5307-00-700-5774
Find complete technical information, availability, and procurement data for: 5307-00-700-5774
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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.
0.550 inches minimum stud thread thread length, +0.2301 to 0.2314 inches stud thread thread pitch diameters, right-hand nut thread thread direction, right-hand stud thread thread direction, 0.490 inches minimum nut thread thread length
Product Characteristics
Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.
- Thread Pitch Diameters
- +0.2301 to 0.2314 inches stud thread
- Thread Direction
- right-hand nut thread
- Thread Direction
- right-hand stud thread
- Thread Length
- 0.490 inches minimum nut thread
- Thread Length
- 0.550 inches minimum stud thread
- Overall Length
- 2.560 inches nominal
- Distance From Cotter Pin Hole Centerline To Nut End
- 0.110 inches nominal first hole
- Cotter Pin Hole Diameter
- 0.065 inches minimum and 0.072 inches maximum first hole
- Thread Quantity Per Inch
- 20 stud thread
- Thread Quantity Per Inch
- 28 nut thread
- Hardness Rating
- 26.0 rockwell c minimum and 32.0 rockwell c maximum
- Nominal Thread Size
- 0.250 inches nut thread
- Nominal Thread Size
- 0.250 inches stud thread
- Material
- steel comp 8740
- Material Document And Classification
- ams 6322 assn std single material response
- Thread Series Designator
- unc stud thread
- Thread Series Designator
- unf nut thread
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FAQs
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