NSN 2840-00-883-5965 · NIIN 008835965 · FSC 2840
NO DASHES 2840008835965
In Stock
LOCK,TURBINE ROTOR BLADE,AIRCRAF
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: TF-33 AIRCRAFT ENGINE
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 |
|---|---|---|
| FEAT | SPECIAL FEATURES | GOES ON THE COMPRESSOR ROTOR-FRONT |
| MATT | MATERIAL | STEEL CORROSION RESISTING |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | ASSN STD SINGLE MATERIAL RESPONSE A-S5517 |
| RDAL | REFERENCE DATA AND LITERATURE | 2J-TF33-4 |
| ABMK | OVERALL WIDTH | INCHES MINIMUM 0.264 AND INCHES MAXIMUM 0.294 |
| CQFM | HARDNESS RATING | ROCKWELL A MINIMUM 63.0 AND ROCKWELL A MAXIMUM 68.0 |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| CZCJ | STAGE NUMBER | 8 |
| ABHP | OVERALL LENGTH | INCHES MINIMUM 1.315 AND INCHES MAXIMUM 1.365 |