N3042C

Substantial
None

Piper PA-44-180S/N: 44-7995-124

Accident Details

Date
Sunday, May 20, 2001
NTSB Number
ATL01LA058
Location
Brooksville, FL
Event ID
20010531X01038
Coordinates
28.479328, -82.420608
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

The fatigue failure of the left main landing gear strut that resulted in collapse of the landing gear.

Aircraft Information

Registration
N3042C
Make
PIPER
Serial Number
44-7995-124
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
PA-44-180PA44
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
SOUTHWEST AVIAITON SPECIALTIES LLC
Address
8720 JACK BATES AVE
Status
Deregistered
City
TULSA
State / Zip Code
OK 74132-4003
Country
United States

Analysis

On May 20, 2001, at 1045 eastern daylight time, a Piper PA-44-180, N3042C, experienced a collapse of the left main landing gear during takeoff roll in Brooksville, Florida. The personal flight was conducted under provisions of Title 14 CFR Part 91 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane sustained substantial damage; the commercial pilot and three passengers were not injured. The flight was departing from Hernando County Airport, Brooksville, Florida, at 1045.

According to the pilot, while on takeoff roll from runway 27, the airplane pulled noticeably to the left. The pilot elected to abort the takeoff and reduced power and applied the brakes. The left main landing gear collapsed. Examination of the landing gear revealed the left main landing gear strut assembly cylinder was broken. The break occurred at the point where the gear strut cylinder is bolted into the fork assembly.

Laboratory examination of the gear strut cylinder revealed fatigue cracks originating from multiple locations on opposite sides of the bolt hole located on the forward side of the cylinder. Microscopic examination of the bolt hole revealed that the surface of the bolt hole was roughly machined. Further examination of the fracture surface showed multiple ratch and crack arrest marks. The total fatigue region occupied about 35 percent of the cross section of the cylinder.

According to the operator, there is no previous history of maintenance problems on the left landing gear strut.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL01LA058