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 5945-01-422-5394
NSN 5998-00-606-3659
NSN 2925-00-402-5582
NSN 5945-00-254-6031
NSN 5835-00-130-6404
NSN 5835-01-632-6627
NSN 6320-01-334-9840
NSN 5990-01-651-6364
NSN 2925-00-225-5386
NSN 6150-01-343-2924
NSN 2925-01-329-3665
NSN 5975-00-166-0614