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Aviation safety reports, made easier to study

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September 30, 2007 · Bellanca 7GCBC · N41695

Laurel, MT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 30, 2007
Injury Outcomes
No injuries (2 uninjured)
Location
Laurel, MT
Aircraft
Bellanca 7GCBC
Tail Number
N41695
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX07CA288

During an instructional flight, the left main landing gear assembly broke during rollout following a normal landing. An examination of the gear assembly revealed evidence that a step had been spot welded onto the gear. Over time, corrosion developed in the vicinity of the weld, and the gear fractured due to corrosion induced fatigue and separated. No evidence of gear maintenance specific to the welding of the step to the gear assembly was documented in the airplane's maintenance records.

NTSB Probable Cause

Corrosion and fatigue-induced failure of the landing gear structure.

Full Narrative

On September 30, 2007, about 1505 mountain daylight time, a Bellanca 7GCBC, N41695, experienced the breakage and separation of its left main landing gear during landing rollout at the Laurel Municipal Airport, Laurel, Montana. The airplane was owned and operated by the private pilot, who was receiving flight instruction from his airline transport certificated flight instructor (CFI). The airplane was substantially damaged. Neither pilot was injured. Visual meteorological conditions prevailed at the time, and no flight plan had been filed. The flight was performed under the provisions of 14 CFR Part 91, and it originated from Billings, Montana, about 1400. The CFI reported to the National Transportation Safety Board investigator that he was providing transition flight training to the student, and they had performed a series of uneventful takeoffs and landings. During the accident landing down the center of runway 22, the left main gear separated at the point where a step had been attached, and as the airplane rolled to a stop, the left wing's lift strut buckled. The Federal Aviation Administration (FAA) coordinator reported that his examination of the airframe revealed evidence that the step had been spot welded onto the spring steel gear assembly. The assembly fatigued and broke in the vicinity of the spot weld. The FAA coordinator stated that evidence of corrosion was observed in the area where the gear assembly fractured. No evidence of gear maintenance, including the welding of the step to the gear assembly, was documented in the airplane's maintenance records.

Flight

Event TypeAccident
Event Time15:05 MDT
Nearest AirportLaurel Municipal (0nm)
Runway22
Runway Length5200 ft
Runway Width75 ft
Flight Plan FiledNone
Aircraft FireNo

Aircraft

AircraftBellanca 7GCBC
Tail NumberN41695
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-A2B · Reciprocating

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 77 · Third Class
Crew 2Age 53 · Third Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data