TM 1-1520-238-T-7
11–187
11–24.
DASE – WIRING INTERCONNECT DIAGRAM (PITCH) (BUCS DEACTIVATED) (cont)
11–24
NOTES:
1.
0 VAC AT MIDTRAVEL (CYCLIC STICK CENTERED). 10 VAC AT MAXIMUM TRAVEL
(CYCLIC STICK FULL FORWARD OR FULL AFT).
2.
+4 MA MAXIMUM CURRENT VARIATION.
3.
0 VAC AT MIDTRAVEL, 2.5 VAC AT MAXIMUM TRAVEL.
4.
0 VAC AT MIDTRAVEL, 5 VAC AT MAXIMUM TRAVEL.
5.
RELAY ACTUATED BY SQUAT SWITCH S350.
ON GROUND - CONTACTS B2 AND B3 CLOSED, SQUAT RELAY DE - ENERGIZED.
6.
AIRBORNE - CONTACTS B2 AND B1 CLOSED, SQUAT RELAY ENERGIZED.
7.
VARIES FROM APPROX. 0.5 VDC TO 5 VDC WITH NO CHANGE AT SOURCE.
8.
VARIES BETWEEN MAXIMUM LIMITS SHOWN. DEPENDS ON AIRSPEED CHANGE DATA.
9.
MAGNETIC SWITCHES, SOLENOID HOLDS SWITCH ON WHEN MANUALLY SET TO ON.
10.
ELECTRICAL SYSTEM (TM 1-1520-238-T-6).
11.
AIR DATA SYSTEM (TM 9-1230-476-20-2).
12.
SCAS = STABILITY COMMAND AUGMENTATION SYSTEM.
13.
HS DESIGNATES A HARD SPLICE WHICH CANNOT BE DISCONNECTED.
M DESIGNATES A SOFT SPLICE WHICH MAY BE DISCONNECTED FOR A WIRING CHECK.
14.
REFER TO PARAGRAPH 11-25. DASE - WIRING INTERCONNECT DIAGRAM (ROLL) (BUCS DEACTIVATED).
15.
REFER TO PARAGRAPH 11-26. DASE - WIRING INTERCONNECT DIAGRAM (YAW) (BUCS DEACTIVATED).
16.
REFER TO PARAGRAPH 11-27. DASE - WIRING
INTERCONNECT DIAGRAM (COLLECTIVE) (BUCS DEACTIVATED).
17.
REFER TO PARAGRAPH 11-89. STABILATOR - WIRING INTERCONNECT DIAGRAM.
18.
AVIONICS CONFIGURATION HEADING ATTITUDE REFERENCE SYSTEM (HARS) (TM 11-1520-238-23-2).
19.
FIRE CONTROL SYSTEM - MULTIPLEX SUBSYSTEM (TM 9-1230-476-20-2).
HIGHWAY USE: THE ALPHA CHARACTER IDENTIFIES A SPECIFIC LINE, AND THE NUMBER IN
PARENTHESIS IDENTIFIES THE SHEET NUMBER WHERE THE SIGNAL TERMINATES.
M70-219-8
SHEET 8 OF 8
