
Catalog excerpts

LACK OF CLADDING IN METALLIC COMPONENTS Qualified according to NTM 51-10-30 & AITM 6-6002 for detection of cladding removal S GO/ NO GO device S Thickness range: 1.3 mm to 5.3 mm S Material: Aluminium alloy S Paint thickness: from 0 pm to 350 pm S Applicable to all Airbus programs NDT technique: Measurement of remaining cladding thickness by high frequency eddy current testing after blending out CLADTOOL KIT S Base: "Smart UE1" instrument S Included accessories: - 2 probes (1 pencil + 1 flat), reference block (AI2024 with and without clad), scanning frame - 2 probe holders READY to detect clad missing. REDO a ZERO when you change fuselage area. airbus groi
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STEP BY STEP SIMPLIFIED INTERFACE Probe: selection & automatic setup Automatic calibration and checking device on the reference block Automatic balancing of the device near the blend out Scanner: to assess 100 % surface coverage AUTOMATIC DETECTION Present or missing clad on the fuselage indicated by a simple LED - RED: No CLAD + Sound ALARM - GREEN: presence of CLAD Coupling monitoring with a LED and lift-off sound alarm. contact us to know more AN airbus group company contact@testia.com www.t
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