Aviation Crash Map

Gulfstream-Schweizer A/C G-164B N425LS

25 July 2014 · Bonifay, Florida, United States · No injuries

Summary

On 25 July 2014 at about 13:23 local time, a Gulfstream-Schweizer A/C G-164B registered N425LS, operated by Croom Aviation, was involved in an accident near Bonifay, Florida, United States. One person was on board and nobody was 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 13:23
Classification
Accident
Location
Bonifay, Florida, United States
Nearest airport
Tri-County Airport (1J0)
Coordinates
30.8453, -85.5906
Aircraft
Gulfstream-Schweizer A/C G-164B
Registration
N425LS
Category
Airplane
Year built
1979
Engines
1
Operator
Croom Aviation
Operating rule
Part 91: General Aviation
Purpose of flight
Positioning
Phase of flight
Not recorded
Route
Donalsonville → Bonifay
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
ERA14LA368

People

Nobody was injured.

On board Died Serious Minor Uninjured
1 0 0 0 1

Probable cause

A partial blockage of the No. 2 bearing oil nozzle jet by bearing material, which resulted in oil starvation and the subsequent failure of the No. 2 bearing and total loss of engine power.

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

Read the full NTSB narrative

The commercial pilot was conducting a cross-country positioning flight in the turboprop airplane. The pilot reported that, while on approach to the destination airport, the propeller began wind-milling, and "pieces of metal" began coming out of the right engine exhaust duct. The pilot subsequently conducted a forced landing, during which the airplane struck trees. Postaccident examination of the engine revealed that the No. 2 bearing oil nozzle jet was partially blocked, which resulted in oil starvation and the subsequent disintegration of the No. 2 roller bearing. The material blocking the oil nozzle jet was consistent with material used in the composition of the bearing races and rollers. A review of maintenance records revealed that the No. 1 engine bearing had failed about 1,000 flight hours before the accident and was replaced along with the No. 2 bearing. In addition, the Nos. 1 through 5 bearings were replaced about 300 flight hours before the accident. The investigation could not determine if the No. 2 bearing oil nozzle jet was blocked by bearing material as a result of the previous bearing failure or if the blockage developed during the engine's subsequent operation.

Quoted verbatim from the NTSB record.

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