TM 1-1520-238-T-7
11–116
11–13.
FLIGHT CONTROL SYSTEM – WIRING INTERCONNECT DIAGRAM (cont)
11–13
4 TO 5,7 TO 8, 10 TO 11
TERMINALS CONNECTED
(PERMANENT)
28 VDC INPUT ACTIVITIES MAGNETIC BRAKE (FORCE TRIM ON).
PRESENT AT FORCE TRIM RELEASE.
WITH PILOT OR CPG FORCE TRIM SWITCH AT FORCE TRIM
WITH PILOT FORCE TRIM SWITCH AT FORCE TRIM ON POSITION.
PUSHBUTTON SWITCH, USED ONLY FOR FORCE TRIM RELEASE.
6.
RELEASE POSTION.
FORCE TRIM RELEASE
SHOWN AT FORCE TRIM ON POSITION. SPRING LOADED FROM
FORCE TRIM RELEASE POSITION TO FORCE TRIM ON POSITION.
FORCE TRIM ON
7. ELECTRICAL SYSTEM (TM 1-1520-238-T-6).
FORCE TRIM OFF
(MOMENTARY RELEASE)
ON = 28 VDC
5.
(NORMAL)
SWITCH POSITION
NOTES:
2.
5 TO 6,8 TO 9, 11 TO 12
4 TO 5,8 TO 9, 10 TO 11
OFF = OPEN
3.
4.
1.
AVIONICS CONFIGURATION HEADING ATTITUDE REFERENCE SYSTEM (HARS) (TM 11-1520-238-23-2).
8.
M70-001-3
SHEET 3 OF 3
HIGHWAY USE: THE ALPHA CHARACTER IDENTIFIES A SPECIFIC LINE, AND THE NUMBER IN
PARENTHESIS IDENTIFIES THE SHEET NUMBER WHERE THE SIGNAL TERMINATES.
