N59661

Substantial
None

PIPER PA-36-300S/N: 36-7760071

Accident Details

Date
Saturday, February 25, 2012
NTSB Number
ERA12LA195
Location
Americus, GA
Event ID
20120228X91509
Coordinates
32.110553, -84.188888
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 maintenance personnel to properly secure a portion of the right wing leading edge, which resulted in the separation of the associated section of the leading edge during takeoff and the loss of directional control during the subsequent landing.

Aircraft Information

Registration
N59661
Make
PIPER
Serial Number
36-7760071
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
PA-36-300PA36
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
NONE
Status
Deregistered
City
XXX
State / Zip Code
OK 73125
Country
United States

Analysis

On February 25, 2012, about 1615 eastern standard time, a Piper PA-36-300, N59661, was substantially damaged following a loss of control on the ground during landing, after a section of the right wing leading edge separated in flight, at the Jimmy Carter Regional Airport (ACJ), Americus, Georgia. Day visual meteorological conditions prevailed and no flight plan had been filed. The certificated commercial pilot was not injured. The maintenance test flight was conducted under the provision of 14 Code of Federal Regulations Part 91.

According to the pilot, the flight departed runway 28 and during the initial climb, about 75 feet above ground level, the airplane pulled abruptly to the right. The pilot applied maximum power and left rudder in order to maintain control of the airplane. During the landing touchdown on runway 5, the airplane veered immediately to the right, departed the side of the runway, crossed a taxiway and a ditch, and then came to rest approximately 300 feet to the right of the runway.

According to photographs provided by the operator, the 66 inch midspan section of the fiberglass leading edge had separated along the gang channel. Approximately 18 inches remained at the accident location but was separated from the wing, and the remaining section was not located.

A Federal Aviation Administration inspector examined the airplane and noted that several of the 92 screws required to hold the midspan section exhibited signs of uneven torque and that two of the screws located on the top inboard corner, and several screws located underside of the leading edge were unable to be located.

According to the airplane maintenance records, the most recent 100-hour inspection was completed on August 17, 2011, and the recorded Hobbs time was 4,899.5 hours. The most recent logbook entry was dated October 6, 2011; the recorded Hobbs time was 4,994.5 hours. According to the operator, aerial spray equipment had just been installed; however, no entry for the installation was noted in the maintenance 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# ERA12LA195