N2580D

Substantial
None

CESSNA 170BS/N: 20732

Accident Details

Date
Wednesday, January 21, 2015
NTSB Number
ANC15LA008
Location
Anchorage, AK
Event ID
20150122X20352
Coordinates
61.184444, -149.963607
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

The pilot’s loss of directional control during takeoff, which resulted in a runway excursion.

Aircraft Information

Registration
Make
CESSNA
Serial Number
20732
Engine Type
Reciprocating
Year Built
1952
Model / ICAO
170BC170
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
170B

Registered Owner (Current)

Name
PLACE ASHLEY K
Address
6821 71ST ST E
City
BRADENTON
State / Zip Code
FL 34203-7176
Country
United States

Analysis

On January 21, 2015 at 1142 Alaska standard time, a tailwheel-equipped, Cessna 170B airplane, N2580D, sustained substantial damage following a loss of control during takeoff from Lake Hood Seaplane Base (Z41), Anchorage, Alaska. The private pilot and three passengers were not injured. The airplane was registered to a private individual and operated by the pilot under the provisions of 14 Code of Federal Regulations (CFR) Part 91 as a personal flight. Visual meteorological conditions prevailed and a visual flight rules (VFR) flight plan had been filed.

During an interview with an investigator from the National Transportation Safety Board (NTSB) on January 21, 2015, the pilot stated that during the takeoff roll, after the brakes were released and full power was applied, the airplane began to veer to the left. The pilot applied right rudder and right brake in an effort to correct for the veer, but the airplane continued to the left, struck a runway edge light, and departed the runway into the snow covered median between the runway and an adjacent taxiway, sustaining substantial damage to the right wing.

A post accident examination of the airplane by the NTSB, along with a Federal Aviation Administration (FAA) aviation safety inspector from the Anchorage Flight Standards District Office revealed no mechanical irregularities that would have precluded normal operation.

A post-accident weight and balance was accomplished by the NTSB using fuel load, passenger weights and seating location provided by the pilot. The aircraft was found to be about 82 pounds over the approved maximum gross weight of 2,200 pounds. The estimated center of gravity at the time of the accident was positive 43.53 inches. The center of gravity range at 2,200 pounds (maximum gross weight) is positive 40.8 inches to positive 46.4 inches.

The closest weather reporting facility is Anchorage International Airport, Anchorage Alaska, less than one mile from the accident site. At 1153, an aviation routine weather report (METAR) from the Anchorage Airport was reporting in part: wind from 120 degrees at 8 knots; sky condition, clear; visibility, 10 statute miles; temperature 12 degrees F; dew point 9 degrees F; altimeter 29.34inHG.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC15LA008