N5290B

Substantial
None

Cessna 152S/N: 15283828

Accident Details

Date
Thursday, October 28, 2004
NTSB Number
DEN05CA016
Location
Santa Teresa, NM
Event ID
20041203X01923
Coordinates
31.881111, -106.704719
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the student pilot' failure to maintain directional control during the takeoff roll. Contributing to the accident was the student pilot's failure to abort the takeoff.

Aircraft Information

Registration
N5290B
Make
CESSNA
Serial Number
15283828
Engine Type
Reciprocating
Year Built
1979
Model / ICAO
152C152
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
TTEA INC
Address
8000 AIRPORT RD UNIT 12
Status
Deregistered
City
SANTA TERESA
State / Zip Code
NM 88008-9714
Country
United States

Analysis

On October 28, 2004, at approximately 0820 mountain daylight time, a Cessna 152, N5290B, piloted by a student pilot, was substantially damaged when it impacted terrain and subsequently nosed over during takeoff roll from Dona Ana County Airport (5T6), Santa Teresa, New Mexico. Visual meteorological conditions prevailed at the time of the accident. The training flight was being conducted under the provisions of Title 14 CFR Part 91 without a flight plan. The pilot reported no injuries. The local flight originated at approximately 0745.

According to the accident report submitted by the student pilot, he had performed two touch and go landings on runway 28. During the ground roll, the pilot advanced the throttle forward to perform another takeoff. The pilot reported that the airplane "veered sharply to the left" and departed the runway. He stated that he was not able to "reduce the power" because it was bumpy. The nose wheel struck an outcropping of sagebrush, separating the nose gear. Subsequently, the airplane nosed over. The top 12 inches of the vertical stabilizer and rudder were crushed to the left and the leading edge of the right wing tip was crushed down and aft. The engine cowling was wrinkled and crushed and the propeller separated at the hub. A postaccident inspection of the airplane systems, by the FAA inspector, revealed no anomalies.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN05CA016