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Aviation safety reports, made easier to study

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November 5, 2005 · Hughes 269A · N1020Q

Omaha, NE

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
November 5, 2005
Injury Outcomes
No injuries (2 uninjured)
Location
Omaha, NE
Aircraft
Hughes 269A
Tail Number
N1020Q
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CHI06CA029

The helicopter was damaged during landing following a reported loss of engine power. The pilot reported that while on approach to hover, the engine lost power as he was passing through 60 feet above ground level. He stated that he "pulled back on the stick to slow down and enter autorotation, and began to roll off the throttle and lower the collective." He further stated; "Almost immediately I felt the power come up and the needles joined accompanied by the aircraft yawing. I attempted to apply power and recover but my rate of descent and altitude along with the adverse yaw complicated my recovery." The helicopter subsequently impacted the ground and slid to a stop. Postaccident examination of the helicopter failed to reveal any pre-impact anomalies.

NTSB Probable Cause

The loss of engine power for an undetermined reason and the pilot's improper execution of the emergency procedure which resulted in an excessive descent rate and subsequent hard landing.

Full Narrative

On November 5, 2005, about 1445 central standard time, a Hughes 269A helicopter, N1020Q, piloted by an airline transport pilot, sustained substantial damage during landing following a reported loss of engine power. The helicopter was on approach to land on runway 30 (3,801 feet by 75 feet, concrete), at the Millard Airport, Omaha, Nebraska, when the loss of power occurred. The 14 CFR Part 91 personal flight was operating in visual meteorological conditions without a flight plan. The pilot and passenger were not injured. The local flight originated about 1440. The pilot held an airline transport certificate with a rating for multi-engine land airplanes. The certificate also listed commercial priveledges for Rotorcraft-Helicopter and Instrument Helicopter ratings. The pilot reported that while on approach to hover, the engine lost power as he was passing through 60 feet above ground level. He stated that he "pulled back on the stick to slow down and enter auto rotation, and began to roll off the throttle and lower the collective." He further stated; "Almost immediately I felt the power come up and the needles joined accompanied by the aircraft yawing. I attempted to apply power and recover but my rate of descent and altitude along with the adverse yaw complicated my recovery." The helicopter subsequently impacted the ground and slid to a stop. Postaccident examination of the helicopter failed to reveal any pre-impact anomalies.

Flight

Event TypeAccident
Event Time14:45 CST
Nearest Airport0nm
Flight Plan FiledNone
Aircraft FireNo

Aircraft

AircraftHughes 269A
Tail NumberN1020Q
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HO-360 · Reciprocating · 180

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 48 · None · Minor

Conditions

ConditionsVMC
LightDaylight
WindCalm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0

Appendix: Source Data