2C14728G01: TEMPLATE,ENGINE MAINTENANCE,AIRC.
TEMPLATE,ENGINE MAINTENANCE,AIRC. Key specifications include material: PLASTIC, overall_width: 6.000 INCHES NOMINAL IN, overall_height: 3.000 INCHES NOMINAL IN, overall_length: 30.000 INCHES NOMINAL IN, end_item_identification: C-5M AIRCRAFT CF6-80C2L1F ENGINE, reference_data_and_literature: SERD 03-01-0021. This part is cataloged in the U.S.
Government catalog under NSN 4920-01-520-4679, 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 | PLASTIC |
| overall_width | 6.000 INCHES NOMINAL IN |
| overall_height | 3.000 INCHES NOMINAL IN |
| overall_length | 30.000 INCHES NOMINAL IN |
| end_item_identification | C-5M AIRCRAFT CF6-80C2L1F ENGINE |
| reference_data_and_literature | SERD 03-01-0021 |
| part_name_assigned_by_controlling_agency | C-5M ENGINE STAGE 1 FAN BLADE REPAIR TEMPLATE |
| NSN | 4920-01-520-4679 |
| OVERALL HEIGHT | 3.000 INCHES NOMINAL IN |
| REFERENCE DATA AND LITERATURE | SERD 03-01-0021 |
| OVERALL LENGTH | 30.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 6.000 INCHES NOMINAL IN |
| FUNCTIONAL DESCRIPTION | PLEXIGLASS TEMPLATE MOLDED TO FIT BLADE CONVEX CONTOUR AND OVERHANGS THE LEADING EDGE FOR LENGTH OF AIRFOIL. USED AFTER REPAIR AND BLENDING OF THE BLADES WITHOUT REMOVAL OF ENGINE FROM AIRCRAFT. ALIGNMENT BRACKET AND STORAGE CASE INCLUDED |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | C-5M ENGINE STAGE 1 FAN BLADE REPAIR TEMPLATE |
| END ITEM IDENTIFICATION | C-5M AIRCRAFT CF6-80C2L1F ENGINE |
| MATERIAL | PLASTIC |
No substitute or cross-reference records for this part.