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> Figure 4.33. Torquemeter System (T53L701).
Electrical system
Figure 4.34. Electrical System.
Army Aircraft Gas Turbine Engines
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Figure 4.33. Torquemeter System (T53L701).
b.
Exhaust
gas
temperature
harness.
An
exhaust
thermocouple
harness,
consists
of an
electrical
connector,
a
shielded
manifold,
and six thermocouples, as shown in figure 4.36.
141