Aviation Crash Map

Rovey Jason H RV-8 N391V

2 November 2013 · Wickenburg, Arizona, United States · No injuries

Summary

On 2 November 2013 at about 18:41 local time, a Rovey Jason H RV-8 registered N391V was involved in an accident near Wickenburg, Arizona, 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 18:41
Classification
Accident
Location
Wickenburg, Arizona, United States
Nearest airport
Wickenburg Muni (E25)
Coordinates
33.9706, -112.6950
Aircraft
Rovey Jason H RV-8
Registration
N391V
Category
Airplane
Year built
2007
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Wickenburg → Wickenburg
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
WPR14LA046

People

Nobody was injured.

On board Died Serious Minor Uninjured
1 0 0 0 1

Probable cause

The fatigue failure of a propeller pitch change pin due to excessive shot peening of the pin’s surface during the manufacturing process.

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

Read the full NTSB narrative

The pilot reported that, during cruise flight, he felt a sustained vibration, which he thought was from the engine or propeller, and that the airplane then started to slow down. The pilot made a forced landing to the desert, and the airplane came to rest on its nose, which caused substantial damage to the airplane. A postaccident engine run and subsequent engine examination revealed no mechanical anomalies that would have precluded normal operation. The propeller examination revealed that one of the propeller pitch change pins had broken. The pin's fracture would have resulted in the sustained vibration and loss of speed reported by the pilot. A metallurgical examination of the pin revealed that it had failed due to a fatigue crack that had progressed through about 70 percent of the pin. The fatigue crack initiated at dimples that had a depth and width consistent with excessive shot peening, which likely occurred during the manufacturing process.

Quoted verbatim from the NTSB record.

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