T-38A FLAMEOUT EVALUATION
Abstract
The results of a test program to develop a flameout emergency landing pattern for the T-38 aircraft are presented. This was accomplished by preliminary tests, actual double engine flameout landings, and control surface rate tests to verify the slow response rates noted during the deadstick landings. The results of these tests indicate that a deadstick landing is not advisable. It is recommended that a pilot eject from the aircraft rather an attempt a deadstick landing. If a deadstick landing capability is required, it is recommended that a battery powered hydraulic backup pump be incorporated in the aircraft and the flameout landing pattern developed during this program be used. Airstart capability in a double engine flameout condition is satisfacry. Aircraft systems operation is satisfactory for deadstick glides to suitable airstart altitudes or to a safe ejection area. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1961
- Accession Number
- AD0265390
Entities
People
- Norris J. Hanks
- Robert W. Sudderth
Organizations
- Air Force Test Center