ST8870-1

Custom 5 m hz 45° transverse wave transducer with end mount microdot connector.

Includes: Test report and certificate of conformance.

Reference: AIRBUS A300-600 PART 4 54-50-15

Description

BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 20 FIGURE 7. GR/EP SKIN/NOMEX CORE DISBOND DEFECT