TB 1-4920-443-35
AEDATS IV T64 ALIGNMENT WORKSHEET
(2) Gas producer speed indication (NG)
(a) Set the calculating counter controls as follows: (Channel 1)
1 DEC
5
2 C
14286
3 10n
0
4 Auto
depressed
5 x10
released
6 Sample rate (fast)
1
7 Test
released
(b) Input the following frequencies into the flight harness connector
1 T64 Flight Harness Connector P89, Pins (A+) and (B-).
(c) Set the tachometer tester controls to
the following:
1 Motor direction-stop,
2 Set rpm-10%,
3 Power on
4 Set the motor direction switch to forward
Calculating
AEDATS 4
Gauge Analog
Gauge Digital
tester
counter
+/- .3%
+/- .3%
(NG)
+/- .3%
+/- 0.1%
7hz (10%)
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____________
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28hz (40%)
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42hz (60%)
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56hz (80%)
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70hz (100%)
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Transducer: T45 Hardware Name: F01
No alignment requirement must verify frequencies.
(3) Over speed power section #1 T64 (Refer to
page 37 step 41)
(a) Use the B. F Goodrich EPU to perform this test.
(b) Set the EPU to the second "MODE" display
(c) Cal: V=9.497 I=19.601 J2 CONN=3333 HZ
Thumbwheel
indication
Limit control
settings
indicator
+/- 3 Hz
3800
In limit
____________
90% alarm
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3700
90%
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100% alarm
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3333
100%
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Audible
____________
alarm
Note: over speed power section #2 is not connected
(4) Torque measurement system,
(a) Set the modulus code to
match the modulus code of
the torque shaft that is
installed in
the
dynamometer.
(b) Set the AEDATS channel 23 (QDyno) for T-64 engine
(c) Set the EPU to the first "MODE" display:
1 Display should read 512 Hz. 0 volt
2 TB 609 1 (+) 2(-) ______________ +/-20 mv
198