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 5985-01-381-1018
NSN 5925-01-085-6444
NSN 6145-00-004-7323
NSN 6135-00-444-1402
NSN 7035-01-589-1281
NSN 6320-00-977-3930
NSN 6135-00-917-1894
NSN 6145-01-261-5150
NSN 7035-01-423-8343
NSN 5855-01-423-5839
NSN 5835-00-770-2843
NSN 6145-01-044-4922