Two temperature sensors embedded within fiberglass structure of forward fairing for temp. Monitoring; socket head cap screws are secured with lockwire; components normally shipped looseunless specifically defined by purchase order; fairing construction thickness 0.100 in. Except in areas of temp. Sensors, electrical lead wire, flanges, hardware attachment or as specified; assembly consists of fairing assembly, forward, right hand p/n k870 302-104; fairing assembly, aft upper, right hand p/n k870302-106; fairing assembly, aft lower, right hand p/n k870302-108; station location sta 120.75; opposite of p/n k870302-101
A secondary structure whose function is to reduce drag by providing a streamlined surface or covering.
Classification: Other parts, nesoi, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communication satellites)
NSN 5935-00-468-6074
NSN 6650-01-350-0067
NSN 6110-01-037-4863
NSN 6320-01-371-3047
NSN 7035-01-287-9817
NSN 4140-01-312-8632
NSN 6240-01-487-6459
NSN 5945-00-994-4602
NSN 4140-01-406-2054
NSN 5985-00-268-3778
NSN 5960-01-474-4843
NSN 5930-00-103-9313