Aviation Crash Map

Soko GALEB G 2 N90SR

21 February 2018 · Elko, Nevada, United States · Serious injuries

Summary

On 21 February 2018 at about 18:15 local time, a Soko GALEB G 2 registered N90SR was involved in an accident near Elko, Nevada, United States. One person was on board and one was seriously injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 18:15
Classification
Accident
Location
Elko, Nevada, United States
Nearest airport
Elko Rgnl (EKO)
Coordinates
40.8233, -115.7886
Aircraft
Soko GALEB G 2
Registration
N90SR
Category
Airplane
Year built
1966
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Reno → Elko
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
WPR18LA094

People

1 person was seriously injured.

On board Died Serious Minor Uninjured
1 0 1 0 0

Probable cause

An improperly installed brake cylinder, which resulted in insufficient hydraulic pressure being provided to three of the brake cylinders and the left brake being inoperable during landing.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The pilot reported that, upon initial landing the airplane, the left brake was inoperative, and he chose to conduct a go-around and set up for a single-brake landing. The subsequent landing was uneventful, but the left brake was still inoperative. The pilot reported that, with about 1,500 ft of runway remaining, he chose to veer the airplane off the runway to the right to avoid running off the end. Subsequently, the airplane struck a drainage ditch berm, which resulted in substantial damage to the fuselage. Examination and disassembly of the hydraulically driven left brake assembly revealed that the No. 2 brake cylinder had not been properly installed, which allowed the brake pucks to move and resulted in three of them separating from the brake assembly. The separation of the brake pucks resulted in the No. 2 cylinder's piston being moved to the full-scale inward position. Subsequently, the No. 2 cylinder's piston then fully deflected, which resulted in a hydraulic leak that subsequently led to insufficient hydraulic pressure being provided to the other brake cylinders and subsequently to the left brake being inoperative during landing.

Quoted verbatim from the NTSB record.

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