevailed for the personal flight that departed KAEG about 0900.

The pilot reported that the purpose of the accident flight, which consisted of several practice takeoff-and-landings, was to become better acquainted with the flying characteristics of the tailwheel-equipped airplane that he had recently purchased. The pilot reported having about 3 hours of flight experience in the accident airplane make/model. The accident occurred during a full-stop landing on runway 22 (7,398 feet by 100 feet, asphalt). The pilot reported that he made an uneventful approach and three-point touchdown on the runway centerline; however, about 500-600 feet into the landing roll the airplane suddenly veered to the left. The pilot stated that he was unable to regain directional control and that the airplane subsequently departed the left side of the runway before nosing over. The aircraft fuselage and wings were substantially damaged during the accident sequence.

A Federal Aviation Administration (FAA) maintenance inspector examined the airplane multiple times following the accident and confirmed flight control continuity. Additionally, no anomalies or mechanical discontinuities were identified with the tailwheel locking assembly during a functional test. The FAA inspector did not identify any preimpact mechanical malfunctions or failures that would have precluded normal operation of the airplane.

At 0950, the KAEG automated surface observing system reported the following weather conditions: wind 030 degrees true at 3 knots, visibility 10 miles, sky clear, temperature 17 degrees Celsius, dew point -14 degrees Celsius, altimeter setting 30.16 inches of mercury.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN13LA243