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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

June 25, 1997 · Enstrom F-28-F · N99YC

Riverside, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 25, 1997
Injury Outcomes
3 injuries (3 minor injuries)
Location
Riverside, CA
Aircraft
Enstrom F-28-F
Tail Number
N99YC
Operator
Stits Aircraft
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
LAX97LA224

During takeoff, the helicopter lost power and landed hard. Postaccident examination revealed the No. 2 cylinder intake valve rocker shaft migrated out of the shaft bosses of the cylinder head. The shaft, cover, and nuts were found; the washers were not. According to owner/pilot there were internal star washer imprints on the cover plate commonly caused by torque or tightening of the nut. The helicopter had 61.5 total hours since new, and received one 50-hour inspection since delivery to the owner/pilot. The owner/pilot changed the oil and filter just prior to the inspection.

NTSB Probable Cause

failure by unknown maintenance personnel to retorque the nuts on the retainer cover.

Full Narrative

On June 25, 1997, at 1243 hours Pacific daylight time, an Enstrom F-28-F helicopter, N99YC, was substantially damaged after a loss of power during a takeoff/climb at Riverside, California. The pilot and two passengers received minor injuries. Visual meteorological conditions prevailed for the local flight and no flight plan was filed. The flight was destined for Corona Airport, Corona, California. According to the pilot, the loss of engine power occurred less than 200 feet agl. He attempted an auto rotation and landed hard. Postaccident examination of the engine revealed that the intake valve rocker shaft migrated out of the shaft bosses of the cylinder head. The shaft, cover, and nuts were found; the washers were not. The pilot stated that there were internal star washer imprints on the cover plate that is commonly caused by the torque or tightening of the nut. The helicopter had 61.5 total hours since new and received one inspection at 50.9 hours since delivery to the owner/pilot. The owner/pilot changed the oil and filter prior to the formal 50-hour inspection by a private contractor. The inspection form revealed no specific inspection of the retainer plates are required except for a general condition inspection of the engine, accessories, and of the fluid systems for leaks.

Flight

Event TypeAccident
Event Time12:43 PDT
Nearest AirportRiverside Municipal (0nm)
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftEnstrom F-28-F
Tail NumberN99YC
Aircraft CategoryHeli
DamageSubstantial
OperatorStits Aircraft
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360-F1AD · Reciprocating · 205
Seats3

People & Injuries

Injury Summary3 injuries (3 minor injuries)
Fatal0
Serious0
Minor3
Uninjured0
Total3
Crew 1Age 76 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind300° @ 9 kt
Visibility4 sm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0
Observation Time19:47
Weather SourceWFAC

Appendix: Source Data