Matches in DBpedia 2016-04 for { ?s ?p "Blade inspection method is a system to detect cracks in the main rotor blades. The method involved pressurizing the interior cavity of the rotor blades. If a crack is present, pressure is lost and a red indicator on the rotor blade root end was tripped. Later, the BIM system was connected to a cockpit display. BIM allowed only flawed rotor blades to be swapped out. This method has been used on Sikorsky's S-61 series and some later helicopter models."@en }
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- Blade_inspection_method abstract "Blade inspection method is a system to detect cracks in the main rotor blades. The method involved pressurizing the interior cavity of the rotor blades. If a crack is present, pressure is lost and a red indicator on the rotor blade root end was tripped. Later, the BIM system was connected to a cockpit display. BIM allowed only flawed rotor blades to be swapped out. This method has been used on Sikorsky's S-61 series and some later helicopter models.".
- Q4923717 abstract "Blade inspection method is a system to detect cracks in the main rotor blades. The method involved pressurizing the interior cavity of the rotor blades. If a crack is present, pressure is lost and a red indicator on the rotor blade root end was tripped. Later, the BIM system was connected to a cockpit display. BIM allowed only flawed rotor blades to be swapped out. This method has been used on Sikorsky's S-61 series and some later helicopter models.".
- Blade_inspection_method comment "Blade inspection method is a system to detect cracks in the main rotor blades. The method involved pressurizing the interior cavity of the rotor blades. If a crack is present, pressure is lost and a red indicator on the rotor blade root end was tripped. Later, the BIM system was connected to a cockpit display. BIM allowed only flawed rotor blades to be swapped out. This method has been used on Sikorsky's S-61 series and some later helicopter models.".
- Q4923717 comment "Blade inspection method is a system to detect cracks in the main rotor blades. The method involved pressurizing the interior cavity of the rotor blades. If a crack is present, pressure is lost and a red indicator on the rotor blade root end was tripped. Later, the BIM system was connected to a cockpit display. BIM allowed only flawed rotor blades to be swapped out. This method has been used on Sikorsky's S-61 series and some later helicopter models.".