Abstract: According to one non-limiting embodiment, a method includes accessing distributions of flight loads associated with one or more flight regimes for a fleet of aircraft. Using the distributions of flight loads, a factor for at least one of the flight regimes is determined that provides a flight load adjustment for a component on each aircraft of a fleet of aircraft known to be affected through at least load damage by the at least one flight regime.

Abstract: According to one non-limiting embodiment, a method includes accessing flight regime rates of occurrence distributions associated with one or more flight regimes for a fleet of aircraft. Using the accessed flight regime distributions, a factor for at least one of the flight regimes is determined that provides a predetermined amount of reliability for a component on each aircraft on the fleet of aircraft known to be affected through at least fatigue damage by the at least one flight regime.

Abstract: According to one non-limiting embodiment, a method includes accessing flight regime rates of occurrence distributions associated with one or more flight regimes for a fleet of aircraft. Using the accessed flight regime distributions, a factor for at least one of the flight regimes is determined that provides a predetermined amount of reliability for a component on each aircraft on the fleet of aircraft known to be affected through at least fatigue damage by the at least one flight regime.

Abstract: According to one non-limiting embodiment, a method includes accessing distributions of flight loads associated with one or more flight regimes for a fleet of aircraft. Using the distributions of flight loads, a factor for at least one of the flight regimes is determined that provides a flight load adjustment for a component on each aircraft of a fleet of aircraft known to be affected through at least load damage by the at least one flight regime.

Abstract: A system and method are disclosed that provide for transmitting data from a downhole location to the surface. In one embodiment, a communications medium provides data transfer capabilities to the surface. A first downhole instrument is associated with the communications medium in order to measure a first downhole parameter and transmit first data relative to the first downhole parameter to the surface via the communications medium at a first time. A second downhole instrument is associated with the communications medium in order to measure a second downhole parameter and transmit second data relative to the second downhole parameter to the surface via the communications medium at a second time such that the first data is interleaved with the second data.

Abstract: Universal synchronous marine navigation light system comprising plural duplex lamp stations. Each duplex lamp station includes a microcomputer, all microcomputers being interconnected by an RS422 communications loop so as to operate all stations in synchronism and in conformance with any existing international standard of operation. Each duplex station comprises a first section having a pair of ac operated lamps and a second section having a pair of lamps one of which is ac operated and the other of which is dc operated. The ac lamps are operated in an on/off flash pattern under normal conditions in "15 mile" or "12 mile standby" modes. If all ac lamps fail, the dc lamp is operated in a "default" flash pattern in a "10 mile" mode.