Abstract: A method, computer program, or apparatus for determining with various degrees of precision the power delivered by an engine and also the best possible power of the engine for the given operating conditions. Typically, this invention is for an aircraft engine. The disclosed invention uses a variety of parameters, such as the rotation rate, manifold pressure, outside air temperature, and fuel flow to calculate or approximate the power delivered by the engine and the best power available from the engine. The engine's altitude does not have to be involved in the calculations. Display of the calculated engine power is provided relative to best power and/or maximum engine power.

Abstract: Provided herein is a description of an open-loop gift card system and method.

Abstract: An integrated card system providing multiple payment and loading mechanisms is provided herein.

Abstract: A dual card package having cards secured within. A first panel of the package includes an access flap that is pivotal about a fold line. A second panel is also foldable along a fold line substantially corresponding to the fold line of the access flap. One card is accessible by the access flap so that the package is selectively movable from a closed position in which an magnetic strip on the card is covered and an open position in which the access flap and the second panel is swung out from the card such that the magnetic strip is exposed for activation purposes.

Abstract: The present invention provides an ACH compatible loadable debit card system and method.

Abstract: The present invention provides a network access system and method using debit cards for payment.

Abstract: The present invention provides a loadable debit card capable of online payments to merchants for good and/or services.

Abstract: A method, computer program, or apparatus for determining with various degrees of precision the power delivered by an engine, typically, an aircraft engine. The disclosed invention uses a variety of parameters, such as the rotation rate, manifold pressure, outside air temperature, and fuel flow to determine or approximate the power delivered by the engine. The engine's altitude does not have to be involved in the calculations.