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RIGHT-Hand
hexagon
0.048in. ⁓1/16"
95000 pounds per square inch
door assembly, no 4 passenger on B757 aircraft
cetyl alcohol lubricant
0.1879 microinches
100.0 degrees
bolt
finish: aluminum pigmented coating per bms 10-85 type i, class a
black
titanium alloy
ams 4928 or ams 4967 assn std single material response
aluminum
grip length: 0.5625"
lubrication: cetyl alcohol per AS87132 type i or type iii, grade optional
81205-BACB30Nw standard (includes industry or association standards, individual manufactureer standards, etc.) .
Titanium alloy
Hexagon
Right-hand
Schedule B number: 8108908000
nmfc 093486
Other wrought titanium
FSC 5306 ⁓ Bolts
Used on door assembly, no 4 passenger on b757 aircraft. aluminum surface treated finish: aluminum pigmented coating per bms 10-85 type i, class a bolt hexagon head style right-hand
Nothing similar to this part number was found in our inventory
A high strength, 160,000 pounds per square inch (1100 megapascals) minimum tensile strength externally threaded fastener designed for use in applications involving great shear stress. the head is designed to accommodate an external wrench or driver. the head is not designed to be held or driven with an inserted driver, nor is it designed for rotation by the thumb and fingers. the unthreaded portion is of specific grip length, plated or unplated, and is machined to a tolerance of one thousandth (0.001) of an inch (0.025 mm) or less of a specific diameter for items one inch (25 mm) or less in diameter. items over one inch (25 mm) in diameter shall have a tolerance of fifteen ten thousandths (0.0015) of an inch (0.038 mm) or less. the nominal major diameter of the threads shall be at least one thousandth (0.001) of an inch (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. a locking feature may be incorporated in the design of the head or threads. see bolt, machine and bolt, clevis.