Cirrus Aircraft Bolt - AN3-34

Price:

6,98

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Cirrus Aircraft Bolt - AN3-34

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Cirrus Aircraft Bolt - AN3-34
Genuine OEM Parts


Description: BOLT
Part number: AN3-34
Industry Standard Specification: AIA/NAS NASM3-20


Airframe Bolt - Length: 3-17/32", Grip: 3-1/8", Thread: 10-32, Cadmium Plated Steel, Drilled Shank


AN3-34   FEATURES

ParameterCharacteristics
Thread Class  :3A
Thread Direction:Right-hand
Thread Length:0.406 inches minimum
Fastener Length:3.531" inches nominal
Head Style:Hexagon
Head Height:0.109" inches minimum and 0.141" inches maximum
Width Between Flats:0.365" inches minimum and 0.377" inches maximum
Shank Unthreaded Hole Diameter:0.070" inches nominal first hole
Nominal Thread Diameter:0.190" inches
Grip Length:3.125" inches nominal
Features Provided:Finished head
Thread Quantity per Inch:32
Minimum Tensile Strength:125000 pounds per square inch
Hardness Rating:26.0 rockwell C minimum overall and 32.0 rockwell C maximum overall
Distance from Head Largest Bearing Surface to Shank Hole Center:3.391" inches nominal first hole
Material

:

Steel comp 4037 overall or steel comp 4130 overall or steel comp 8630 overall
or steel comp 8735 overall or steel comp 8740 overall or steel comp 4140 overall
Material Document and Classification:MIL-B-6812 mil spec all material responses overall
Surface Treatment:Cadmium overall and chromate overall
Surface Treatment Document and Classification:QQ-P-416, ty 2, cl 3 fed spec all treatment responses overall
Thread Series Designator:UNF



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Dimensions
Dimensions (W x H x D) 0.19" x 0.19" x 3.531" Inches
Length 3.531" Inches
Weight 0.03 lb
Specifications
8130-3 Eligible NO
Available Conditions NE / NS
Country of origin United States of America
ECCN / USML EAR99
FAA Approval Code STD
Grip 3.125" Inches
Hazmat Code Not Applicable
Hazmat(Y/N) N
Material Steel
NSN 5306-00-144-3669
Schedule B 7318.15.2000
Thread UNF-3A
Total Shelf Life (days) Not Applicable
Type Bolt
Units of Measure (UoM) Each
Condition status Depreciated