"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"
MATT
MATERIAL
STEEL CORROSION RESISTING OVERALL
Product Specifications:
FSG With Name
28 - Engines, Turbines, and Components
Part Number
6809081
MFG Name
ALLISON TRANSMISSION INC
Item Name
BLADE,COMPRESSOR,AIRCRAFT GAS TU
FSC With Name
2840 - Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Cage Code
73342
NSN Number
2840-00-877-0065 (2840008770065)
FSC Name
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components