N80166

Substantial
None

Air Tractor AT802S/N: 802A-0685

Accident Details

Date
Tuesday, July 14, 2020
NTSB Number
ANC20LA069
Location
Birch Creek , AK
Event ID
20200715X05658
Coordinates
65.991028, -144.544690
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A loss of control for undetermined reasons while on the surface of the water during scoop operations in support of wildland firefighting operations.

Aircraft Information

Registration
Make
AIR TRACTOR
Serial Number
802A-0685
Engine Type
Turbo-prop
Year Built
2017
Model / ICAO
AT802AT8T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
AT-802A

Registered Owner (Current)

Name
AERO SPRAY INC DBA
Address
PO BOX 143
City
APPLETON
State / Zip Code
MN 56208-0143
Country
United States

Analysis

On July 14, 2020, about 1555 Alaska daylight time, an Air Tractor AT802A airplane, N80166, sustained substantial damage when it was involved in an accident near Birch Creek, Alaska. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 firefighting flight.

The mission-specific modified airplane was used to support wildland firefighting operations. The airplane was equipped with Wipline 10000 amphibious floats. Scoops/probes could be manually deployed by a switch located on the control stick of the airplane that actuated an electrically driven hydraulic pump; when the switch was released the scoops would retract. Water was routed through the scoops located on each float to a hopper located in the aircraft. In addition, the airplane was equipped with an asymmetric scoop warning system. In the event of an asymmetric scoop deployment, an audible warning “scoop malfunction” would sound, and a red warning light would illuminate on the instrument panel.

According to the pilot, on the 28th scoop of the day, he touched down on the surface of the water and deployed the scoops to begin filling the airplane’s hopper when the airplane veered to the right. In an effort to correct for the veer he released the scoop switch and applied left rudder to no avail. He retarded the throttle and applied reverse thrust as the airplane began to impact trees located on the lake’s shoreline. The airplane came to rest upright in a marshy area on the lake’s shoreline sustaining substantial damage to the right wing.

A series of postaccident examinations of the airplane including its fuel system, flight control system and water scoop system revealed no preaccident mechanical failures or malfunctions that would have precluded normal operations. Control continuity was established for all flight and engine controls.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC20LA069