The PLUG ASSEMBLY,SEALING is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, design_type: FRICTION, surface_treatment: CHROMATE AND ANODIZE, end_item_identification: AIRCRAFT, AIRLIFTER C-17A; AIRCRAFT, STRATOLIFTER C-135; AIRCRAFT, B-1B; AIRCRAFT, EAGLE F-15 A, material_document_and_classification: QQ-A-225/6, T4 FED SPEC SINGLE MATERIAL RESPONSE OR QQ-A-225/6, T351 FED SPEC SINGLE MATERIAL RESPONSE, tube_outside_diameter_for_which_designed: 0.1553 INCHES MINIMUM AND 0.1562 INCHES MAXIMUM IN. This product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5340-01-243-7398, 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 | ALUMINUM ALLOY 2024 |
| design_type | FRICTION |
| surface_treatment | CHROMATE AND ANODIZE |
| end_item_identification | AIRCRAFT, AIRLIFTER C-17A; AIRCRAFT, STRATOLIFTER C-135; AIRCRAFT, B-1B; AIRCRAFT, EAGLE F-15 A |
| material_document_and_classification | QQ-A-225/6, T4 FED SPEC SINGLE MATERIAL RESPONSE OR QQ-A-225/6, T351 FED SPEC SINGLE MATERIAL RESPONSE |
| tube_outside_diameter_for_which_designed | 0.1553 INCHES MINIMUM AND 0.1562 INCHES MAXIMUM IN |
| opening_inside_diameter_for_which_designed | 0.110 INCHES NOMINAL IN |
| surface_treatment_document_and_classification | MIL-C-5541 MIL SPEC SINGLE TREATMENT RESPONSE AND MIL-A-8623, TYPEII MIL SPEC SINGLE TREATMENT RESPONSE |
| NSN | 5340-01-243-7398 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/6, ALLOY 2024, T4 FED SPEC SINGLE MATERIAL RESPONSE |
| END ITEM IDENTIFICATION | AIRCRAFT, AIRLIFTER C-17A; AIRCRAFT, STRATOLIFTER C-135; AIRCRAFT, B-1B; AIRCRAFT, EAGLE F-15 A |
| SPECIAL FEATURES | ALUM. ALLOY 2024-T4 QQ-A-225,C/O PLUG AND PIN,PLUG ANODIZED PER MIL-A-8625 TY 2,PIN ALODINED PER MIL-C-5541;PLUG 0.155/0.156 IN. DIA,0.238/0.252 IN. LG,PLUG CONTAINS A TAPERED BORE TO ACCOMMODATE PIN,0.180/0.194 IN. BORE DEPTH,0.122/0.123 IN. PIN DIA,0.160/0.170 IN. PIN LG,PIN CONTAINS A VENT HOLE THRU 0.030 IN. DIA,PLUG AND PIN ARE CHAMFERED IN |
| MATERIAL | ALUMINUM ALLOY 2024 |