L5338270-001: DUCT ASSEMBLY,AIR CONDITIONING-H.
DUCT ASSEMBLY,AIR CONDITIONING-H. Key specifications include material: ALUMINUM ALLOY 6061, overall_length: 3.500 INCHES NOMINAL IN, aircraft_location: CREW AIR OVERHEAD SUPPLY, material_thickness: 0.035 INCHES NOMINAL IN, aircraft_station_number: YF325.7, end_item_identification: B-1B AIRCRAFT. This part is cataloged in the U.S.
Government catalog under NSN 1660-01-166-1220, 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 6061 |
| overall_length | 3.500 INCHES NOMINAL IN |
| aircraft_location | CREW AIR OVERHEAD SUPPLY |
| material_thickness | 0.035 INCHES NOMINAL IN |
| aircraft_station_number | YF325.7 |
| end_item_identification | B-1B AIRCRAFT |
| aircraft_mission_design_series | B-1B |
| material_document_and_classification | WW-T-700/6 FED SPEC SINGLE MATERIAL RESPONSE |
| NSN | 1660-01-166-1220 |
| AIRCRAFT STATION NUMBER | YF325.7 |
| MATERIAL DOCUMENT AND CLASSIFICATION | WW-T-700/6 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 3.500 INCHES NOMINAL IN |
| MATERIAL THICKNESS | 0.035 INCHES NOMINAL IN |
| SPECIAL FEATURES | CONSIST OF WEB TUBE; WEB,ALUMINUM ALLOY SHEET 6061-0 PER QQ-A-250/11; FLANGE,ALUMINUM ALLOY SHEET 6061-0; TUBE 1.250 IN. OD; WEB 0.600 IN. LG,O.O4O IN. THK,0.380 IN WD; FLANGE 1.500 IN. LG,0.040 IN. THK,1.500 IN. WD IN |
| AIRCRAFT LOCATION | CREW AIR OVERHEAD SUPPLY |
| END ITEM IDENTIFICATION | B-1B AIRCRAFT |
| MATERIAL | ALUMINUM ALLOY 6061 |
| AIRCRAFT MISSION DESIGN SERIES | B-1B |
No substitute or cross-reference records for this part.