RING,RETAINING
Fastening Devices
Application: W/S:GUIDED MISSILE, INTERCEPT; ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); HELICOPTER, SEA KNIG H-3; AIRCRAFT, F-111; ENGINE, AIRCRAFT, J85-GE-21 (F-5E/F); AIRCRAFT, THUNDERBOLT II, A-10; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135. B-52H); HELICOPTER, MH-53E; ENGINE, AIRCRAFT, J85-GE-5/13 (F-5A/B, T-38A)
Technical characteristics
11 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 |
|---|---|---|
| AARX | INSIDE DIAMETER | INCHES NOMINAL 1.984 |
| AAGR | CROSS-SECTIONAL SHAPE STYLE | |
| ABKV | OUTSIDE DIAMETER | INCHES NOMINAL 2.260 |
| ACXD | RING STYLE | |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ASSN STD SINGLE MATERIAL RESPONSE SAE 1070 - 1090 |
| ABMC | MAJOR THICKNESS | INCHES NOMINAL 0.048 |
| AASG | CASEHARDENING INDICATOR | NOT CASE-HARDENED |
| AGAV | END ITEM IDENTIFICATION | W/S:GUIDED MISSILE, INTERCEPT; ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); HELICOPTER, SEA KNIG H-3; AIRCRAFT, F-111; ENGINE, AIRCRAFT, J85-GE-21 (F-5E/F); AIRCRAFT, THUNDERBOLT II, A-10; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135. B-52H); HELICOPTER, MH-53E; ENGINE, AIRCRAFT, J85-GE-5/13 (F-5A/B, T-38A) |
| ALBY | USAGE DESIGN | INTERNAL |
| AWQD | STRENGTH RATING | POUNDS PER SQUARE INCH (PSI) MINIMUM TENSILE 211000.0 |
| MATT | MATERIAL | STEEL |
Cross-references
12 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.
| Manufacturer part number | CAGE |
|---|---|
| 402047 | 33823 |
| 327B436P5 | 33823 |
| WH-216 | 51814 |
| RD15951-216 | 51663 |
| 626-001-9162 | 70210 |
| RR-216 | 72547 |
| MCF13375 | 76050 |
| 402047 | 77445 |
| RR216 | 80756 |
| RR216 | 03350 |
| 10598916-1 | 18876 |
| 10043943-174 | 18876 |
Supersedes
This item replaces cancelled NIIN 009190843. An older drawing citing one of those numbers resolves here.