NSN 2840-00-877-0065 · NIIN 008770065 · FSC 2840
NO DASHES 2840008770065
In Stock
BLADE,COMPRESSOR,AIRCRAFT GAS TU
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: T56 AIRCRAFT ENGINE
Technical characteristics
7 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 | CONTOUR OF CONCAVE AND CONVEX SIDES OF AIRFOIL SECTIONS MAY VARY WITHIN A .006 BAND PARALLEL TO BASIC; TOLERANCE BAND APPLIES TO SECTION CONTOURS UP TO TANGENT POINT OF LEADING AND TRAILING EDGE RADII; AIRFOIL SURFACES SHALL BLEND SMOOTHLY BETWEEN DEFINED CONTOUR POINTS AND SECTIONS; THE STACKING AXIS IS A STRAIGHT LINE DEFINING THE BASIC LOCATION OF THE AIRFOIL SECTION STACKING POINTS; AIRFOIL SECTION STACKING POINTS MAY BE DISPLACED A MAXIMUM OF .003" FROM STACKING AXIS; THE ANGULAR RELATION OF THE STACKING AXIS MAY VARY .010" PER INCH IN ANY DIRECTION IN RELATION TO THE GAGE PLANE OF THE BASE; ANGULAR VARIATION OF AIRFOIL SECTIONS ABOUT THE STACKING AXIS SHALL NOT EXCEED 0 DEGREES 15' RELATIVE TO ANGLE DATUM PLAN; FORGING SHALL CONFORM TO E15 502; NO PERMANENT TYPE MARKING PERMITTED ON AIRFOIL SURFACES |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE, COMPRESSOR-1ST STAGE |
| ABHP | OVERALL LENGTH | INCHES NOMINAL 3.753 |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| MATT | MATERIAL | OVERALL STEEL CORROSION RESISTING |
| AGAV | END ITEM IDENTIFICATION | T56 AIRCRAFT ENGINE |
| ABMK | OVERALL WIDTH | INCHES NOMINAL 1.197 |