N115ND

Substantial
None

Piper PA-28-161 S/N: 2841035

Accident Details

Date
Friday, June 9, 2000
NTSB Number
LAX00LA219
Location
MESA, AZ
Event ID
20001212X21261
Coordinates
33.330600, -111.630691
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the failure of the pilot to maintain directional control in that he failed to properly position the ailerons during his landing roll. Gusty, crosswind conditions, from a direction and velocity that equaled the aircraft's maximum demonstrated crosswind capability, were a factor in this accident.

Aircraft Information

Registration
N115ND
Make
PIPER
Serial Number
2841035
Engine Type
Reciprocating
Model / ICAO
PA-28-161 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Analysis

On June 9, 2000, at 1045 hours mountain standard time, a Piper PA-28-161, N115ND, struck a distance remaining marker sign on the landing rollout at the Williams Gateway Airport, Mesa, Arizona. The airplane, owned and operated by the University of North Dakota under 14 CFR Part 91 as an instructional flight, sustained substantial damage. The solo student pilot was not injured. Visual meteorological conditions existed for the local training flight, and no flight plan was filed. The flight originated at 0900 from the accident airport and was scheduled to terminate at the time of the accident.

The student pilot, on a supervised solo flight, had returned from the practice area to practice stop-and-go landings on runway 12R. On the first landing the airplane veered to the right side of the runway, and struck a distance remaining sign with the right wing. After the collision, the airplane taxied to the ramp without further incident.

The Automatic Terminal Information System (ATIS) broadcast located on the field reported at 0947 the winds to be 120 degrees at 6 knots. At 1050, the winds were reported to be from 180 degrees at 12 knots gusting to 20 knots. Witnesses at the accident site reported that the winds were variable in direction with gusty conditions. According to the pilot's operating handbook (POH), the demonstrated crosswind capability for this airplane is 17 knots. According to the chart, the effective crosswind component at the time of the accident was 17 knots.

The student had received the prescribed dual instruction in the performance of crosswind landings according to his training records.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX00LA219