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October 13, 1996 · Cunningham Rotorway EXEC Rotorway E · N18WC

Mather, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
October 13, 1996
Injury Outcomes
1 injury (1 fatality)
Location
Mather, CA
Aircraft
Cunningham Rotorway EXEC Rotorway E
Tail Number
N18WC
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
LAX97LA014

The pilot of a home built helicopter was attempting to drop an object (bag of flour) to a target on the ground. Approaching the target area, the helicopter was observed to maneuver, then it went out of control and crashed. Investigation revealed evidence that the main rotor blades contacted and severed the tailboom. Also, there was evidence of mast bumping. The helicopter was equipped with composite main rotor blades; kit/factory approved blades were made of metal. No mechanical malfunction was found.

NTSB Probable Cause

excessive maneuvering by the pilot, which allowed the main rotor blades to contact and sever the tail rotor system and allowed mast bumping to occur.

Full Narrative

On October 12, 1996, at 1755 hours Pacific daylight time, an experimental Rotorway Exec helicopter, N18WC, crashed at Mather Airport, Mather, California. The pilot was conducting a local visual flight rules personal flight. The helicopter, registered to and operated by the pilot, was destroyed by impact forces and the resulting postimpact fire. The certificated private pilot, the sole occupant, sustained fatal injuries. Visual meteorological conditions prevailed with the winds estimated by witnesses to be at 10 to 15 miles per hour with gusts. The flight departed Mather Airport at an undetermined time. Ground witnesses reported that they observed the helicopter execute a hard right turn followed by a hard left turn with some oscillations. During this maneuver, the main rotor blades struck the tailboom. The helicopter entered an uncontrolled descent, crashed and burned. Examination of the wreckage revealed that the main rotor blades were of a composite material and not the aluminum blades authorized by the manufacturer. There was evidence of some mast bumping next to the teeter stops behind the thrust stops. There was no evidence found of a mechanical malfunction. According to a manufacturer representative at the accident site, he was informed by other pilots that the accident pilot was making a bomb run over a ground target using a bag of flour. He was told that a bag of flour was somewhere in the cabin area and the helicopter was at the correct location over the target area when the accident sequence began.

Flight

Event TypeAccident
Event Time17:55 PDT
Nearest AirportSacrmento Mather (0nm)
Runway0
Flight Plan FiledNone
Aircraft FireGrd
Aircraft ExplosionNo

Aircraft

AircraftCunningham Rotorway EXEC Rotorway E
Tail NumberN18WC
Aircraft CategoryHeli
DamageDestroyed
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsRotorway · Reciprocating

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 50 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind180° @ 10 kt
Visibility20 sm
CeilingBroken clouds 20000 ft
Temperature / Dew Point57
Altimeter29.00 inHg
Observation Time00:47
Weather SourceWFAC

Appendix: Source Data