5310-14-200-1309

1309 6350152001309 152001309 BASE PER RIVELATORE https//www.nsnlookup.com /fsg-53/fsc-5310/fr 5310-14-200-1309
5310142001309 142001309 5310-14-200-1309 5310142001309 142001309 https//www.nsnlookup.com /fsg-

1420-01-309-8315 1420013098315 013098315 is a movable airfoil, forming a part and/or all of the main directional control surfaces of a missile. it is usually perpendicular or approximately perpendicular to the longitudinal axis of the missile. its function is to maintain uniformity of direction and to aid in the control of yaw, pitch, and roll of a guided missile in flight.

1420-01-309-5856 1420013095856 013095856 is a hydraulically or pneumatically powered actuating cylinder with provisions for directional control (positioning) in direct relation with a primary control of comparatively low level force. the primary control input to the servocylinder may be mechanical and/or electrical.

1660-01-144-4529 1660011444529 011444529 is an item designed to regulate aircraft cabin and/or compartment pressure by providing a reference pressure signal to control the operation of one or more valves discharging cabin and/or compartment air to the atmosphere. may contain or operate in conjunction with selector controls for desired altitude pressure and altitude rate of change or be pre-set for automatic operation without selector controls. for items consisting of a controller and a valve, see regulator, air pressure, aircraft cabin.

1420-01-309-5858 1420013095858 013095858 is a portion of a guided missile specifically designed for seeking out a target by detection of reflected laser energy. location of the target is then translated into homing command signals by related equipment.excludes seeker section, electro-optical, guided missile; seeker section, infrared, guided missile; and seeker section, radar, guided missile.