H16DW410-22

III End Item Identification: F-16A/B aircraftSpecial Features: Consists of connector P/N 16VE049001-52, -54;WAFER P/N 16VE049010-11, -12, -50;PLUG P/N 16VE049002-52, M83723/75R24619, MS27473T20F35PC, MS27473T20F35PD, MS27473T14F35SA, MS3116F8-4S, MS27473T16F35S;M83723/77R2255N, M83723/77R2461N, M83723/77R2041N, M83733/04RA051, M83723/28-20, MS27488-22;SPLICE P/N C4812-33, NAS1744-3;BUS P/N C8865-2, -3;ENDBELL P/NC8821-1-20, -22, C8821-2-15, C8824-2-21, C8824-1-24, C8822-1-24, C8822-2-17;SLEEVING P/N C8844-2, -3;SLEEVE P/N C8867-2;WASHER AN960PD6L;NUT P/N MS21042L06;SCREW P/N NAS1101-06-6;TERMINAL P/N M7928/1-13, -15, M7928/1-29;EXACT length to be determined on first installation;braid harness per 16PR106;SOLDER per MIL-STD-454D requirement 5III Fsc Application Data: Control, flight instrument, aircraft