ARMY TM 9-6115-464-34
AIR FORCE TO 35C2-3-445-2
NAVY NAVFAC P-8-624-34
1.
2.
3.
4.
5.
6.
NOTES:
EXACT VALUES DETERMINED DURING TEST, SEE
TEST PROCEDURES DWG 69-737.
NOMINAL VALUES:
C3=8µF
C4=4µF
CB SHALL BE 30µF TO 120µF NON- POLARIZED,
TANTALUM. EXACT VALUE DEPENDS ON
GOVERNOR APPLICATION.
THROTTLE CLOSED BY CURRENT INCREASE IN
COIL A-B, OPEN THROTTLE DECREASES
OUTPUT OF TRANSDUCER.
ACTUATOR PISTON ATTACHED TO ENGINE
THROTTLE.
REFERENCES:
FOR CONTROL UNIT ASSEMBLY, SEE DWG
69-700
FOR WIRING DIAGRAM, SEE DWG 69-730
FOR WIRING HARNESS, SEE DWG 69-731
ALL COMPONENTS SHOWN OUTSIDE THE
DOTTED LINES ARE FOR REFERENCE ONLY.
Figure 3-74. 50/60 Hz Governor Control Unit Schematic Diagram, Drawing No. 69-729 (Sheet 1 of 2)
3-173
