INSTALLED SYSTEMS FUNCTIONAL TEST PROCEDURE.
GENERAL ELECTRIC CO CINCINNATI OHIO ADVANCED ENGINE AND TECHNOLOGY DEPT
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The purpose of these tests is to demonstrate that the XV-5A aircraft systems function in accordance with the design requirements. The testing procedure is divided into 12 major tests. The order of appearance is the desired chronological order. When the aircraft is received for functional tests, the hydraulic and pneumatic systems will have been flushed, filled and bled in accordance with Ryan Report 14359-6. The controls will have been rigged in accordance with Ryan Report 14395-5. Author
- Research and Experimental Aircraft