O-RING
O-Ring
Application: W/S: AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); ENGINE, AIRCRAFT TF33-PWPP-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT, TF33-100 (E3A/B/C); HELICOPTER, HH-53H PAVE LOW; AIRCRAFT, C-18A, EC-18B; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B)
Technical characteristics
5 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 1.612 AND INCHES MAXIMUM 1.648 |
| ADVN | CROSS-SECTIONAL HEIGHT | INCHES MINIMUM 0.100 AND INCHES MAXIMUM 0.106 |
| ADYT | CENTER HOLE DIAMETER | INCHES MINIMUM 1.418 AND INCHES MAXIMUM 1.430 |
| AGAV | END ITEM IDENTIFICATION | W/S: AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); ENGINE, AIRCRAFT TF33-PWPP-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H); ENGINE, AIRCRAFT, TF33-100 (E3A/B/C); HELICOPTER, HH-53H PAVE LOW; AIRCRAFT, C-18A, EC-18B; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B) |
| MATT | MATERIAL | RUBBER BUTADIENE-ACRYLONITRILE CLASS NBR |
Supersedes
This item replaces cancelled NIINs 001062769 · 002901047 · 002913832 · 006410122 · 008018402. An older drawing citing one of those numbers resolves here.