1339. Test Procedures Used in Determining Aircraft Suitability for STAN* Integral Weight and Balance System
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Paper
1339. Test Procedures Used in Determining Aircraft Suitability for STAN* Integral Weight and Balance System. 1980.
Abstract
Prior to Fairchild committing to produce a STAN Integral Weight and Balance System for a new aircraft type, it is necessary for us to conduct extensive testing of a minimum of two aircraft of the type to be equipped. Such testing is described in detail including the use of Peak Pressure, Averaging Tests and Taxi Tests. Actual examples of recent tests conducted wi l l be used to illustrate the data formats used and the data obtained.
