BOLT - AN6-22A



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BOLT - AN6-22A
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BOLT - AN6-22A
Genuine OEM Parts

Description:   BOLT
Part number:   AN6-22A
Industry Standard Specification:   AIA/NAS NASM3-20

Airframe Bolt - Length: 2-21/64", Grip: 1-11/16", Thread: 3/8-24, Cadmium Plated Steel, Undrilled Shank


Thread Class  3A
Thread DirectionRight-hand
Thread Length0.640 inches minimum
Fastener Length2.328 inches nominal
Head StyleHexagon
Head Height0.203 inches minimum and 0.235 inches maximum
Width Between Flats0.553 inches minimum and 0.565 inches maximum
Nominal Thread Diameter0.375 inches
Grip Length1.688 inches nominal
Features ProvidedFinished head
Thread Quantity per Inch24
Minimum Tensile Strength125000 pounds per square inchHardness Rating
Hardness Rating26.0 rockwell C minimum overall and 32.0 rockwell C maximum overall
MaterialSteel 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 ClassificationMIL-B-6812 mil spec all material responses overall
Surface TreatmentCadmium overall and chromate overall
Surface Treatment Document and ClassificationQQ-P-416 ty 2 cl 3 fed spec all treatment responses overall
Thread Series DesignatorUNF

This part is used on the following aircraft:

  1. •Textron Aviation Cessna 750 Citation X

Between AirParts' branded hardware products, and our Seller's hardware offerings, we have hundreds of thousands of hardware parts in stock.

Dimensions (W x H x D) 0.375" x 0.375" x 2.328" Inches
Length 2.328" Inches
Weight 0.084 lb
8130-3 Eligible NO
Available Conditions NE / NS
Country of origin United States of America
FAA Approval Code STD
Grip 1.688" Inches
Hazmat Code Not Applicable
Hazmat(Y/N) N
Material Steel
NSN 5306-00-208-9806
Schedule B 7318.15.2000
Thread 3A-UNF
Total Shelf Life (days) Not Applicable
Type Bolt
Units of Measure (UoM) Each
Brand Aeronautical Standard Group Inc
Condition status Depreciated