N100AG

Substantial
None

Raytheon HAWKER 800XPS/N: 258747

Accident Details

Date
Saturday, March 14, 2020
NTSB Number
WPR20LA109
Location
Scottsdale, AZ
Event ID
20200316X11409
Coordinates
33.622776, -111.910552
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot’s inability to maintain directional control during landing for undetermined reasons, which resulted in a runway excursion.

Aircraft Information

Registration
Make
RAYTHEON
Serial Number
258747
Engine Type
Turbo-fan
Year Built
2005
Model / ICAO
HAWKER 800XP
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
15
FAA Model
HAWKER 800XP

Registered Owner (Current)

Name
DODSON INTL PARTS INC
Address
2155 VERMONT RD
City
RANTOUL
State / Zip Code
KS 66079-9014
Country
United States

Analysis

On March 14, 2020, about 1600 mountain standard time, a Raytheon Aircraft Company Hawker 800XP, N100AG, was substantially damaged when it was involved in an accident at Scottsdale Airport, Scottsdale, Arizona. The pilot and copilot were not injured. The airplane was being operated under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight.

The pilot stated that the flight departed from Roger, Arkansas, about 1315 central standard time (1215 mountain standard time). After an uneventful flight, the airplane touched down on the runway 21 centerline with light and variable wind conditions. The pilot recalled that the touchdown felt normal but that, during the landing roll, the airplane began to veer to the right. The pilot added full left rudder, but the airplane continued to veer off the runway surface and encountered large rocks located between the runway and taxiway. The airplane collided with runway lights and a sign, puncturing the left wing; both engines sustained foreign object damage from the rocks.

The pilot thought that the loss of control was a result of the nosewheel steering system not being aligned correctly. A postaccident operational check of the steering system revealed no mechanical malfunctions or anomalies that would have precluded normal operation. The left-side nosewheel tire was not adequately inflated and was worn to the point at which the cord was exposed; the right-side tire was within tolerances. Also, one-third of the rim was absent on the nosewheel left-side outer wheel half. On the basis of the available evidence, a determination could not be made regarding whether the damage occurred before the touchdown or as a result of the accident sequence.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR20LA109