TB 1-4920-443-35
AEDATS IV T53/T55/T63 ALIGNMENT WORKSHEET
(2) Gas producer speed indication (GP),
(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 T55 Flight Harness pins G and H.
2 T53 Flight Harness pins G and H
3 T63 Flight Harness 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%
(N1)
+/- .3%
+/- .01hz
7hz (10%)
____________
____________
____________
____________
28hz (40%)
____________
____________
____________
____________
42hz (60%)
____________
____________
____________
____________
56hz (80%)
____________
____________
____________
____________
70hz (100%)
____________
____________
____________
____________
T53 - Transducer: T43
Hardware Name: F01
T55 - Transducer: T44
Hardware Name: F01
T63 - Transducer: T45
Hardware Name: F01
No alignment requirement must verify frequencies.
(3) Over speed power section #1, T53/T55/T63
(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
+/- .3Hz
3800
In limit
____________
90% alarm ____________
3700
90%
____________
100% alarm ____________
3333
100%
____________
Audible
____________
alarm
Note: over speed power section #2 is not connected
174