TM 1-1520-238-T-7
11–201
11–26.
DASE – WIRING INTERCONNECT DIAGRAM (YAW) (BUCS DEACTIVATED) (cont)
11–26
NOTES:
HIGHWAY USE: THE ALPHA CHARACTER IDENTIFIES A SPECIFIC LINE, AND THE NUMBER IN PARENTHESIS
IDENTIFIES THE SHEET NUMBER WHERE THE SIGNAL TERMINATES.
1. 10 VAC WITH DIRECTIONAL PEDALS FULL LEFT OR FULL RIGHT.
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. AIRBORNE - CONTACTS B1 AND B2 CLOSED. SQUAT RELAY ENERGIZED.
6. VARIES BETWEEN MAXIMUM LIMITS SHOWN. DEPENDS ON AIRSPEED CHANGE DATA.
7. ABOVE 60 KNOTS PROVIDES AUTOMATIC TURN COORDINATION 25
º MAXIMUM RANGE.
8. MAGNETIC SWITCHES, SOLENOID HOLDS SWITCH ON WHEN MANUALLY SET TO ON.
9. TWO - MINUTE TURN RATE: 2.6 VDC MINIMUM.
10. ASE INDICATORS LIGHT WHEN DASEC REMOVES 28 VDC.
11. VARIES BETWEEN APPROXIMATELY 0.5 VDC TO 5 VDC WITH NO CHANGE AT SOURCE.
12. ELECTRICAL SYSTEM (TM 1-1520-238-T-6).
13. AVIONICS CONFIGURATION VIDEO DISPLAY UNIT (TM 11-1520-238-23-2).
14. HS DESIGNATES A HARD SPLICE WHICH CANNOT BE DISCONNECTED.
M DESIGNATES A SOFT SPLICE WHICH MAY BE DISCONNECTED FOR A WIRING CHECK.
15. SCAS = STABILITY COMMAND AUGMENTATION SYSTEM.
16. REFER TO PARAGRAPH 11-25. DASE - WIRING INTERCONNECT DIAGRAM (ROLL) (BUCS DEACTIVATED) .
17. AVIONICS CONFIGURATION HEADING ATTITUDE REFERENCE SYSTEM (HARS) (TM 11-1520-238-23-2).
18. REFER TO PARAGRAPH 11-24. DASE - WIRING INTERCONNECT DIAGRAM (PITCH) (BUCS DEACTIVATED).
19. REFER TO PARAGRAPH 11-27. DASE - WIRING INTERCONNECT DIAGRAM (COLLECTIVE) (BUCS DEACTIVATED).
20. REFER TO PARAGRAPH 11-89. STABILATOR - WIRING INTERCONNECT DIAGRAM.
21. AIR DATA SYSTEM (TM 9-1230-476-20-2).
22. FIRE CONTROL SYSTEM - MULTIPLEX SUBSYSTEM (TM 9-1230-476-20-2).
M70-221-7A
SHEET 7 OF 7
