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NTSB Report

September 3, 2007 · Hughes 269C · N58332

Ramona, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 3, 2007
Injury Outcomes
1 injury (1 minor injury), 1 uninjured
Location
Ramona, CA
Aircraft
Hughes 269C
Tail Number
N58332
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
LAX07CA267

The helicopter landed hard during performance of a practice autorotation during the instructional flight. The certified flight instructor indicated that the engine lost power after the student initiated the autorotation about 800 feet above the designated dirt field, whereupon the instructor took the controls. The instructor misjudged the landing flare, the helicopter bounced, and it yawed left 90 degrees before coming to rest on its skids. The helicopter's tail boom was broken from the fuselage, and the main rotor blades were bent. Following the helicopter's recovery its engine was run up and the control system was examined. The engine and control system operated normally, and no evidence was found of any malfunction.

NTSB Probable Cause

a loss of engine power for undetermined reasons.

Full Narrative

On September 3, 2007, about 1015 Pacific daylight time, a Hughes 269C, N58332, touched down hard during a practice autorotation about 7 miles north of Ramona, California. The helicopter was operated by Civic Helicopters, Inc., Carlsbad, California, and it was substantially damaged. The commercial pilot held a certified flight instructor (CFI) certificate, and he was not injured. The student pilot held a private pilot certificate (airplanes), and he received minor injuries. Visual meteorological conditions prevailed at the time of the instructional flight, and no flight plan had been filed. The flight was performed under the provisions of 14 CFR Part 91, and it originated from Carlsbad about 1000. In pertinent part, the CFI reported to the National Transportation Safety Board investigator that he planned to practice autorotations with his student. The CFI observed that the engine lost power after the student initiated the autorotation about 800 feet above the designated dirt field. The CFI took the controls and the helicopter descended. The CFI indicated that the helicopter touched down hard and bounced. The helicopter yawed left 90 degrees before coming to rest on its skids. The helicopter's tail boom was broken from the fuselage, and the main rotor blades were bent. Following the helicopter's recovery the operator reported to the Safety Board investigator that its engine and control system were examined. The engine was run up. No evidence of any mechanical malfunction was observed. The engine and control system operated normally, according to the operator.

Flight

Event TypeAccident
Event Time10:15 PDT
Nearest Airport0nm
Flight Plan FiledNone
Aircraft FireNo

Aircraft

AircraftHughes 269C
Tail NumberN58332
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360-D1A · Reciprocating

People & Injuries

Injury Summary1 injury (1 minor injury), 1 uninjured
Fatal0
Serious0
Minor1
Uninjured1
Total2
Crew 1Age 55 · Second Class · None
Crew 2Second Class · Minor

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data