N8561L

Substantial
None

Piper PA-25-260 S/N: 5-4983

Accident Details

Date
Thursday, July 8, 1999
NTSB Number
FTW99LA187
Location
WALLIS, TX
Event ID
20001212X19268
Coordinates
29.629882, -96.060974
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The loss of engine power for an undetermined reason. A factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N8561L
Make
PIPER
Serial Number
5-4983
Engine Type
Reciprocating
Year Built
2001
Model / ICAO
PA-25-260 PA25
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SMITH JEFFREY A
Address
564 STATE ROUTE 94 N
Status
Deregistered
City
WARWICK
State / Zip Code
NY 10990-3159
Country
United States

Analysis

On July 8, 1999, at 1230 central daylight time, a Piper PA-25-260 agricultural airplane, N8561L, was substantially damaged during a forced landing following a loss of engine power near Wallis, Texas. The commercial pilot, sole occupant, was not injured. The airplane was owned and operated by Double L Flying Service of Wallis, Texas. Visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 137 aerial application flight. A flight plan was not filed for the local flight. The airplane was departing at the time of the accident.

The pilot reported that the aircraft experienced a "significant loss of power, followed shortly thereafter by a complete loss in power" after takeoff. The pilot made a right turn toward a cotton field, and the aircraft began to descend. The FAA inspector stated that physical evidence in the cotton field revealed that the "aircraft's landing gear skimmed the cotton field for about 300 feet before contacting the ground." Approximately 75 feet beyond the initial touchdown point, the left wing impacted the ground. The aircraft then continued for another 20 feet before making a 180 degree left turn and coming to rest upright.

During a telephone conversation with the NTSB investigator-in-charge, the operator stated that he test ran the engine both in the field before moving the aircraft, and later, at the operator's hanger. He stated that the engine "ran wide open for several minutes," and he found "no problem with the engine."

According to the FAA inspector, the inboard section of the left wing was "flattened" and the wing was bent upward, the right wing sustained leading edge damage, and the propeller blade tips were bent.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW99LA187