N6179Q

Substantial
None

Cessna 152 S/N: 152-85185

Accident Details

Date
Friday, January 21, 2000
NTSB Number
FTW00LA071
Location
SLIDELL, TX
Event ID
20001212X20367
Coordinates
33.229282, -97.589843
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 improper approach planning, which resulted in a downwind landing. A factor was the loss of engine power for undetermined reasons.

Aircraft Information

Registration
Make
CESSNA
Serial Number
152-85185
Engine Type
4-cycle
Model / ICAO
152 C152
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
152

Registered Owner (Current)

Name
GONZALES JERRY
Address
1751 DEKE SLAYTON LN
City
EL PASO
State / Zip Code
TX 79936-5537
Country
United States

Analysis

On January 21, 2000, at 1600 central standard time, a Cessna 152 airplane, N6179Q, was substantially damaged during a forced landing following a loss of engine power near Slidell, Texas. The airplane was owned and operated by Delta Qualiflight, Inc., of Fort Worth, Texas. The instrument rated private pilot and his pilot-rated passenger were not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The cross-country flight originated from the Fort Worth Meacham International Airport at an unknown time and was destined for Ardmore, Oklahoma.

In the enclosed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the pilot stated that he was near the Bowie VOR diverting back to Fort Worth due to weather. The airplane was at 3,500 feet, when the engine experienced a gradual loss of power. The pilot applied carburetor heat and noted that the engine RPM started to increase. As the airplane began to descend, the "engine stopped." The pilot performed the "emergency procedures" and secured the engine. The pilot elected to land in a field with a tailwind and 10 degrees of flaps extended. He reported that the tailwind was "very strong" and his ground roll was "long." The airplane impacted trees and a fence at the end of the field, structurally damaging the left wing.

At 1553, the weather observation facility in Denton, Texas (located 37 miles southeast of the accident site), reported the wind from 140 degrees at 15 knots, visibility 10 statute miles, scattered clouds at 4,000 feet agl, temperature 56 degrees Fahrenheit, dewpoint 31 degrees Fahrenheit, and altimeter setting 29.99 inches of mercury.

On January 22, 2000, an aircraft mechanic conducted an engine test run at the accident site with all the engine components attached to the airplane. The mechanic stated that the engine started and operated throughout its power range without any anomalies noted.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW00LA071