Description
AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PROCEEDURE 1, FIGURE 11, PAGE 15 ALUMINUM 2014-T6 CONDUCTIVITY RANGE 35-40 IACS.. Includes Test Report and Certificate of Conformance.
AFNDT-2008/F
AFNDT-2008/F
$410.00
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
