N38JK

Substantial
None

John H. Korb Jr. KITFOX III S/N: 751

Accident Details

Date
Sunday, May 24, 1998
NTSB Number
LAX98LA173
Location
CARSON CITY, NV
Event ID
20001211X10138
Coordinates
39.260852, -119.789840
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The failure of the right landing gear shock cord because of ultraviolet deterioration in an area of abraded outer fabric, that resulted in a loss of directional control on landing and subsequent ground collision. Factors were the owner/builder's failure to replace the worn shock cord, and the kit manufacturer's failure to include its replacement in the annual inspection checklist.

Aircraft Information

Registration
N38JK
Make
JOHN H. KORB JR.
Serial Number
751
Engine Type
None
Model / ICAO
KITFOX III FK9
No. of Engines
0

Registered Owner (Historical)

Name
SCHUMER KENNETH E
Address
53666 CENTRAL WAY
Status
Deregistered
City
LA PINE
State / Zip Code
OR 97739-9726
Country
United States

Analysis

On May 24, 1998, at 0930 hours Pacific daylight time a Korb Kitfox III, N38JK, an experimental airplane, veered to the right off runway 27 while practicing touch-and-go landings at the Carson City, Nevada, airport. The airplane, operated under 14 CFR Part 91, sustained substantial damage. The private pilot/owner/builder, and a pilot rated passenger were not injured. Visual meteorological conditions existed for the local personal flight and no flight plan was filed.

The pilot reported that on the fourth touch-and-go landing, the airplane veered to the right and departed the runway. The pilot attempted a go-around, but he stated that the airspeed was too low. He reported that the shock cord on the right main landing gear broke, "making it impossible to control the airplane."

According to a Federal Aviation Administration (FAA) inspector, the airplane had recently gone through an annual inspection 2 months prior to the accident with no discrepancies noted. Approximately 125 hours had accrued on the airframe since the annual inspection, with no replacement of the shock cords. The kit manufacturer stated that they recommend replacement of the shock cord at the time of the annual inspection.

The Product Development Manager from the airplane kit manufacturer inspected the shock cord. He stated that the shock cord is designed to be the weak link in the landing gear system and will fail at some point. The manager stated that the ends showed signs of ultra violet aging on the internal rubber that may have been caused by missing outer fabric lacing, or from it being worn through at the break point. He further stated that there was damage on the outer fabric lacing which may have been due to abrasion or from over stress. The report stated that signs of UV and abrasion to the bungee "point toward the shock cord rubbing on something that may or may not have played a part on the failure."

The manager further stated that the airplane will normally veer away from the broken cord; however, it is possible with certain variables in place for the airplane to travel the same direction as the broken shock cord due to added drag on that side.

Review of the manufacturer's maintenance and inspection criteria revealed that there were no provisions made in the annual inspection checklist for replacement of the shock cords during the annual inspection due to natural aging of the shock cord. In the manufacturer's newsletter, under Maintenance Items, there is a reminder to replace the shock cords annually. The pilot stated that he was not aware that the shock cords needed to be replaced on an annual basis. The manufacturer has since amended the annual inspection checklist to "replace bungee (recommended each year due to natural aging of bungee)."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX98LA173