NSN 2835-01-359-1671 · NIIN 013591671 · FSC 2835
NO DASHES 2835013591671
In Stock
BLADE,TURBINE ROTOR,NONAIRCRAFT
Gas Turbines and Jet Engines; Non-Aircraft Prime Mover, Aircraft Non-Prime Mover, and Components
Application: AUXILIARY POWER UNIT,C-17 ACFT; AF TO. 2G-GTCP331-4 APPLIES; SOME SURF. HAVE DIFFUSED AL/PRECIOUS METAL APPLIED. MATL IS DEFINED BY PROCESS VENDOR
Technical characteristics
11 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 |
|---|---|---|
| ABHP | OVERALL LENGTH | INCHES MINIMUM 0.975 AND INCHES MAXIMUM 0.985 |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 0.4897 |
| AGAV | END ITEM IDENTIFICATION | AUXILIARY POWER UNIT,C-17 ACFT; AF TO. 2G-GTCP331-4 APPLIES; SOME SURF. HAVE DIFFUSED AL/PRECIOUS METAL APPLIED. MATL IS DEFINED BY PROCESS VENDOR |
| APGF | DESIGN TYPE | CENTRIFUGAL |
| BGLW | BLADE ATTACHMENT METHOD | FIR TREE |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABMK |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| CZCJ | STAGE NUMBER | 1 |
| FEAT | SPECIAL FEATURES | NOMENCLATURE PER MFR DWG IS BLADE,TURBINE ROTOR FIRST STAGE |
| MATT | MATERIAL | BLADE NICKEL ALLOY |
| PRPY | PROPRIETARY CHARACTERISTICS | PACS |