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National Aerospace Standards - Shear Bolt - NAS6203-22D

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National Aerospace Standards - Shear Bolt - NAS6203-22D
Standard Part

Description: Shear Bolt 
Part Number: NAS6203-22D
Alternate Part Numbers: NAS1103-22D, NAS464P3-22


Product Overview

NAS6203 series shear hexagon head bolts with a 10-32 thread and a nominal diameter of 3/16 inch (0.1875") supersede NAS1103 high strength bolts. These bolts are designed to shear if put under too much mechanical pressure. Their shearing feature is used to minimize damage to more critical components within the application. They are made from alloy steel with cadmium or chromium finishes and offered in different grips and lengths in inches with undrilled or drilled head and/or shank. NAS6203 series forms part of NAS family of bolts (NAS6203 through NAS6210 series) which includes hex head, close tolerance, alloy steel, short thread, self-locking & non-locking bolts.

 

After the basic part numbers, the following letters specify the bolts' material, finish, and drilling condition.

 

No Finish Code for cadmium plated bolts

 

  1. "C" for chromium plated bolts
  2. "L" for self-locking bolts
  3. "P" for self-locking bolts with patch type locking element only
  4. Grip Dash Number indicating grip in .0625 increments
  5. "D" after the grip dash number for drilled thread bolts
  6. "H" after the grip dash number for bolts with drilled head

 

More than one code letter may be used in sequence.

 

Item Specification

Thread Class

     

3A

Thread Direction

Right-hand

Thread Length

0.323 inches nominal

Fastener Length

1.683 inches minimum and 1.713 inches maximum

Head Style

Dished hexagon

Head Height

0.110 inches minimum and 0.125 inches maximum

Width Between Flats

0.367 inches minimum and 0.376 inches maximum

Grip Diameter

0.1885 inches minimum and 0.1895 inches maximum

Shank Unthreaded Hole Diameter

0.070 inches minimum threads and 0.080 inches maximum threads

Nominal Thread Diameter

0.190 inches

Grip Length

1.365 inches minimum and 1.385 inches maximum

Thread Quantity per Inch

32

Minimum Tensile Strength

160000 pounds per square inch

Distance from Head Largest Bearing Surface to Shank Hole Center

0.168 inches nominal threads

Surface Finish

32.0 microinches bearing surface of head

Surface Finish

32.0 microinches grip

Surface Finish

32.0 microinches threads

Material

Steel comp 4340 overall or steel comp 8740 overall

Material Document and Classification

MIL-S-5000 mil spec 1ST material response overall or ams 6322 assn std 2ND material response overall

Surface Treatment

Cadmium overall and chromate overall

Surface Treatment Document and Classification

QQ-P-416, type 2, class 2 fed spec all treatment responses overall

Thread Series Designator

UNJF

Specification/Standard Data

80205-NAS6203 professional/industrial association standard

 

Fits in

  1. Bombardier Global Express
  2. Textron Aviation Cessna 162 Skycatcher
  3. Textron Aviation Cessna 510 Citation Mustang
  4. Textron Aviation Cessna 680 Citation Sovereign

 

Cessna Aircraft Model 162 Skycatcher Illustrated Parts Catalog [ Click Here ] 

 See Page 281, Figure 01, Item 11

Additional info
Colors Gold
Dimensions
Dimensions (W x H x D) 3.95" x 5.95" x 0.65" inches
Length 5.95" inches
Weight 0.09 lb
Specifications
8130-3 Eligible No
ATA Chapter 27 ATA Flight Controls
Available Conditions NE / NS
Cage Code 80205
Country of origin United States of America
ECCN / USML 9A991.d
FAA Approval Code STD
Grip 1.365 inches minimum and 1.385 inches maximum
Hazmat Code Not Applicable
Hazmat(Y/N) N
Material Steel comp 4340 overall or steel comp 8740 overall
NSN 5306-01-442-7555
Schedule B 7318.15.2000
Thread 3A
Total Shelf Life (days) Not Applicable
Type Bolt
Units of Measure (UoM) Each
Brand National Aerospace Standard.
Color Gold
Condition status Depreciated