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TM 11-6625-646-15
C1
c. .. Width........................................ 20.75 inches
b. During open loop testing, the channel output is
d. .. Weight ..................................... 63.25 pounds
routed directly through a meter multiplier resistor and
relay contacts to the metering circuit output of the
1-12. Theory of Operation
actuator-simulator card at pins 20 and 23 of receptacle
J64.
1-13. The test set consists of essentially independent
c. During closed loop testing, the channel output is
circuits which simulate signals normally produced by the
converted to a positive or negative dc voltage, chopped,
extensible links, the pitot-static system, and the yaw
converted to a nominal sine wave, amplified, and fed
(sideslip) ports in the helicopter. The test set includes
back to the SAS amplifier as a simulated feedback
circuits to check the output of each channel of the SAS
signal (para 1-18 through 1-25).
This simulated
amplifier, the demodulator-modulator card, the amplifier
feedback signal is also rectified on the actuator-
card, the metering circuits, and the half-gain mode
simulator card and connected through relay contacts to
circuit. An ASE mode test circuit is not used for CH-47
the metering circuit output at pins 20 and 23 of
SAS amplifiers. Each channel test circuit includes an
receptacle J64.
actuator simulator card.  The demodulator-modulator
card test circuit includes an amplifier card. The test set
d. The open or closed loop metering circuit output
also contains ac and dc power supplies and a pneumatic
of the actuator-simulator card from receptacle J64 pins
system. The power supplies enable operation of the test
20 and 23 is routed to ROLL AXIS meter M3 through
set and the SAS amplifier circuits.  The pneumatic
adapter switch S5.
system enables testing of airspeed and sideslip circuits.
e. The feedback signal output of the actuator-
Refer to figure 1-2 for the schematic diagram of the
simulator card from receptacle J64 pin 25 is routed to
actuator-simulator card.  Refer to figure 1-3 for the
jumpered pins U and W of receptacle J60. From this
schematic diagram of the amplifier card. Refer to figure
point, the signal is routed to the SAS amplifier feedback
1-4 for the schematic diagram of the function meter
(cancellation) circuits.
circuits. Refer to figure 1-5 for the overall schematic
diagram of the test set.  Refer to figure 1-6 for the
f. The 2.5-volt ac feedback resistor excitation
pneumatic system schematic. Refer to figure 1-7 for the
voltage from the SAS amplifier channel is connected to
adapter schematic.
pins V and X of receptacle J60. From pins V and X the
excitation voltage is connected to the reference voltage
1-14. Channel Test Circuits
input of the actuator-simulator card at pins 8 and 9 of
receptacle J64.  On the actuator-simulator card, the
1-15. Roll Channel
excitation voltage is used to phase-relate the operation
of a chopper stage to the operation of the SAS amplifier
The roll channel test circuit measures the open and
channel (para 1-22).  The excitation voltage is also
closed loop channel output of a SAS amplifier under
connected to the ac metering circuits through the ROLL
test.
(or PITCH) FEEDBACK POT. EXCITATION position of
a. The channel output signal is connected to pins
FUNCTION switch S7 (para 132).
R, S, and T of receptacle J60. From here the signal is
g. From pins p of SAS amplifier receptacle J1 and
connected through pins 2, 3 (dc common), and 5 of
adapter receptacle J101, 26 volts ac is connected to the
receptacle J64 to the phase inverter stage of the
primary of adapter transformer T101.  A primary tap
actuator-simulator card. The differential output of the
supplies approximately 13-volt ac to SAS amplifier roll
SAS amplifier channel at pins 2 and 5 is also connected
signal demodulator Q302.  The secondary of T101 is
by jumper wires to pins 21 and 24 of receptacle J64.
connected through dropping resistors R101
Only one of these simulator card input circuits is active,
depending on the mode of test set operation selected by
AXES METERS READ switch S4.
3

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