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Aeronautical Standards Group​​ - Bolt - AN3-11A

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Aeronautical Standards Group - BOLT - AN3-11A
Genuine OEM Part

Description:   BOLT 
Part number:   AN3-11A 
Alternate part number:   130909B21

Hex head aircraft bolts are made of high-strength type 4037 or 8740 alloy steel (type 8740 is most commonly used). The bolts are centerless ground and threaded after heat treatment. Minimum tensile strength 125,000 PSI. Cadmium plated per specification QQ-P-416A, Type II, Class 3. Available with shank drilled for cotter pin or undrilled for stop nut application, and with or without drilled head for safety wire. Specify bolts to have undrilled shank by adding letter "A" after the dash number. For bolts with drilled head add letter "H" after the AN number. (AN3H-15) See illustrated examples. The length of AN aircraft bolts is measured from under the head to the end of the shank. The "grip" is the unthreaded portion of the shank. See table for conversion of length and/or grip to proper AN callout. "C" stands for stainless. Others are cadmium plated.


TECHNICAL FEATURES 

  1. Hexagon Head
  2. Undrilled Head
  3. No Cotter Pin Hole
  4. Fine Threads
  5. UNF-3A
  6. Material: Steel
  7. Major Diameter: 0.19 in.
  8. Thread Per Inch (TPI): 32
  9. Length: 1.156 in.
  10. Grip Length: 0.75 in.
  11. Industry Standard Specification: AIA/NAS NASM3-20





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Additional info
Features • Airframe Bolt • Length: 1-5/32" • Grip: 3/4" • Thread: 10-32 • Cadmium Plated Steel • Undrilled Shank
Dimensions
Dimensions (W x H x D) 0.19" x 0.19" x 1.15" Inches
Length 1.15" Inches
Weight 0.01 lb
Specifications
8130-3 Eligible NO
Available Conditions NE / NS
Cage Code 9V172
Country of origin United States of America
ECCN / USML EAR99
FAA Approval Code STD
Grip 0.75" Inches
Hazmat Code Not Applicable
Hazmat(Y/N) N
Material Steel overall. Surface Treatment: Cadium
NSN 5306-00-685-3027
Schedule B 7318.15.2000
Thread 3A-UNF
Total Shelf Life (days) Not Applicable
Type Bolt, Machine Bolt
Units of Measure (UoM) Each
Brand Aeronautical Standard Group Inc