21C2674P010: ROLLER,EJECTION SEAT.
The ROLLER,EJECTION SEAT is a the manufacturer industrial component. Key specifications include blade_lock: INCLUDED, blade_shape: STRAIGHT, blade_length: 7.940 INCHES MINIMUM AND 8.060 INCHES MAXIMUM IN, blade_quantity: 12, blade_thickness: 0.0450 INCHES ELEVENTH BLADE IN, blade_tip_width: 0.090 INCHES MINIMUM AND 0.160 INCHES MAXIMUM IN. This part is cataloged in the U.S.
Government catalog under NSN 5210-00-075-1257, 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.
| blade_lock | INCLUDED |
| blade_shape | STRAIGHT |
| blade_length | 7.940 INCHES MINIMUM AND 8.060 INCHES MAXIMUM IN |
| blade_quantity | 12 |
| blade_thickness | 0.0450 INCHES ELEVENTH BLADE IN |
| blade_tip_width | 0.090 INCHES MINIMUM AND 0.160 INCHES MAXIMUM IN |
| special_features | SIX 0.0050 IN. BLADES AND SIX 0.0450 IN. BLADES IN |
| measurement_system | ENGLISH |
| blade_group_quantity | 2 |
| functional_description | USED TO CHECK CLEARANCE BETWEEN TURBINE BUCKET TIPS AND STATOR CASING |
| end_item_identification | GE AIRCRAFT ENGINE |
| NSN | 5210-00-075-1257 |
| MEASUREMENT SYSTEM | ENGLISH |
| BLADE TIP WIDTH | 0.090 INCHES MINIMUM AND 0.160 INCHES MAXIMUM IN |
| BLADE SHAPE | STRAIGHT |
| BLADE LENGTH | 7.940 INCHES MINIMUM AND 8.060 INCHES MAXIMUM IN |
| BLADE THICKNESS | 0.0050 INCHES FIFTH BLADE IN |
| BLADE THICKNESS | 0.0050 INCHES FIRST BLADE IN |
| BLADE THICKNESS | 0.0050 INCHES SIXTH BLADE IN |
| BLADE THICKNESS | 0.0050 INCHES FOURTH BLADE IN |
| BLADE THICKNESS | 0.0050 INCHES SECOND BLADE IN |
| BLADE THICKNESS | 0.0050 INCHES THIRD BLADE IN |