Abstract: A tool mountable on a helicopter blade for selectively bending the trailing edge trim tab of the blade about a selected axis along the span of the trim tab, and including a device to counterbalance the weight of the trim tab bending mechanism so that the true degree of bending of the trim tab can be determined at any time during the bending operation. The tool also includes apparatus for simultaneously calibrating the counterbalance device and the mechanism used to measure the degree to which the tab has been bent, prior to commencing the bending operation.

Abstract: A work stand for rotably mounting an engine thereon during the initial construction of the engine, or for repair of the engine, includes two concentric rings which are disposed in upstanding relationship and are mounted on a base. The inner ring is rotably mounted within the outer ring and includes a plurality of axially extending arms which engage the engine. The latter is mounted in a generally horizontal disposition and is rotable with the inner ring whereby access to the engine is unobstructed from either the top or bottom of the engine, as well as along the entire length of the engine. A locking mechanism is provided between the inner and outer rings of the work stand for maintaining the engine at the desired angular attitude, and the engine is mounted such that its center of gravity is disposed adjacent the upstanding planes of the concentric rings.