Accession Number:

ADA300964

Title:

U.S. Navy T-45A Departure and Spin Evaluation.

Descriptive Note:

Professional paper,

Corporate Author:

NAVAL AIR WARFARE CENTER AIRCRAFT DIV PATUXENT RIVER MD

Personal Author(s):

Report Date:

1995-08-03

Pagination or Media Count:

17.0

Abstract:

U.S. Navy T-45A departure and spin evaluation was conducted from 8 July to 30 September 1994. The initial T-45A flight manual departure and spin recovery procedures evaluated proved unsatisfactory in providing consistent recoveries from inverted spin modes. Specifically, the procedures allowed the rudder to blow-out in the pro-spin direction during recovery, resulting in spin mode transitions and delayed recoveries. Furthermore, a third sustained inverted spin mode was discovered during flight tests. The initial flight manual procedures were successfully modified to reduce the occurrence of rudder blow-out during recovery attempts and provided more consistent recovery characteristics.

Subject Categories:

  • Training Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE