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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

May 14, 1994 · Luscombe 8E · N71128

Deland, FL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 14, 1994
Injury Outcomes
1 injury (1 minor injury)
Location
Deland, FL
Aircraft
Luscombe 8E
Tail Number
N71128
Operator
Citrus Soaring Club
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
MIA94LA140

THE LUSCOMBE 8E WAS EQUIPPED WITH A LYCOMING O-320 ENGINE (150 HP) AND WAS BEING USED TO TOW GLIDERS. WHILE LANDING AFTER A GLIDER RELEASE, THE LEFT MAIN LANDING GEAR STRUT FAILED AND THE WHEEL SEPARATED. THE AIRCRAFT THEN NOSED OVER AND CAME TO REST INVERTED. AN EXAMINATION OF THE FAILED LANDING GEAR STRUT INDICATED IT WAS RUSTED ON THE INSIDE AND A PREEXISTING CRACK WAS PRESENT AT THE POINT OF FAILURE.

NTSB Probable Cause

CORROSION AND SUBSEQUENT FAILURE OF THE LEFT MAIN LANDING GEAR STRUT.

Full Narrative

On May 14, 1994, about 1425 eastern daylight time, a Luscombe 8E, N71128, registered to Elizabeth B. Burbank, operating as a 14 CFR Part 91 glider tow flight, crashed on landing at the Bob Lee Airport, Deland, Florida. The airplane sustained substantial damage and the commercial pilot received a minor injury. Visual meteorological conditions prevailed and no flight plan was filed. The flight originated at Deland, Florida, at 1415. The pilot stated that on landing touchdown the left main landing gear wheel separated when the gear strut failed. The remainder of the strut dug into the grass runway and the aircraft nosed over on to its back. Examination of the aircraft by FAA inspectors indicated the left landing gear strut was rusted and had a preexisting crack at the point the lower strut and main wheel separated. Water had been trapped inside the strut tube. No drain holes were present in the tube. The holder of the Luscombe FAA Type Certificate stated that the strut has several bolt holes through it. The strut "sweats" internally causing water to build up in the lower part of the strut. Rust then forms, resulting in strut failure due to cracking.

Flight

Event TypeAccident
Event Time14:25 EDT
Nearest AirportBob Lee Flight Strip (1nm E)
Runway9
Runway Length3300 ft
Runway Width72 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftLuscombe 8E
Tail NumberN71128
Aircraft CategoryAir
DamageSubstantial
OperatorCitrus Soaring Club
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-320-A2B · Reciprocating · 150
Seats2

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 67 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind90° @ 10 kt, gusting 15 kt
Visibility7 sm
CeilingOvercast 30000 ft
Temperature / Dew Point70 F
Altimeter30.00 inHg
Observation Time17:51
Weather SourceWFAC

Appendix: Source Data