N35408

Substantial
None

CESSNA 172S/N: 17281081

Accident Details

Date
Saturday, August 20, 2016
NTSB Number
GAA16CA442
Location
Anchorage, AK
Event ID
20160822X91159
Coordinates
61.250831, -149.809448
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The facility's designation of the taxiway for use by maintenance personnel to conduct high thrust tests without appropriate safeguards in place, which led to maintenance personnel conducting high-power, run-up thrust procedures across the active taxiway and resulted in the loss of directional control of a light, single-engine airplane on the taxiway when it encountered a sudden, unexpected blast of engine thrust.

Aircraft Information

Registration
Make
CESSNA
Serial Number
17281081
Engine Type
Reciprocating
Model / ICAO
172C172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
172R

Registered Owner (Current)

Name
ELMENDORF AERO CLUB
Address
PO BOX 6292
City
JBER
State / Zip Code
AK 99506-6292
Country
United States

Analysis

The flight instructor of a light single-engine airplane reported that while he and the student pilot were on a taxiway under air traffic control (ATC) instruction, the airplane encountered prop wash, originating from a larger (four engine) turbine-powered airplane performing a maintenance engine(s) run-up. The maintenance run-up was performed in a location adjacent to the active taxiway that was authorized for parking as well as 80% engine(s) power run-ups. The larger turbine-powered airplane was the third in a row a five, of like model airplanes being parked at the location. The light single-engine airplane was not on frequency when the larger turbine-powered airplane was given the clearance, and was not told by ATC at any time during their taxi of the larger turbine-powered airplane's intentions. Subsequently, the light single-engine airplane was blown approximately 80 feet from its original location while taxing behind the larger turbine-powered airplane, which resulted in substantial damage to the firewall.

The flight instructor reported that there were no pre impact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation.

As a safety recommendation the flight instructor stated that the incident could have been prevented with better communications between the tower controllers and the larger turbine-powered airplane's ground personnel.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# GAA16CA442