Aviation Crash Map

Hefner Pitts S1S N10HJ

17 August 1997 · Van Nuys, California, United States · Fatal

Summary

On 17 August 1997 at about 20:00 local time, a Hefner Pitts S1S registered N10HJ was involved in an accident near Van Nuys, California, United States. One person was on board and one died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 20:00
Classification
Accident
Location
Van Nuys, California, United States
Coordinates
34.1902, -118.4907
Aircraft
Hefner Pitts S1S
Registration
N10HJ
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Aircraft damage
Destroyed
Weather
VMC
Light
Not Reported
NTSB number
LAX97FA291

People

1 person died.

On board Died Serious Minor Uninjured
1 1 0 0 0

Probable cause

the operation of the propeller beyond the design rpm limitations and the resultant gyroscopic loads from aerobatics. Contributing to the accident was the lack of a required instrument panel rpm restriction for the propeller mandated by an airworthiness directive.

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

Read the full NTSB narrative

The pilot departed and requested a right-hand departure to the practice area. During the downwind departure he declared an emergency and witnesses observed the aircraft spiraling downward at a 45-degree angle into a residential street. Parts from the aircraft were found some distance from the accident site. The propeller along with the severed crankshaft flange were found still bolted together less part of one propeller blade. Metallurgical examination revealed that a blade had failed midspan due to fatigue. The propeller was being operated above the design rpm red line of 2,700. Additionally, the propeller was being subjected to gyroscopic aerobatic loads. An rpm restriction for the propeller mandated by an airworthiness directive was not placarded on the instrument panel per the AD. The engine was designed for a type certificated helicopter application and was approved for a 3,200 rpm red line.

Quoted verbatim from the NTSB record.

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