4135040: DAMPER,TURBINE BLADE,AIRCRAFT TU.
DAMPER,TURBINE BLADE,AIRCRAFT TU. Key specifications include end_item_identification: F135-PW-100 ENGINE ON F-35 AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 4730-01-074-6965, 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.
| end_item_identification | F135-PW-100 ENGINE ON F-35 AIRCRAFT |
| NSN | 4730-01-074-6965 |
| CONNECTION STYLE | PLAIN (PIPE) ALL ENDS |
| CONNECTION TYPE | THREADED INTERNAL PIPE ALL ENDS |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-C-390 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| OPERATING PRESSURE | 125.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| LEG LENGTH | 0.710 INCHES NOMINAL ALL ENDS IN |
| NOMINAL THREAD SIZE | 0.250 INCHES ALL ENDS IN |
| SPECIFICATION/STANDARD DATA | 81348-WW-P-460B GOVERNMENT SPECIFICATION |
| MAXIMUM OPERATING TEMP | 150.0 FAHRENHEIT SINGLE RESPONSE DEGF |
| NONDEFINITIVE SPEC/STD DATA | A CLASS |
| MEDIA FOR WHICH DESIGNED | STEAM SINGLE RESPONSE |