CHARGE
AMPLIFIER
________________
_______ _______
CHARGE
AMPLIFIER
2C6461P08
TRIM
BALANCE
ANALYZER
2C6398
2C6461P04
110V
AC
50/400
Hz
2C6461P03
2C6461P04
OR
2C14963P18
AIRCRAFT
CONNECTOR
PMC)
(ENGINE
N0.
1
BRG
ACC
ENGINE
2C6398P43
N1
SPEED
CONNECTOR
2C14963P19
2C6398P45
COMPRESSOR
REAR
FRAME
CONNECTION
2C6461P10
ACCELEROMETER
CONNECTION
NO.
1
BEARING
SETTING
10-110
INT GND
50pC/g
GND
DIFF
CONTROL
SENS
(pC/g)
SENSITIVITY
DIAL
SHIELD
ACCELEROMETER
EXT
GND/INT
GND
ANALYZER
-
SD119C-50
____________________
_______ _______SETTING
FAST
10
VEL
D
IN
0
AUTO
TRACT
MINUS
MIDRANGE
CONTROL
DISPLAY
RANGE
MODE
TACH
TRIGGER
POT
PICKUP/AMP
FILTER
FAST SLOW
TACH
TRIGGER
TO
INPUT BEING
USED
INPUT
SELECTOR
1019742-04-A
720593 S00061423146_V1
Trim Balance Analyzer, 2C6398G08
Figure 501/72-52-00-990-801-G00
767
AIRCRAFT MAINTENANCE MANUAL
CF6-80A SERIES ENGINES
72-52-00
NoC
Page 509
D633T1B7 Aug 22/2017
ECCN 9E991 BOEING PROPRIETARY - Copyright © Unpublished Work - See title page for details
EFFECTIVITY
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