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 6620-01-492-8470
NSN 5950-00-205-2932
NSN 5895-00-149-1110
NSN 5920-01-548-7960
NSN 6220-00-808-8434
NSN 5975-00-210-4652
NSN 5910-01-427-3819
NSN 5999-01-394-4919
NSN 6620-01-428-7072
NSN 6105-01-171-7748
NSN 6110-00-840-6560
NSN 5905-00-051-4226