N105LM

Substantial
Serious

Oakes J3 CUB S/N: LM-1057

Accident Details

Date
Thursday, April 29, 1999
NTSB Number
FTW99LA125
Location
GREENBRIAR, AR
Event ID
20001205X00473
Coordinates
35.220256, -92.379005
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The student pilot's failure to compensate for the gusty wind condition while maneuvering, which resulted in the inadvertent stall. A factor was the gusty wind condition.

Aircraft Information

Registration
N105LM
Make
OAKES
Serial Number
LM-1057
Engine Type
Reciprocating
Year Built
1994
Model / ICAO
J3 CUB SA03
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
OAKES DONALD C
Address
RT 3 PO BOX 43
Status
Deregistered
City
CLINTON
State / Zip Code
AR 72031
Country
United States

Analysis

On April 29, 1999, approximately 1125 central daylight time, an Oakes J-3 Cub experimental homebuilt airplane, N105LM, was substantially damaged during terrain impact while maneuvering near Greenbriar, Arkansas. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal cross-country flight. The aircraft was owned and operated by the pilot/builder. The student pilot, sole occupant of the aircraft, sustained minor injuries. The flight originated from Clinton, Arkansas, with a destination of Chael, a private airstrip near Wooster, Arkansas.

A witness reported observing the aircraft's nose drop as it made a right turn. Subsequently, the aircraft's right wing and nose impacted the ground. The witness further reported that the engine was running during the entire event.

The 71-hour student pilot reported to the FAA inspector that "the aircraft entered a slow right hand, uncontrolled turn, [and] continued [in] that mode of flight until impacting the earth." The aircraft came to rest inverted.

Examination of the aircraft wreckage by the FAA inspector revealed that the engine was separated from the fuselage. The outboard section of the right wing was separated. The left and right wings were partially separated from the fuselage. The main landing gear was separated from the fuselage.

According to the FAA inspector, high gusty wind conditions prevailed at the time of the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW99LA125