WASHER,FLAT
Nuts and Washers
Application: W/S:ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); MISSILE, ADVANCED MEDIUM RANGE AIR-TO-AIR (AMRAAM)/AIM120A; AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); SUPPORT EQUIPMENT, B-1 AIRCRAFT; SUPPORT EQUIPMENT, B-52 AIRCRAFT; MISSILE, TOMAHAWK; TEST CONSOLES, MINI-SACE; AIRCRAFT, THUNDERBOLT II, A-10; AIRCRAFT, EAGLE F-15; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H)
Technical characteristics
9 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 | |
| AAUB | HOLE DIAMETER | INCHES MINIMUM 0.164 AND INCHES MAXIMUM 0.184 |
| ABMW | PERIPHERAL SHAPE STYLE | |
| ABMX | CENTER HOLE SHAPE STYLE | |
| ABNM | THICKNESS | INCHES MINIMUM 0.028 AND INCHES MAXIMUM 0.036 |
| ADAV | OVERALL DIAMETER | INCHES MINIMUM 0.370 AND INCHES MAXIMUM 0.395 |
| AGAV | END ITEM IDENTIFICATION | W/S:ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); MISSILE, ADVANCED MEDIUM RANGE AIR-TO-AIR (AMRAAM)/AIM120A; AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); SUPPORT EQUIPMENT, B-1 AIRCRAFT; SUPPORT EQUIPMENT, B-52 AIRCRAFT; MISSILE, TOMAHAWK; TEST CONSOLES, MINI-SACE; AIRCRAFT, THUNDERBOLT II, A-10; AIRCRAFT, EAGLE F-15; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H) |
| MATT | MATERIAL | OVERALL ALUMINUM ALLOY 2024 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | OVERALL FED SPEC SINGLE MATERIAL RESPONSE QQ-A-250 TO 5 |
Cross-references
11 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.
Supersedes
This item replaces cancelled NIINs 014322093 · 007601680. An older drawing citing one of those numbers resolves here.