# Rework Procedures_old

ProcedureDescription:
Visual discr. at tip cut due to ink/electro react


ProcedureDescription:
PRE-ROOT MILL RE-INSP OF NICKS ON L/E AIRFOIL


ProcedureDescription:
NICKS-L/E ENDCAP DATUM - J117176-000-001 ONLY


ProcedureDescription:
BLADE - UN-EVEN SHOT PEEN ON ROOT@ FINAL


ProcedureDescription:
Airfoil Visual Non Conformances after peen


ProcedureDescription:
CLEAN STAIN FROM ROOT (USE THIS BEFORE RP-409)


ProcedureDescription:
REMOVE HIGH SPOT LEFT BY INCOMPLETE ETCH


ProcedureDescription:
NICKS & DINGS PRIOR TO ANTIGALL APPLICATION


ProcedureDescription:
Nicks, Pitting, and Scratches from Airfoil/Platfor


ProcedureDescription:
Removal of Grinding Smut Identified at OP 170


ProcedureDescription:
4 corner radius, Triplane, Surface, Dimensional


ProcedureDescription:
SELECTIVE POLISH FOR DIMENSIONAL AND SURFACE DISCR


ProcedureDescription:
SELECTIVE POLISH TO REMOVE NICKS, PIT, DIMENSION..


ProcedureDescription:
SELECTIVE POLISH FOR PITTS,NICKS,SCRATCH, DIMEN…


ProcedureDescription:
AIRFOIL ANGLE NONCONFORMANCE (N, LEA, TEA)


ProcedureDescription:
SURFACE/DIMENSIONAL DISCREPANCIES FOR ROOT ONLY


ProcedureDescription:
NONCONFORMING ROUND EDGE AT DOVETAIL MIN NECK


ProcedureDescription:
SURFACE FINISH NONCONFORMANCE PRIOR TO PEEN


ProcedureDescription:
overspray of aluminum-bronze coating on airfoil


ProcedureDescription:
COATING DISCREPANCIES-OSV STRIP AND RECOAT


PartNumber:
JAP105, JAP106, JAP107, JAP108, JAP109 (ALL VARIANTS)


ProcedureDescription:
SELECTIVE POLISH OF AIRFOIL AND/OR ROOT FEATURES


ProcedureDescription:
TRIPLANE RADIUS IS UNDERSIZED - SELECTIVE POLISH


ProcedureDescription:
Part Mark operation missing at or prior to Op. 70


ProcedureDescription:
VISUAL AND DIMENSIONAL DISCREPANCIES FOR SEMIFINIS


ProcedureDescription:
Rework for discrepant surface finish on Tip


ProcedureDescription:
RE-WORK FOR L/E PLATFORM CHAMFER, U/MIN CONDITION

Application Guideline:
POLISH INDICIES 75, 75 & 77 ALONG INDEX 63


Application Guideline:
RTV PARTS TO ADDRESS NON-CONF DETAILED ON NCMR


ProcedureDescription:
PART MARK NOT LEGIBLE AFTER PLATING AT OP 295


ProcedureDescription:
SELECTIVE POLISH DEFECTS DETECTED AT OP 050


ProcedureDescription:
4 corner rounds under blueprint tolernaces


ProcedureDescription:
SELECTIVE POLISH DIMENSIONAL DEFECTS DETECTED


Application Guideline:
RE-PROCESS PARTS THAT WERE INADVERTAINTLY RE-AIRFOIL PEENED


