PIN-RIVET
Rivets
Application: W/S:AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); AIRCRAFT, AWACS, E-3A; HELICOPTER, HH-53H PAVE LOW; AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); HELICOPTER, ADVANCE ATTACK, AH-1W; HELICOPTER, MH-53E; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); HELICOPTER, CARRIER BASED ASW, SH-60F
Technical characteristics
21 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| AATB | WIDTH BETWEEN FLATS | INCHES MINIMUM 0.079 AND INCHES MAXIMUM 0.081 |
| AAJD | THREAD CLASS | 3A |
| CQJX | NOMINAL THREAD SIZE | INCHES 0.190 |
| AAZE | SHANK DIAMETER | LOCATION NOT OTHERWISE SPECIFIED INCHES MINIMUM 0.189 AND INCHES MAXIMUM 0.190 |
| MATT | MATERIAL | OVERALL STEEL COMP 4140 OR STEEL COMP 8740 OR STEEL COMP 4130 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL MIL SPEC 1ST MATERIAL RESPONSE -IL-S-5626 OR MIL SPEC 2ND MATERIAL RESPONSE -IL-S-6049 OR MIL SPEC 3RD MATERIAL RESPONSE -IL-S-6758 |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| SFTT | SURFACE TREATMENT | OVERALL CADMIUM |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | OVERALL FED SPEC SINGLE TREATMENT RESPONSE QQ--416,TY 2,CL 3 |
| THSD | THREAD SERIES DESIGNATOR | UNIFIED NATIONAL JOINT FINE (UNJF) |
| CMLP | THREAD QUANTITY PER INCH | 32 |
| CRSQ | COUNTERSINK ANGLE | RADIANS NOMINAL 0.9 |
| AASK | HEAD STYLE | |
| ANEE | GRIP LENGTH | LOCATION NOT OTHERWISE SPECIFIED INCHES MAXIMUM 0.255 |
| AASU | HEAD HEIGHT | LOCATION NOT OTHERWISE SPECIFIED INCHES MINIMUM 0.064 AND INCHES MAXIMUM 0.074 |
| AAZF | SHANK STYLE | |
| AAZG | HEAD MAJOR DIAMETER | LOCATION NOT OTHERWISE SPECIFIED INCHES MINIMUM 0.357 AND INCHES MAXIMUM 0.377 |
| AGAV | END ITEM IDENTIFICATION | W/S:AIRCRAFT, C-2A (REPROCURED); ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); AIRCRAFT, AWACS, E-3A; HELICOPTER, HH-53H PAVE LOW; AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); HELICOPTER, ADVANCE ATTACK, AH-1W; HELICOPTER, MH-53E; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); HELICOPTER, CARRIER BASED ASW, SH-60F |
| CQBC | MINIMUM TENSILE STRENGTH | POUNDS PER SQUARE INCH 160000 |
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AASB | FASTENER LENGTH | LOCATION NOT OTHERWISE SPECIFIED INCHES MINIMUM 0.565 AND INCHES MAXIMUM 0.585 |
Cross-references
26 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.
| Manufacturer part number | CAGE |
|---|---|
| HL20PB6-4 | 1RC86 |
| GB511E3-4 | 26512 |
| HL20PB-6-4 | 56878 |
| HL1050PB6-4 | 56878 |
| BACB30MB6-4 | 5R793 |
| HL1050PB6-4 | 60516 |
| HL20PB-6-4 | 60725 |
| HL20PB-6-4 | 60516 |
| HL20PB-6-4 | 73197 |
| HL1050PB6-4 | 73197 |
| BACB30MB6-4 | 77272 |
| BACB30MB6-4 | 81205 |
| 5320PL2220352 | 9009H |
| HL20PB-6-4 | 92215 |
| HS5603-6-4 | 8V613 |
| HL20PB6-4 | 97928 |
| 100-048-6-4 | 97499 |
| HL20PB-6-4 | C4293 |
| HL20PB-6-4 | R1120 |
| HL1050PB6-4 | L4528 |
| HL1050PB6-4 | 06725 |
| HL20PB-6-4 | 06950 |
| HL20PB-6-4 | 06725 |
| HL1050PB6-4 | 06950 |
| HL1050PB6-4 | 17446 |
| HL20PB-6-4 | 17446 |
Supersedes
This item replaces cancelled NIINs 002389460 · 007009199 · 007281465. An older drawing citing one of those numbers resolves here.