Part Number 1-160-123-01 Fuel Manifold Nut

Manifold assembly, fuel, p/n 1-160-210-01, engine, T53, turboprop aircraft

Cres per ams 5645, 46.5 to 63.0 hardness rating rockwell c scale, 0.540 in. O/a lg, 0.530 in. Od, 0.468 in. Id, countersink 120 degrees to 0.450 in. Diameter 0.4375-20 UNF-3B thd

99193

• Schedule B: 7318160000
• SITC: 69421
• End Use: Finished metal shapes
• NAICS: 332722
• USDA: 1

Nuts of iron or steel