Description:

C-130 aircraft end item identification, plate, ident p/n 42-10918; pad, compression p/n 42-10924; wiring assy, aux p/n 42-10921; plate assy, base p/n 42-10915; cap, protection p/n 10-101960-18-3; cable assy, flexible p/n 42-10931; lug, terminal p/n ms25036-1; nameplate p/n 50-51042-12; bracket p/n ms24693s26; cover assy p/n 42-10914; angle nut plate 8; wiring assy, main wheel p/n 42-10919 4; gasket, end plate p/n 42-10923 2; plate, end p/n 42-10917 2 .

Special Features:

Plate, ident p/n 42-10918; pad, compression p/n 42-10924; wiring assembly, aux p/n 42-10921; plate assembly, base p/n 42-10915; cap, protection p/n 10-101960-18-3; cable assembly, flexible p/n 42-10931; lug, terminal p/n ms25036-1; nameplate p/n 50-51042-12; bracket p/n ms24693s26; cover assembly p/n 42-10914; angle nut plate 8; wiring assembly, main wheel p/n 42-10919 4; gasket, end plate p/n 42-10923 2; plate, end p/n 42-10917 2

Properties:

An electronic device which processes wheel speed sensor signals and generates command signals to the brake control valve which meters hydraulic brake pressure at slightly less than skid producing level. it also prevents brake application prior to touchdown and may receive direct cockpit electrical input to initiate braking.