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 7035-01-441-4174
NSN 5835-01-098-8737
NSN 5920-01-252-8660
NSN 5990-01-512-9129
NSN 6650-01-376-1692
NSN 6650-01-212-3964
NSN 6650-01-139-9534
NSN 5990-01-304-7597
NSN 6220-01-164-5228
NSN 5935-01-306-8428
NSN 5999-01-099-5168
NSN 5835-00-930-8500