WPR13CA337

NTSB accident investigation · Hughes 269B · Lewiston, ID · July 23, 2013

Accident · No injuriesData collectionFinal report
Date
July 23, 2013, 11:34 local (18:34 UTC)
Place
Lewiston, ID
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Emergency descent
Aircraft
N9484FHughes 269B
Defining event
Autorotation: Hard landing
Weather
Visual (VMC) · Day
Status
Completed · report October 21, 2013
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Administration
FAA report
20130723014809A
Case key
87552

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

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Probable cause

The pilot's incorrect application of the cyclic control during the landing.

Findings · 2

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.

Action: incorrect action performancePersonnel issues › Action/decision · PilotHughes 269B: 1 caseAll aircraft: 1,386 casesProbable cause
Use of equip/info: aircraft controlPersonnel issues › Task performance · PilotHughes 269B: 5 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 pilot stated that he was conducting a full down practice autorotation which involved landing the helicopter as the final step. During the landing, the helicopter bounced which resulted in the main rotor striking the tail boom, severing the tail rotor drive shaft. The pilot stated that the accident could have been prevented if he had applied more forward cyclic after the helicopter had contacted the ground. The pilot reported no preimpact mechanical malfunctions or failures that would have precluded normal operation.

Factual narrative

The pilot stated that he was conducting a full down practice autorotation which involved landing the helicopter as the final step. During the landing, the helicopter bounced, which resulted in the main rotor striking the tail boom, severing the tail rotor drive shaft. The pilot stated that the accident could have been prevented if he had applied more forward cyclic after the helicopter had contacted the ground. The pilot reported no preimpact mechanical malfunctions or failures that would have precluded normal operation.

Aircraft

Registration
N9484F
Reported as
Hughes 269B
Category
Helicopter
Serial number
1160291
Airframe hours
3,883
Engine
Lycoming IO360 SER, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Odonata LLC
Registered owner
Simmons Kent B
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · March 11, 2013
Departed
KLWS · Lewiston, ID
Destination
KLWS · Lewiston, ID
Airport
KLWS · Lewiston-Nez Perce County Airp, runway 30, 5,000 × 100 ft, asphalt

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
33
Injuries
None
Certificates
Commercial, Flight instructor
Medical
Class 2, Without waivers/limitations
Last flight review
May 19, 2012
Seat
Left
Flight hours
241 total · 73 in this make and model · 11 in the last 90 days · 8 in the last 30 days · 0 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
90 °F, dew point 43 °F
Altimeter
29.97 inHg
Observed at
KLWS

Docket · 1

The files NTSB released with the investigation on September 26, 2013, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.4 MB in all.

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 N9484F · 2

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