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