TB 43-0123
AN/ASN-86
JUX
(Illustration Not Available)
AN/ASN-86 Inertial Navigation Set
PL-1306/U
X
1. Brief Description: The AN/ASN-86 Inertial Navigation
TK-90/G
X
X
Set is a self contained navigation and attitude-reference
TK-100/G
X
system that is totally independent of aircraft maneuvers,
TK-101/G
X
weather conditions and terrain. The AN/ASN-86 permits
TK-105/G
X
flight to a predetermined surveillance area under instrument
1801A
X
flight rules (IFR) conditions. Simultaneously the navigation
1821A
X
set provides a visual display of present position data in
8802B
X
universal transverse macerator (UTM) coordinates or
8806B
X
conventional latitude coordinates during all phases of the
flight. When a suspected target is picked up, the AN/ASN-
NOTE
86 will display and/or freeze the geographical coordinates of
the aircraft's position. The input power requirements are 28
volts DC at 26 amps and 115 volts AC, 400 Hz at 510 watts
Refer to TM 11-5826-245-34P for
initial warm-up requires 1350 watts for a maximum .05
additional tools and test equipment not
minute). The major components of this set are as follows:
having part numbers or AN type
designators.
CP-941/ASN-86 .............
Navigational Computer
ID-1579/ASN-86 ............
Control-Indicator
3. Applicable Publications:
MT-4074/ASN-86...........
Mount (for MX-8123/ASN-86)
TM 11-5826-245-20
or
TM 11-5826-245-20P
MT-4447ASN-86............
Mount
TM 11-5826-245-34/1
MT-4075/ASN-86...........
Mount (for CP-941/ASN-86)
TM 11-5826-245-34/2
MX-8123/ASN-86 ..........
Gyro Stabilized Platform
TM 11-5826-245-34/3
Type
AVUM
AVIM
TM 11-5826-245-34P
2. Applicable Tools and Test Equipment:
See appendix B for nomenclature, NSN, etc.
Type No.
AVUM
AVIM
AN/ASM-385
X
AN/ASM-386
X
AN/USA-34
X
X
AN/USM-207A
X
AN/USM-223
X
AN/USM-281A
X
AN/USM-365(V)1
X
ME-202A/U
X
ME-223AIU
X
MT-4145/ASN-86
X
MX-8474/ASN-86
X
II-B-23
