TB 43-0123
AN/ASN-132
NSN: N/A
EIC: N/A
1. Brief Description: The Integrated Inertial Navigation
See appendix B for nomenclature, NSN, etc.
System (IINS) AN/ASN-132 provides self contained
navigation capability to U.S. Army EH-60 aircraft for short
Type No.
AVUM
AVIM
and/or long-range missions and can be updated wherever
AN/NSM-223
X
X
TACAN navigational facilities exist or manually without
TK-101/G
X
TACAN data. The IINS employs a serial bus data for data
TK-105/G
X
interchange within the IINS and with the external mission
Direct Support Test Setup
X
system computer. This system also interfaces with the
aircraft flight instruments and altimeter/encoder AAU-32A.
3. Applicable Publications:
Navigation sensor by path determination data is processed
by the Navigation Processor Unit (NPU). The IINS control
and data entry is accomplished by means of the Control
TM 11-5826302-12
and Display Unit (CDU). Major components of this set are:
TM 11-5826-302-20P
2. Applicable Tools and Test Equipment:
AN/UYK-64(V)2 ..............
Navigation Processor Unit
CN-158/ASN ...................
Standard Inertial Navigation
System
CN-11097/ASN-132........
Control Indicator
CV-3739/ASN-132(V) .....
Signal Data Converter
MT4915/A .......................
Mount (RT-1159A)
PN105749.......................
Mounting Rack (AN/UYK-
64(V)2)
PN880100-1 ...................
Mount (CN-1158/ASN)
RT-1159A/ARN-118 .......
Receiver-Transmitter
11-B-26
