NSN 1560-01-502-4629
Chord
About this product
1.500 inches material thickness, agav criticality code justification, inavy) angle, forward panel, aft fus; also known as stiffener part name assigned by controlling agency, aircraft mission design series: f/a18-e/f.
Manufacturer part number 74A341121-2007 for national stock number 1560015024629.
Datasheet
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Product description
Aircraft Stiffener NSN 1560-01-502-4629.
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MPN or Model
74A341121-2007
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Schedule B
8803.90.9060 (Other parts, nesoi, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communication satellites)) -
NMF (National Motor Freight)
011760 - Aircraft/aircraft Part Viz: -
Overall Length
5.500 inches -
Overall Width
2.000 inches -
Material Thickness
1.500 inches -
End Application
Fighter aircraft-first (f18 e/f) -
Criticality Code Justification
Agav -
Part Name Assigned By Controlling Agency
Inavy) angle, forward panel, aft fus; also known as stiffener -
Aircraft Mission Design Series
F/a18-e/f -
Material
Titanium -
Material Specification
Mil-t-9047 (6al-4v, cond a) military specification single material response
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Aircraft Stiffener
An item, generally a strip, designed to strengthen and resist loads by attachment to various components such as skins, ribs, pylons, and the like.
![Mechanic Bill explains Chord](/public/images/billy-thinking.png)
Pricing and Availability
Get a quote for 1560-01-502-4629 aircraft stiffenerManufacturer Part Numbers and Alternates
MPN manufacturer part number | Registrant or Supplier |
---|---|
74A341121-2007 | Northrop Grumman Systems Corporation |
74A341121-2007 | Boeing Company, The |
Stock Check
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