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Application Reference Chart



  Laser Application Reference Chart
-
Shearography
Holography
Thermography


Stress Method  

 

Application

 COMPOSITES MATERIAL
Solid Laminates
X
X
.
.
.
.
.
Fiberglass
X
X
.
.
.
.
.
Fiber Reinforced Plastics
X
X
.
.
.
.
.
Impact Damage
X
X
.
.
.
.
.
Panel Repairs
X
X
.
.
.
.
.
Face Sheet Delamination
X
X
.
.
.
.
X
Composite Spar
X
X
.
.
.
.
.
Disbonds
X
X
.
.
.
.
X
RMS Composite Booms
X
.
.
.
.
.
.
Bullnose Radome
X
X
.
.
.
.
.
Composite Building Structure
X
X
.
.
.
.
.
FOD in Laminates
X
X
.
.
.
.
.
 HONEYCOMB
Composite Core Splice Joints Defects
X
X
.
.
.
.
.
Composite Honeycomb
X
X
.
.
.
.
.
Metalic Honeycomb
X
X
.
.
.
.
.
Foam Core Honeycomb
X
X
.
.
.
.
.
Aluminum Honeycomb
X
X
.
.
.
.
.
Multi Core Foam Core
X
X
.
.
.
.
.
Crushed Core
X
X
.
.
X
.
.
Metal to Metal Honeycomb
X
X
.
.
X
.
.
Adhesive Bonds
X
X
.
.
.
.
.
Far Skin to Core Disbond
X
X
.
.
.
.
.
Near Skin to Core Disbond
X
X
.
.
.
.
.
Honeycomb Engine Fan Case
X
X
.
.
.
.
.
Graphite Face Sheet w/ Nomex Core
X
X
.
.
.
.
.
 AEROSPACE
Airbus A330 Composite
X
X
.
.
.
.
.
Boeing 757 Spoiler
X
.
.
.
.
.
.
Cryogenic Fuel Tank
X
X
.
X
.
.
.
Pressure Cylinders
X
X
.
X
.
.
.
Rocket Motors
X
.
.
.
X
.
.
Brazed Honeycomb Seals
.
.
.
.
.
M.V.
.
Feltmetal and Plasma Spray Adradable Seals
.
.
.
.
.
M.V.
.
Jet Engine Fan Case
.
.
X
.
.
.
.
Filament Wound Bottles
X
X
.
X
.
.
.
Helicopter Rotor Blades
X
X
.
.
.
.
X
Disbond Under Erosion Strip
X
.
.
.
.
.
.
Tail Rotor Blade
X
X
.
.
.
.
X
Main Rotor Blade
X
X
.
.
.
.
X
 MARINE
Super Yacht Fiberglass Hull
X
X
.
.
.
.
.
Stealth All Composite Ship
X
X
.
.
.
.
.
 BONDING
Aluminum to Aluminum
.
X
.
.
X
M.V.
.
Brazed Metalics
X
X
.
.
X
M.V.
.
Spray On Foam Insulation (SOFI)
X
.
.
.
X
.
.
Bonded On Foam Insulation (SOFI)
X
.
.
.
X
.
.
Bonded Coatings
X
X
.
.
.
.
.
Elastometric Structures
X
X
.
.
.
.
.
Fiberglass Core & Foam Adhesive
X
X
.
.
.
.
.
Aluminum Core to Aluminum Skin
X
X
.
.
.
M.V.
.
 MILITARY
F18 External Fuel Tank
X
X
.
.
.
.
.
F100 Engine Fan Case
X
X
X
.
.
.
.
F117 Compressor Stator
X
.
.
.
.
.
.
KC135 Flap
X
.
.
.
.
.
.
Global Hawk Chin Fairing
X
X
.
.
.
.
.
AWACS Roto Dome
X
X
.
.
.
.
.
Delta IV SOFI TPS
.
.
.
.
X
.
.
BS Engine Inlet, Flaps, Elerons
..
X
.
.
.
.
.
BS Bomb Bay Doors
.
X
.
.
.
.
.
Aircraft Tires
.
X
.
.
.
.
.
Radome
X
X
.
.
.
.
.
Rotodome
X
X
.
.
.
.
.
 MEDICAL & ELECTRONIC
Human Hip & Knee Implants
.
.
X
.
.
M.V.
.
Multilayer Circuit Board
.
X
.
.
.
.
.
Leak Testing of Sealed Electronic Packages
.
.
.
.
.
P.
.
Note: The stress method marked is a suggested recommended method more likely to be effective in the shearography test and which is dependant on the part configuration.

 

Download a Printable Application Reference Chart (PDF File)

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