4730-01-657-4972

4 17 Aug 2016 1990-01-657-4970 Endcap Assembly 161134RNCC: 3 | RNVC: 2 | DAC: 4 17 Aug 2016 4730-01-657-4972

1730-01-008-4345 1730010084345 010084345 GUIDE ASSEMBLY,TROUGH

1560-01-369-4075 1560013694075 013694075 is an auxiliary longitudinal member of the structural framework of a fuselage, nacelle, empennage, wing, and the like. it is designed to stiffen and/or support the skin by attachment of bulkheads, formers, frames, ribs, and the like.

2590-31-014-0997 2590310140997 310140997 KIT MODIFICATION /

5305-00-498-6977 5305004986977 004986977 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.