2805-00-350-2873

: 9 | DAC: 5 9 Jan 1974 5330-00-350-2837 Gasket 1294C18RNCC: 3 | RNVC: 2 | DAC: X 1 Jan 1963 2805-00-350-2873

1560-01-476-4714 1560014764714 014764714 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.

JavaScript in your web browser . 2910-14-354-8545Tubes Injecte Bride2910143548545 143548545 0000387335 387335
(Renault Vehicules (Replaced) Canceled/Obsolete RNCC 5 RNVC 9 DAC 1 387335 F0727 - R.V.I.

3895-15-178-3727 3895151783727 151783727 is a power or hand operated, base mounted machine having a revolving drum with fixed blades mounted on the inner circumference, in which aggregate, cement, and water are mixed in the preparation of concrete.

5306-27-037-0881 5306270370881 270370881 is an externally threaded fastener designed for insertion through holes in assembled parts and normally intended to be tightened or released by torquing a nut. the threaded and unthreaded portions are both of one nominal diameter of 0.190 inch (5 mm) or larger. the head is not designed to be held or driven with an inserted driver or by the thumb and fingers. a locking feature may be incorporated in the design of the head or threads. head dimensions and sizes of threaded and unthreaded portions shall conform to internationally recognized fastener standards. for items having a grip length portion machined to a tolerance of 0.0015 inch (0.038 mm) or less, bolt, shear. see also screw, cap, hexagon head and screw, machine.