TM 1-1520-238-T-7
11–215
11–27.
DASE– WIRING INTERCONNECT DIAGRAM (COLLECTIVE) (BUCS DEACTIVATED) (cont)
11–27
NOTES:
HIGHWAY USE: THE ALPHA CHARACTER IDENTIFIES A SPECIFIC LINE, AND THE NUMBER IN
PARENTHESIS IDENTIFIES THE SHEET NUMBER WHERE THE SIGNAL TERMINATES.
1.
0 VAC AT MID TRAVEL; 10 VAC WITH COLLECTIVE STICK FULLY UP OR DOWN.
2.
±4 MA MAXIMUM CURRENT VARIATION.
3.
0 VAC AT MID TRAVEL; 2.5 VAC AT MAXIMUM TRAVEL.
4.
0 VAC AT MID TRAVEL; 5 VAC AT MAXIMUM TRAVEL.
5.
RELAY ACTUATED BY SQUAT SWITCH S350. ON GROUND - CONTACTS B2 AND B3 CLOSED,
SQUAT RELAY DE-ENERGIZED. AIRBORNE - CONTACTS B2 AND B1 CLOSED, SQUAT
RELAY DE-ENERGIZED.
6.
VARIES FROM APPROX. 0.5 VDC TO 5 VDC; WITH NO CHANGE AT SOURCE.
7.
MAGNETIC SWITCHES; SOLENOID HOLDS SWITCH ON WHEN MANUALLY SET TO ON.
8.
28 VDC IN ONLY WHEN BUCS SELF TEST SWITCH IS HELD IN PLT OR CPG POSITION.
9.
ELECTRICAL SYSTEM (TM 1-1520-238-T-6).
10.
HS DESIGNATES A HARD SPLICE WHICH CANNOT BE DISCONNECTED.
M DESIGNATES A SOFT SPLICE WHICH MAY BE DISCONNECTED FOR A WIRING CHECK.
11.
AVIONICS CONFIGURATION HEADING ATTITUDE REFERENCE SYSTEM (HARS) (TM 11-1520-238-23-2).
12.
HYDRAULIC SYSTEM (TM 1-1520-238-T-5).
13.
REFER TO PARAGRAPH 11-89. STABILATOR - WIRING INTERCONNECT DIAGRAM.
14.
REFER TO PARAGRAPH 11-26. DASE - WIRING INTERCONNECT DIAGRAM (YAW) (BUCS DEACTIVATED).
15.
REFER TO PARAGRAPH 11-25. DASE - WIRING INTERCONNECT DIAGRAM (ROLL) (BUCS DEACTIVATED).
16.
REFER TO PARAGRAPH 11-24. DASE - WIRING DIAGRAM (PITCH) (BUCS DEACTIVATED).
17.
FIRE CONTROL SYSTEM - MULTIPLEX SUBSYSTEM (TM 9-1230-476-20-2).
18.
REFER TO PARAGRAPH 11-28. BUCS ACTIVATED - WIRING INTERCONNECT DIAGRAM.
M70-220-14A
SHEET 14 OF 14
