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May 29, 2007 · Hughes 269A · N63HD

Las Piedras, PR

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 29, 2007
Injury Outcomes
2 injuries (1 serious injury, 1 minor injury)
Location
Las Piedras, PR
Aircraft
Hughes 269A
Tail Number
N63HD
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
MIA07CA103

The pilot stated that he took off from his home airstrip, and during the initial climb at 350 feet and 55 mph, the engine quit. At the time there were power lines in front of him so he opted to make a left 90-degree auto rotation. The helicopter was landed hard causing damage to the tail boom of the helicopter. The passenger stated that about 40 seconds after takeoff, he heard a "pop pop" noise. The aircraft started a fast descent and impacted the ground. His injuries include a burst L1 vertebra. Examination of the helicopter was performed by an FAA airworthiness inspector, which revealed the engine was turned by hand without binding. The aircraft's spark plugs were in good condition and the fuel filter was clean and non-obstructed; fuel was noted in the filter. The flight controls were found to be free and moving. No anomalies with the aircraft or engine were reported by the FAA inspector. Inspection of the aircraft's logbooks revealed that the last annual inspection was performed on June 01, 1997.

NTSB Probable Cause

The failure of the non-certificated pilot to maintain a proper rate of descent during the autorotative landing following a reported loss of engine power for undetermined reasons, resulting in a hard landing.

Full Narrative

The non-certificated pilot stated he took off from his home and during the initial climb at 350 feet and 55 mph, the engine quit. At the time there were power lines in front of him so he opted to make a left 90-degree auto rotation. The helicopter was landed hard causing damage to the tail boom of the helicopter. The passenger stated that about 40 seconds after takeoff, he heard a "pop pop" noise. The aircraft started a fast descent and impacted the ground. His injuries include a burst L1 vertebra. Examination of the helicopter was performed by an FAA airworthiness inspector, which revealed the engine was turned by hand without binding. The aircraft's spark plugs were in good condition and the fuel filter was clean and non-obstructed; fuel was noted in the filter. The flight controls were found to be free and moving. No anomalies with the aircraft or engine were reported by the FAA inspector. Inspection of the aircraft's logbooks revealed that the last annual inspection was performed on June 01,1997.

Flight

Event TypeAccident
Event Time08:15 AST
Nearest AirportBOQUERON (1nm)
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftHughes 269A
Tail NumberN63HD
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO-360 SER · Reciprocating
Seats2

People & Injuries

Injury Summary2 injuries (1 serious injury, 1 minor injury)
Fatal0
Serious1
Minor1
Uninjured0
Total2
Crew 1Age 57 · None · Minor

Conditions

ConditionsVMC
LightDaylight
Wind4 kt
Visibility10 sm
CeilingNone
Altimeter29.95 inHg
Weather SourceWFAC

Appendix: Source Data