856A4008P01: SEAL,BACKFLUSH,HIGH PRESSURE TUR.
SEAL,BACKFLUSH,HIGH PRESSURE TUR. Key specifications include material: RUBBER SYNTHETIC, overall_width: 3.000 INCHES NOMINAL IN, overall_height: 1.000 INCHES NOMINAL IN, overall_length: 4.000 INCHES NOMINAL IN, end_item_identification: F108-CF-100 AIRCRAFT ENGINE,KC-135R AIRPLANE. This part is cataloged in the U.S.
Government catalog under NSN 4920-01-170-9351, 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 | RUBBER SYNTHETIC |
| overall_width | 3.000 INCHES NOMINAL IN |
| overall_height | 1.000 INCHES NOMINAL IN |
| overall_length | 4.000 INCHES NOMINAL IN |
| special_features | SILICONE RUBBER,50A DUROMETER; HAS ADEQUATE ACID RESISTANCE TO WITHSTAND THE ACIDIC RESIDUE WHICH REMAINS IN THE BLADE FROM PREVIOUS TESTING A |
| end_item_identification | F108-CF-100 AIRCRAFT ENGINE,KC-135R AIRPLANE |
| general_characteristics_item_description | IS REQUIRED TO CHANNEL THE BACKFLUSH WATER THROUGH THE COOLING HOLES AND OUT THE BASE OF THE DOVETAIL WHEN INSPECTING THE TURBINE BLADE |
| NSN | 4920-01-170-9351 |
| OVERALL HEIGHT | 1.000 INCHES NOMINAL IN |
| GENERAL CHARACTERISTICS ITEM DESCRIPTION | IS REQUIRED TO CHANNEL THE BACKFLUSH WATER THROUGH THE COOLING HOLES AND OUT THE BASE OF THE DOVETAIL WHEN INSPECTING THE TURBINE BLADE |
| OVERALL LENGTH | 4.000 INCHES NOMINAL IN |
| OVERALL WIDTH | 3.000 INCHES NOMINAL IN |
| SPECIAL FEATURES | SILICONE RUBBER,50A DUROMETER; HAS ADEQUATE ACID RESISTANCE TO WITHSTAND THE ACIDIC RESIDUE WHICH REMAINS IN THE BLADE FROM PREVIOUS TESTING A |
| END ITEM IDENTIFICATION | F108-CF-100 AIRCRAFT ENGINE,KC-135R AIRPLANE |
| MATERIAL | RUBBER SYNTHETIC |
No substitute or cross-reference records for this part.