Description
BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 19 FIGURE 6. GR/EP SKIN/NOMEX CORE DISBOND DEFECT
ST8870-4
ST8870-4
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
