ASN Wikibase Occurrence # 69790
Last updated: 20 April 2014
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
Narrative:Before takeoff, the pilot installed the wings and tail on the glider. During the takeoff, just after the glider became airborne, it pitched up vertically. After the tow rope was released the nose dropped, and the glider impacted the ground. Examination of the glider revealed that the control cables were rigged in reverse and the elevator control bell-crank located in the aft end of the fuselage was installed inverted from its normal position. About 8 days prior to the accident an airframe and powerplant mechanic with inspector authorization performed an annual inspection which included a statement, 'AC assembled and rigged.' At that time, the complete elevator assembly was not installed. The pilot completed the elevator installation after the annual inspection. Prior to the flight, the pilot was asked by a witness if he had performed a 'positive control check' of the primary flight controls, which the pilot stated 'yes.'
|Type:||Schweizer SGS 1-26A|
|C/n / msn:|| |
|Fatalities:||Fatalities: 0 / Occupants: 1|
|Airplane damage:|| Substantial|
|Location:||Fairfield, PA -
United States of America
|Phase:|| Take off|
|Departure airport:||Fairfield, PA|
|Destination airport:||Fairfield, PA|
NTSB Identification: NYC98LA011
Number of views: 624