Part Number
Part Number:
NSN:
NIIN:
Item Name:
RIVET , BLIND
Definition:
AN ITEM CONSISTING OF TWO OR MORE OF THE FOLLOWING COMPONENTS: STEM, RIVET BODY, SLEEVE, EXPANDER, BOLT, AND COLLAR. IT IS A HEADED FASTENING DEVICE WITH THE SHANK DESIGNED TO BE EXPANDED BY MEANS OF A SEPARATE OR INTEGRAL STEM OR MANDREL, OR BOLT AND EXPANDER. IT IS DESIGNED TO BE INSTALLED OR EXPANDED FROM ONE SIDE ONLY. EXCLUDES NUT, BLIND ASSEMBLY.
CAGE Information
Code | Company |
---|---|
11449 | TURBO POWER & MARINE SYSTEM INC SUB |
Federal Supply Class
Title
RIVETS
Inclusions:
Exclusions:
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
CQSX | SHEAR STRENGTH | 450 SINGLE POUNDS PER SQUARE INCH |
CQSX | SHEAR STRENGTH | 450 SINGLE POUNDS PER SQUARE INCH |
MATT | MATERIAL | NICKEL ALLOY 400 SLEEVE |
ABAF | EXPANSION DEVICE | SERRATED STEM-TYPE W |
AASB | FASTENER LENGTH | 0.448 INCHES MAXIMUM |
AASK | HEAD STYLE | FLUSH (FLAT) COUNTERSUNK (INCLUDED ANGLE - LESS THAN 135 DEG W OR W/O CHAMFER) |
AAZF | SHANK STYLE | SELF-PLUGGING MECHANICALLY LOCKED STEM |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-N-281 FED SPEC ALL MATERIAL RESPONSES OVERALL |
CRSQ | COUNTERSINK ANGLE | 99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | W/S: AIRCRAFT, INTRUDER A-6E; ENGINE, AIRCRAFT TF-30; AIRCRAFT, GALAXY C-5 |
ZZZK | SPECIFICATION/STANDARD DATA | 80205-NAS1399 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
ANEE | GRIP LENGTH | 0.251 INCHES MINIMUM AND 0.312 INCHES MAXIMUM |
AAZG | HEAD MAJOR DIAMETER | 0.221 INCHES MINIMUM AND 0.229 INCHES MAXIMUM |
AAZE | SHANK DIAMETER | 0.124 INCHES MINIMUM AND 0.128 INCHES MAXIMUM |
MATT | MATERIAL | NICKEL ALLOY 400 STEM |