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NTSB Report

June 13, 2008 · Schweizer 269C · N54LC

Cedar Valley, UT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 13, 2008
Injury Outcomes
1 injury (1 minor injury)
Location
Cedar Valley, UT
Aircraft
Schweizer 269C
Tail Number
N54LC
Operator
Amw Aerospace
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
LAX08CA178

The pilot reported that the purpose of the flight was to demonstrate the helicopter's performance at an air show. He traveled from overseas by scheduled airline, arriving 2 days before the air show. The day before the air show he flew the helicopter for 50 minutes of demonstration practice at a similar density altitude to that anticipated for the following day's performance. The accident flight began about 1315, and the first two maneuvers were completed without incident. The third maneuver was "a standard 180-degree 'wing-over' commenced from a standard 300 feet." According to the pilot, the helicopter "failed to fully recover from the descent phase of the maneuver and struck the surface at approximately 40-50 knots." The helicopter rolled onto its left side. The pilot reported that the density altitude at the time of the accident was 8,500 feet. He stated that the accident could have been prevented "possibly by greater awareness and practice at the local density altitude conditions."

NTSB Probable Cause

The pilot's failure to maintain terrain clearance while maneuvering. A contributing factor was the high density altitude.

Full Narrative

The pilot reported that the purpose of the flight was to demonstrate the helicopter's performance at an air show. He traveled from overseas by scheduled airline, arriving 2 days before the air show. The day before the air show he flew the helicopter for 50 minutes of demonstration practice at a similar density altitude to that anticipated for the following day's performance. The accident flight began about 1315, and the first two maneuvers were completed without incident. The third maneuver was "a standard 180-degree 'wing-over' commenced from a standard 300 feet." According to the pilot, the helicopter "failed to fully recover from the descent phase of the maneuver and struck the surface at approximately 40-50 knots." The helicopter rolled onto its left side. The pilot reported that the density altitude at the time of the accident was 8,500 feet. He stated that the accident could have been prevented "possibly by greater awareness and practice at the local density altitude conditions."

Flight

Event TypeAccident
Event Time13:20 MDT
Nearest AirportWest Desert Airpark (0nm)
Runway17
Runway Length2600 ft
Runway Width40 ft
Flight Plan FiledNone
Aircraft FireNo

Aircraft

AircraftSchweizer 269C
Tail NumberN54LC
Aircraft CategoryHeli
DamageSubstantial
OperatorAmw Aerospace
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360 · Reciprocating

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 75 · First Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility15 sm
CeilingNone
Temperature / Dew Point28 C
Altimeter30.23 inHg
Observation Time19:49
Weather SourceWFAC

Appendix: Source Data