Lack of Cladding with HF EC in Metallic Components.
■ GO/ NO GO device.
■ Thickness fuselage range : 1.3mm to 5.3mm.
■ Material Aluminium 2024.
■ Paint thickness : 0 μm < paint thickness < 350μm thickness.
■ Applicable to all programs.
NDT technique: Measurement of remaining cladding thickness by high frequency eddy current after blending following AITM6-6002 issue 2.
Referenced in the NTM 51-10-30 procedure
■ Same UE1 packaging.
■ All included : Smart UE1,
– 2 probes (pencil and flat probe), Reference block (Al2024 with and without Clad), scanner
– 2 holder probes.
Step by Step Simplified Gui
■ 2 probes: automatic setup (same process for the two probes).
■ Calibration: automatic calibration and checking devise with two areas with and without clad on reference block.
■ Only one button: balancing the device near the blend out.
■ Scanner: to check on large blend out.
■ Calibration on the reference block.
■ Simple steps.
■ Same process for the 2 two probes.
■ On presence Clad area.
■ On Clad missing area.
■ Presence or missing clad on the fuselage indicate by a simple LED :
– RED : No CLAD + Sound ALARM
– GREEN : presence of CLAD
■ Good coupling with a LED and sound alarm lift off