N3024C

Substantial
None

PIPER PA28S/N: 28-7990149

Accident Details

Date
Friday, June 24, 2016
NTSB Number
ERA16LA234
Location
Poughkeepsie, NY
Event ID
20160630X24758
Coordinates
41.626667, -73.884162
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

An overstress failure of the left main landing gear attachment bolts, which resulted in the left main landing gear collapse.

Aircraft Information

Registration
Make
PIPER
Serial Number
28-7990149
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
PA28P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-28-181

Registered Owner (Current)

Name
CASH MANAGEMENT CONSULTING LLC
Address
15 JAMES WAY
City
GRANITE SPRINGS
State / Zip Code
NY 10527-1116
Country
United States

Analysis

On June 24, 2016, at 1130 eastern daylight time, a Piper PA-28-181, N3024C, was substantially damaged while taxing at the Dutchess County Airport (POU), Poughkeepsie, New York. The flight instructor and student pilot were not injured. Visual meteorological conditions prevailed and no flight plan was filed. The airplane was registered to and operated by West Field Flight Academy, in accordance with 14 Code of Federal Regulations Part 91 as an instructional flight.According to the flight instructor, after landing on runway 6, he contacted the POU air traffic control tower and requested to taxi on the crossing runway to the ramp. They taxied the airplane about 3,000 ft down the runway and just prior to the turn, the airplane started to veer to the left. The flight instructor heard a "metallic sound" left main landing gear collapsed bringing the airplane to a stop. The flight instructor informed the tower controller, performed an engine shut down, and exited the airplane with the student pilot.

Examination of the airplane by a Federal Aviation Administration inspector revealed that the left main landing gear strut separated from the wing spar attachment. Further examination revealed the wing spar bent upward. Examination of the landing gear strut revealed that the attaching bolts had sheared in the vicinity of the threads. The fracture features of the bolts displayed signatures consistent with overstress failure.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA16LA234