DFW08CA120

NTSB accident investigation · Hughes 269A · Lincoln, NE · April 27, 2008

Accident · No injuriesData collectionFinal report
Date
April 27, 2008, 13:00 local (18:00 UTC)
Place
Lincoln, NE
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N1020QHughes 269A
Defining event
Maneuvering: Collision with terr/obj (non-CFIT)
Weather
Visual (VMC) · Day
Status
Completed · report May 28, 2008
Report
Approved by Office Director
Parties
FAA FSDO
FAA report
20080427833159A
Case key
67896

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

The pilot's failure to properly execute a steep approach, which resulted in a tail strike and a loss of control.

Findings · 1

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Use of equip/info: aircraft controlPersonnel issues › Task performance · PilotHughes 269A: 9 casesAll aircraft: 9,295 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The commercial rated pilot was practicing a steep approach in a single-engine helicopter, when she flared too low to the ground and the tail rotor struck the ground. Subsequently, the tail rotor drive shaft failed and the pilot was unable to maintain control of the helicopter. The rear portion of the right skid contacted the ground and the helicopter rolled over on to its side. Examination of the helicopter revealed it sustained substantial damage to the mast, tail boom, and the right skid was torn from the fuselage.

Factual narrative

The 35-year-old commercial rated pilot was practicing a steep approach in a single-engine helicopter, when she flared too low to the ground and the tail rotor struck the ground. Subsequently, the tail rotor drive shaft failed and the pilot was unable to maintain control of the helicopter. The rear portion of the right skid contacted the ground and the helicopter rolled over on to its side. Examination of the helicopter revealed it sustained substantial damage to the mast, tail boom, and the right skid was torn from the fuselage.

Aircraft

Registration
N1020Q
Reported as
Hughes 269A
Category
Helicopter
Serial number
115-0426
Engine
Lycoming IO-360, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Chandra Clanton
Registered owner
Advanced Air Incorporated
Airworthiness certificate
Standard, Normal
Departed
NONE · Lincoln, NE

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
35
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2
Seat
Right
Flight hours
1,672 total · 23 in this make and model · 30 in the last 90 days · 19 in the last 30 days

Weather

Conditions
Visual (VMC) · Day

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N1020Q · 1

Matched to the same aircraft by N-number and date.