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BOLT - AN4-3A

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BOLT - AN4-3A
Aeronautical Standard Parts


Description:   BOLT
Part number:   AN4-3A
Industry Standard Specification:   AIA/NAS NASM3-20

Airframe Bolt - Length: 15/16", Grip: 1/16", Thread: 1/4-28, Cadmium Plated Steel, Undrilled Shank



AN4-3A   FEATURES


Parameter    Characteristics
Thread Class:3A
Thread Direction:Right-hand
Thread Length:0.407 inches maximum
Fastener Length:0.469 inches nominal
Head Style:Hexagon
Head Height:0.140 inches minimum and 0.172 inches maximum
Width Between Flats:0.428 inches minimum and 0.440 inches maximum
Hole Diameter:0.046 inches nominal
Nominal Thread Diameter:0.250 inches
Grip Length:0.062 inches nominal
Hole Quantity:1
Hole Type:Drilled
Features Provided:Finished head
Thread Quantity per Inch:28
Minimum Tensile Strength:125000 pounds per square inch
Hardness Rating:26.0 rockwell C minimum overall and 32.0 rockwell C maximum overall
Hole Configuration Style:Hexagon flats
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, type 2, class 3 fed spec all treatment responses overall
Thread Series Designator:UNF



This part is used on the following aircraft:

  1. • Embraer Legacy 600-650
  2. • Textron Aviation Beechcraft King Air 200 - all variants
  3. • Textron Aviation Cessna 500 Citation I-ISP
  4. • Textron Aviation Cessna 525 Citation Citationjet
  5. • Textron Aviation Cessna 550 Citation I-II-Bravo
  6. • Textron Aviation Cessna 560 Citation V-Ultra-Encore-Excel-XLS
  7. • Textron Aviation Cessna 650 Citation III-IV-VI-VII
  8. • Textron Aviation Cessna 750 Citation X




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