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, left hand p/n k870302-103; fairing assembly, aft upper, left hand p/n k870302-105; and fairing assembly, aft lower, left hand p/n k870302-107; station location sta 120.75; opposite of p/n k870302-102
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 6105-01-354-5874
NSN 6240-01-301-8668
NSN 5985-01-629-6477
NSN 6150-00-159-0813
NSN 6105-01-264-5443
NSN 6135-01-014-9755
NSN 5960-00-287-9932
NSN 5990-01-357-6175
NSN 6320-01-302-5157
NSN 5999-01-626-4265
NSN 5930-00-119-8684
NSN 5855-01-167-2162