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MAINTENANCE
Honeywell HY!#b
Dimensions,
including
bracket
(maximum):
Length
(TM-260)
.. ..... .. ... ... .. ..... .. ... ..
11.28
in.
(286.5 mm)
Length
(SM-600)
.. .. .. ... ...... .. .... . .... ...
11.75
in. (298.5 mm)
Width .......................................
8.08 in. (205.2 mm)
Height ......................................
4.17 in. (105.9 mm)
Weight including bracket (maximum) ................
10.2 lb (4.63 kg)
Power Requirements:
Clutch ........................................... 28 V dc, 1.9 VA
Synchro .................................... 26 V, 400 Hz, 10.4 VA
Mating Connector:
J1 (TM-260, SM-600) ............................... MS27473E12A35S
J2 (TM-260, SM-600) .............................. MS27473E12A35SA
J1 (TB-261) ....................................... MS27473E1OA35S
J2 (TB-261) ...................................... MS27473E1OA35SA
Mounting ................................................. Hard Mount
SM-600 and TM-260 Dual Servo
Leading Particulars
Table 7-5
The dual servo translates electrical inputs into a brake controlled
rotational mechanical output. The tachometer output is fed back to the
flight guidance computer servo amplifier to null the command signal. The
SM-600 synchro position output is not used in the system.
Each servo of the dual servo is identical and is connected to a separate
output connector. Servo connector J1 is connected to the pi1ot's flight
guidance computer, and connector J2 is connected to the copilot's side.
The active flight guidance computer provides a brake output to disable
the other servo.
22-14-00
Page 198.65/198.66
Aug 15/91
Use or disclosure Of information on this page is sub]ecl to the restrictions on the title page of this document.
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