O-RING
O-Ring
Application: JOINT STARS TARGET RADAR SYSTEM; HELICOPTER, SOF / HH-53H PAVE LOW; ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); MOORED TRAINING SHIP; AIRCRAFT, SOF ( AC-130H, MC-130H, EC-130E, HC-130); U-2 AIRFRAME; ENGINE, AIRCRAFT, T56-A-7/15 (C-130B/E/H/N/P); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); LANDING CRAFT AIR CUSHION (LCAC)
Technical characteristics
6 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 |
|---|---|---|
| ABHE | OUTSIDE DIAMETER | INCHES MINIMUM 1.864 AND INCHES MAXIMUM 1.910 |
| ADYT | CENTER HOLE DIAMETER | INCHES MINIMUM 1.599 AND INCHES MAXIMUM 1.619 |
| MATT | MATERIAL | RUBBER BUTADIENE-ACRYLONITRILE CLASS NBR |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |
| ADVN | CROSS-SECTIONAL HEIGHT | INCHES MINIMUM 0.135 AND INCHES MAXIMUM 0.143 |
| AGAV | END ITEM IDENTIFICATION | JOINT STARS TARGET RADAR SYSTEM; HELICOPTER, SOF / HH-53H PAVE LOW; ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); MOORED TRAINING SHIP; AIRCRAFT, SOF ( AC-130H, MC-130H, EC-130E, HC-130); U-2 AIRFRAME; ENGINE, AIRCRAFT, T56-A-7/15 (C-130B/E/H/N/P); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); LANDING CRAFT AIR CUSHION (LCAC) |
Supersedes
This item replaces cancelled NIINs 002501180 · 004118946 · 007168996 · 009463228 · 011035438. An older drawing citing one of those numbers resolves here.