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 |
|---|---|
| 53551 | ALLFAST FASTENING SYSTEMS INC |
Federal Supply Class
Title
RIVETS
Inclusions:
Exclusions:
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| ABAF | EXPANSION DEVICE | SERRATED STEM-TYPE W |
| ABAF | EXPANSION DEVICE | SERRATED STEM-TYPE W |
| AAZG | HEAD MAJOR DIAMETER | 0.090 INCHES MAXIMUM |
| AAZE | SHANK DIAMETER | 0.094 INCHES NOMINAL |
| AASK | HEAD STYLE | FLUSH (FLAT) COUNTERSUNK (INCLUDED ANGLE - LESS THAN 135 DEG W OR W/O CHAMFER) |
| CRSQ | COUNTERSINK ANGLE | 99.0 DEGREES MINIMUM AND 101.0 DEGREES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | W/S: TICONDEROGA CLASS CG (47); SPRUANCE CLASS DD (963); HELICOPTER, HH-53H PACE LOW; ENGINE, AIRCRAFT, TF39-GE-1 (C-5A); HELICOPTER, ADVANCE ATTACK, AH-1W; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); AIRCRAFT, (AC-130H, MC-130H, EC-130E, HC-130); ENGINE, AIRCRAFT, TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT, TF33-PW-102 (C-135E, EC-135H/K/P); HH-60L MEDIVAC |
| MATT | MATERIAL | STEEL OVERALL |
| AASB | FASTENER LENGTH | 0.328 INCHES NOMINAL |
| ANEE | GRIP LENGTH | 0.188 INCHES MINIMUM AND 0.250 INCHES MAXIMUM |
| AAZF | SHANK STYLE | PULL THROUGH HOLLOW SHANK |