PACKING,PREFORMED
Packing and Gasket Materials
Application: W/S: AIRCRAFT, AIRLIFTER C-17A; ENGINE, AIRCRAFT TF33-PW-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); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); U-2 ENGINE (F118-GE-101); ENGINE, AIRCRAFT F-117, PW-100 (C-17A); AIRCRAFT, STRATOLIFTER C-135; AIRCRAFT, STRATOFORTRESS B-52; AIRCRAFT, PHANTOM F-4
Technical characteristics
8 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 |
|---|---|---|
| AAGR | CROSS-SECTIONAL SHAPE STYLE | |
| ZZZV | FSC APPLICATION DATA | ENGINE,AIRCRAFT,TURBO-FAN |
| ADVN | CROSS-SECTIONAL HEIGHT | INCHES MINIMUM 0.510 AND INCHES MAXIMUM 0.540 |
| ADYT | CENTER HOLE DIAMETER | INCHES MINIMUM 0.986 AND INCHES MAXIMUM 1.012 |
| ADVX | RIM SURFACE WIDTH | INCHES NOMINAL 0.250 |
| ADYU | PERIPHERAL DIAMETER | INCHES MINIMUM 1.345 AND INCHES MAXIMUM 1.375 |
| AGAV | END ITEM IDENTIFICATION | W/S: AIRCRAFT, AIRLIFTER C-17A; ENGINE, AIRCRAFT TF33-PW-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); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); U-2 ENGINE (F118-GE-101); ENGINE, AIRCRAFT F-117, PW-100 (C-17A); AIRCRAFT, STRATOLIFTER C-135; AIRCRAFT, STRATOFORTRESS B-52; AIRCRAFT, PHANTOM F-4 |
| MATT | MATERIAL | OVERALL RUBBER SYNTHETIC |
Cross-references
8 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.
Supersedes
This item replaces cancelled NIIN 008084908. An older drawing citing one of those numbers resolves here.