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General Electric Aircraft Engines
Part # 2158M43G01=CW Forecastable
Forecastable
First Leg Thickness: 0.057 Inches Minimum and 0.069 Inches Maximum Second Leg Style: Angle First Leg Angle: 85.8 Degrees Nominal End Item Identification: F110 Engine Special Features: Two Rivet Holes, 0.100 In, One Each On Alternate Sides Of Larger Second Leg Hole Along Length First Leg Hole Diameter: 0.274 Inches Minimum and 0.288 Inches Maximum Style Designator: Angle First Leg Style: Angle Features Provided: Nut Material: Nickel Alloy K-500 Second Leg Thickness: 0.057 Inches Minimum and 0.069 Inches Maximum Second Leg Hole Arrangement Style: Three Holes Second Leg Hole Diameter: 0.274 Inches Minimum and 0.288 Inches Maximum First Leg Hole Arrangement Style: One Hole Second Leg Relationship To First Leg: Not Identical
Harmonized Tariff Schedule Code DISCLAIMER: Product information provided “as is.” Boeing may add, change, discontinue or remove this information at any time. Product photos may not be exact match to product delivered. Seeterms & conditions .
