5306-00-557-8365

1963 5306-00-619-4615 Continuous Thread Rod 00-345A290RNCC: 3 | RNVC: 1 | DAC: 4 1 Jan 1963 5306-00-557-8365
2007 5306-01-545-6357 Continuous Thread Rod 98812A029RNCC: 3 | RNVC: 2 | DAC: 5 20 Nov 2006 5306-01-539

5305-01-381-5754 5305013815754 013815754 is a screw, machine or screw, cap, socket head whose unthreaded portion is of specified grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001 in.) (0.025 mm) or less of a specific diameter for items (1.000 in.) (25 mm) or less in diameter. items over (1.000 in.) (25 mm) in diameter shall have a tolerance of fifteen ten thousandths (0.0015 in.) (0.038 mm) or less. the nominal major diameter of the threads shall be at least one thousandth (0.001 in.) (0.025 mm) below the minimum shank diameter, but not below the minimum major diameter for applicable class of fit, as shown in the screw thread standards, fed std h28 and/or other nationally recognized standards. the head is designed to be held or driven with an inserted driver. it is not designed for rotation by the thumb and fingers. a locking feature may be incorporated in the design of the head or threads.

6240-14-283-0892 6240142830892 142830892 is an item whose principal purpose is to produce light from a glowing filament(s). it includes metal backed and reflecting types, seal beam and flood types. it may include an integral filament shield to control and/or modify its illumination pattern.

1560-01-701-2376 1560017012376 017012376 is a device of various shapes to be permanently attached to the structure of an aircraft. it is designed to permanently mount and/or support an integral member, or group of members of the airframe in a proper position and bear the stress imposed by the components being supported. it may have mounting provisions, such as slots, holes, and/or attachments to facilitate installation. excludes items which are primarily designed for dampening shock and/or vibration. excludes bracket, angle; bracket, double angle; bracket, shelf; bracket, mounting; bracket (1), structural component, aircraft; and radius block.

1560-01-713-5658 1560017135658 017135658