TM 1-1520-238-T-5
877
811.
ENGINE INSTRUMENTS WIRING INTERCONNECT DIAGRAM (CONT)
811
M68-001-19
SHEET 19 OF 19
NOTES:
HIGHWAY USE: THE ALPHA CHARACTER IDENTIFIES A SPECIFIC LINE, AND THE NUMBER IN
PARENTHESIS IDENTIFIES THE SHEET NUMBER WHERE THE SIGNAL TERMINATES.
1.
FUEL SYSTEM (TM 1-1520-238-T-7).
2.
FLIGHT CONTROL SYSTEM (TM 1-1520-238-T-7).
3.
ELECTRICAL SYSTEM (TM 1-1520-238-T-6).
4.
AUXILIARY POWER UNIT (TM 1-1520-238-T-8).
5.
TORQUE SHARING SYSTEM (TM 1-1520-238-T-4).
6.
HS DESIGNATES A HARD SPLICE WHICH CANNOT BE DISCONNECTED.
M DESIGNATES A SOFT SPLICE WHICH MAY BE DISCONNECTED FOR A WIRING CHECK.
7.
HELICOPTERS WITH T700-GE-701C ENGINES INSTALLED ARE EQUIPPED WITH EMI SHIELDING.
8.
HELICOPTERS WITH T700-GE-701C ENGINES INSTALLED ARE EQUIPPED WITH DIGITAL
ELECTRONIC CONTROL (DECU).