Accident Pitts S-1S N2HT,
ASN logo
ASN Wikibase Occurrence # 43228
 
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:Sunday 4 August 1996
Time:18:37 LT
Type:Silhouette image of generic PTS1 model; specific model in this crash may look slightly different    
Pitts S-1S
Owner/operator:Clarence A. Speal
Registration: N2HT
MSN: 1-0014
Total airframe hrs:1255 hours
Engine model:Lycoming IO360-B4A-MOD
Fatalities:Fatalities: 1 / Occupants: 1
Aircraft damage: Destroyed
Category:Accident
Location:Pittsburgh, PA -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Unknown
Departure airport:, PA (KAGC)
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot received clearance into the approved airshow aerobatic airspace, and initiated his first maneuver, a double snap roll. A video tape of the maneuver showed a deformation of the lower left wing within seconds of initiation of the maneuver. This was followed by a failure of the left outboard portion of the upper wing. Both the failed lower left wing and the failed upper left outboard portion of the top wing displaced aft against the empennage. The video then captured the airplane in a descent until water impact in an inverted attitude. According to witnesses, the pilot utilized airspeeds greater than the manufacturer's recommended maneuvering airspeeds. Witnesses also reported seeing the 'g' meter in the cockpit at higher positive and negative readings than recommended by the manufacturer. The pilot had voiced his concern about the airplane's wings because of flutter he experienced during recent flights.

Probable Cause: The pilot's utilization of airspeeds greater than the manufacturer recommended maneuvering airspeeds which exceed the design limits of the airplane and resulted in the subsequent failure of the wing spar.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: IAD96FA126
Status: Investigation completed
Duration: 1 year and 7 months
Download report: Final report

Sources:

NTSB IAD96FA126

Location

Revision history:

Date/timeContributorUpdates
24-Oct-2008 10:30 ASN archive Added
21-Dec-2016 19:24 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
09-Apr-2024 05:09 ASN Update Bot Updated [Time, Operator, Other fatalities, Departure airport, Source, Narrative, Category, Accident report]

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