DAMPER,TURBINE BLADE,AIRCRAFT TU. Key specifications include end_item_identification: F135-PW-100 ENGINE ON F-35 AIRCRAFT, Form Factor: Blade. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) 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 |
| Form Factor | Blade |
| NSN | 4730-01-074-6965 |
| OPERATING PRESSURE | 125.0 POUNDS PER SQUARE INCH (PSI) MAXIMUM SINGLE RESPONSE LBS |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-C-390 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
| CONNECTION TYPE | THREADED INTERNAL PIPE ALL ENDS |
| MAXIMUM OPERATING TEMP | 150.0 FAHRENHEIT SINGLE RESPONSE DEGF |
| CONNECTION STYLE | PLAIN (PIPE) ALL ENDS |
| LEG LENGTH | 0.710 INCHES NOMINAL ALL ENDS IN |
| MEDIA FOR WHICH DESIGNED | STEAM SINGLE RESPONSE |
| THREAD SERIES DESIGNATOR | NPT ALL ENDS |
| NONDEFINITIVE SPEC/STD DATA | A CLASS |
| NOMINAL THREAD SIZE | 0.250 INCHES ALL ENDS IN |