6809081: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: STEEL CORROSION RESISTING OVERALL, overall_width: 1.197 INCHES NOMINAL IN, overall_length: 3.753 INCHES NOMINAL IN, end_item_identification: T56 AIRCRAFT ENGINE, criticality_code_justification: AGAV, part_name_assigned_by_controlling_agency: BLADE, COMPRESSOR-1ST STAGE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-877-0065, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | STEEL CORROSION RESISTING OVERALL |
| overall_width | 1.197 INCHES NOMINAL IN |
| overall_length | 3.753 INCHES NOMINAL IN |
| end_item_identification | T56 AIRCRAFT ENGINE |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | BLADE, COMPRESSOR-1ST STAGE |
| NSN | 2840-00-877-0065 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 3.753 INCHES NOMINAL IN |
| OVERALL WIDTH | 1.197 INCHES NOMINAL IN |
| 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 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE, COMPRESSOR-1ST STAGE |
| END ITEM IDENTIFICATION | T56 AIRCRAFT ENGINE |
| MATERIAL | STEEL CORROSION RESISTING OVERALL |
No substitute or cross-reference records for this part.