CLADTOOL

Product catalog summary

Lack of Cladding in Metallic Components

This document outlines the specifications and procedures for detecting the removal of cladding in metallic components, specifically for Airbus programs. The detection is qualified according to NTM 51-10-30 & AITM 6-6002 standards.

Specifications:

Device Type: GO/NO GO device
Thickness Range: 1.3 mm to 5.3 mm
Material: Aluminium alloy
Paint Thickness: 0 μm to 350 μm

Non-Destructive Testing (NDT) Technique:

The technique involves measuring the remaining cladding thickness using high-frequency eddy current testing after blending out.

CLADTOOL KIT Components:

Base Instrument: "Smart UE1"
Accessories: 2 probes (1 pencil, 1 flat), reference block (Al2024 with and without clad), scanning frame, 2 probe holders
Features: Automatic probe selection and setup, automatic calibration and checking on the reference block, automatic balancing near blend out, 100% surface coverage scanner
Indicators: LED for clad presence (RED for no clad with sound alarm, GREEN for presence of clad), coupling monitoring with LED and lift-off sound alarm

User Interface:

The device features a step-by-step simplified interface with automatic detection capabilities.

Contact Information:

For more information, contact Testia at [email protected] or visit www.testia.com.

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 [email protected] www.t

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