TB 43-0123
UH60 CIS
(Illustration Not Available)
UH-60 Command Instrument System
1. Brief Description: The UH-60 Command Instrument
2. Applicable Tools and Test Equipment: See
System is an integrated navigational system based on a
central computer that processes signals from navigation
and flight instruments/systems to produce visible
steering commands allow the pilot to fly a desired
Type No.
AVUM
AVIM
AN/USM-223
X
heading, reach a selected course, make an ILS landing
SG-13/ARN
X
and keep at a fixed altitude. The CIS receives primary
TK- 1OO/G
flight information from the AFCS, attitude indicating
X
system, compass system and radar altimeter.
TK-101/G
X
Navigational inputs are obtained from the VOR/MB/GS
system, the Doppler navigational system and the No. 1
3. Applicable Publications:
VHFIFM system. Major components are:
TM 11-1520-237-23-1 (Pertains to UH-60 Aircraft)
TM 11-1520-237-23-2 (Pertains to UH-60 Aircraft
C-10998/A ........... HNSI Mode Select Panel (2 ea)
TM 11-1520-237-23-3 (Pertains to UH-60 Aircraft )
C-10999/A ........... CIS Mode Select Panel
TM 11-1520-237-23P (Pertains to UH-60 Aircraft)
CP-1470/A ........... CIS Processor
ID-2277/A ............. Vertical Situation Indicator (2 ea)
ID-2278/A ............ Horizontal Situation Indicator (2 ea)
MT-6226/A ........... Mount (CP-1470)
II-H-5
