Loss of control Accident Hughes 269C N9679F,
ASN logo
ASN Wikibase Occurrence # 146930
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Tuesday 24 July 2012
Time:19:00
Type:Silhouette image of generic H269 model; specific model in this crash may look slightly different    
Hughes 269C
Owner/operator:Private
Registration: N9679F
MSN: 310103
Year of manufacture:1971
Total airframe hrs:2393 hours
Engine model:Lycoming HIO-360-D1A
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:4550 35th Street North, Lealman, St. Petersburg, FL -   United States of America
Phase: Take off
Nature:Private
Departure airport:St. Petersburg, FL
Destination airport:St. Petersburg, FL
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
According to the pilot, the helicopter's last annual inspection had been completed 12 years prior to the accident. On the day of the accident, he decided to fly it to lubricate the parts. After liftoff, he brought the helicopter to a hover about 25 feet in the air and initiated some pedal turns. The nose of the helicopter then began to drift toward the right. He applied left pedal but the helicopter didn’t respond. The helicopter then circled 6 to 8 times, so the pilot lowered the collective, and the helicopter impacted the ground on the left skid, struck a fence, and then rolled over on its left side.

However, according to witnesses, the helicopter was about 50 feet in the air, did not circle but moved side to side, and was described as being out of control before it impacted the ground. Total flight time from liftoff to impact was about 2 minutes in duration. Postaccident examination did not reveal any preimpact failures or malfunctions of the helicopter which would have precluded normal operation. However, the cyclic control system would not move freely because the lateral friction control was tightened down. Once the lateral friction control was released, lateral movement of the cyclic control was possible.
Probable Cause: The pilot's failure to assure that the lateral friction control was released prior to flight.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ERA12LA477
Status: Investigation completed
Duration: 1 year
Download report: Final report

Sources:

NTSB
FAA register: 2. FAA: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=9679F

Location

Revision history:

Date/timeContributorUpdates
25-Jul-2012 23:03 Geno Added
13-Feb-2016 20:20 Dr.John Smith Updated [Time, Operator, Location, Source, Narrative]
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
27-Nov-2017 20:57 ASN Update Bot Updated [Operator, Other fatalities, Departure airport, Destination airport, Source, Narrative]

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org