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May 20, 2001 · Piper PA-44-180 · N3042C

Brooksville, FL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 20, 2001
Injury Outcomes
No injuries (3 uninjured)
Location
Brooksville, FL
Aircraft
Piper PA-44-180
Tail Number
N3042C
Operator
Clearwater Aviation
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ATL01LA058

During the takeoff roll the pilot noticed the aircraft pulling to the left. He aborted takeoff, reduced power and as the pilot applied brakes the left main landing gear collapsed. 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. The total fatigue region occupied about 35 percent of the cross section of the cylinder.

NTSB Probable Cause

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

Full Narrative

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.

Flight

Event TypeAccident
Event Time10:45 EDT
Nearest AirportHernando County (0nm N)
Runway27
Runway Length7001 ft
Runway Width150 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-44-180
Tail NumberN3042C
Aircraft CategoryAir
DamageSubstantial
OperatorClearwater Aviation
Operating RulePart 91
Engines2
Engine TypeReciprocating
Engine DetailsLycoming · L-0-360 · Reciprocating
Seats4

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 26 · First Class · None

Conditions

ConditionsVMC
LightDaylight
Wind4 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point64 F
Altimeter29.97 inHg
Observation Time18:53
Weather SourceWFAC

Appendix: Source Data