Incident Pitts S-1S G-TAYL,
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ASN Wikibase Occurrence # 178861
 
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Date:Saturday 5 July 2014
Time:13:15 LT
Type:Silhouette image of generic PTS1 model; specific model in this crash may look slightly different    
Pitts S-1S
Owner/operator:Private
Registration: G-TAYL
MSN: 20940
Year of manufacture:1981
Engine model:Lycoming AEIO-360-B4A
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Location:Perth/Scone Airfield, Perh, Tayside, Scotland -   United Kingdom
Phase: Approach
Nature:Private
Departure airport:Perth/Scone Airfield, Scotland (EGPT/PSL)
Destination airport:Perth/Scone Airfield, Scotland (EGPT/PSL)
Investigating agency: AAIB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
Substantially damaged (see pictures below) when crashed (side slipped) and went out of control on approach to Perth/Scone Airfield, Perth, Tayside, Scotland, on 5/7/2014. According to the following synopsis from the official AAIB report into the accident:

"The pilot was on his second flight in a Pitts Special. Because visibility of the landing area during the approach is not good in this type of aircraft, he flew an approach in which his initial aiming point was about a third of the way along the runway and, when certain of reaching the airfield, side-slipped the aircraft to steepen the approach and bring the touchdown point closer to the threshold.

The accident occurred when the pilot stopped the side-slip and flared the aircraft for landing. The rate of descent was too high and the flare did not prevent the aircraft from hitting the ground hard. The undercarriage collapsed, allowing the propeller to strike the ground, and the aircraft ground looped before stopping. The pilot, who was uninjured, made the aircraft safe and vacated it normally. There was no fire.

The pilot considered that he did not maintain sufficient airspeed whilst side-slipping, so the flare did not arrest the high rate of descent. He thought that the energy absorbing seat foam and using a seven-point harness had prevented injury"

Damage sustained to G-TAYL: Landing gear, propeller, wing tip and wing fabric damaged

Accident investigation:
cover
  
Investigating agency: AAIB
Report number: EW/G2014/07/21
Status: Investigation completed
Duration:
Download report: Final report

Sources:

1. https://assets.digital.cabinet-office.gov.uk/media/548b0f17e5274a42900002df/Pitts_Special_S-1S_G-TAYL_12-14.pdf
2. http://www.caa.co.uk/aircraft-registration/

Revision history:

Date/timeContributorUpdates
21-Aug-2015 14:03 Dr. John Smith Added
21-Aug-2015 23:42 Dr. John Smith Updated [Time, Aircraft type]

Corrections or additions? ... Edit this accident description

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