Honeywell SPZ-8000 Maintenance Manual page 53

A/c
Ref
System Component
Qty Honeywell Part No. Des
LASEREF@ II Inertial Reference Unit 2
HG1075AEO3 (PHASE 2) N/A
HG1075AEO4 (See Note)
HG1075GEO4 (See Note)
NOTE: The HG1075AEO4 LASEREF @ II were factory installed on aircraft 1164
and subsequent. The HG1075AEO4 functions identically to the AE03, but
the AE04 has been reconfigured to facilitate updating to the optional
HG1075GEO4. The GE04 has the same functions as the AE03 and AE04, but
will also interface with GPS and provide IRS, GPS, and hybrid GPS/IRS
outputs.
Attitude Heading Reference Unit
1**
HG1076AAO1 N/A
Mode Select Unit 1 CG1227AC10/ACOl* N/A
Inertial System Display Unit (ISDU) 1 CGl136AC10/AC20* N/A
LASERTRAKW Navigation Display Unit
l*** CG1230AC10/AC20*
N/A
CG1230AC11/AC21
(EFIS DISPLAY OPTION)
CG1230AG11/AG21*
(GPS READ OUTS)
Engine Pressure Ratio Transmitter 2 LG1189BC03
(4063258-3)
O~tional VLF/Omeqa System Components
OZ-800 Receiver Processor Unit
1 7004608-901
(Omega/VLF)
AT-800 Antenna Coupler Unit, 1 7011102
Teardrop H-Field
AT-801 Ant~;na Coupler Unit,
1 7011103
Brick H-Field
AT-803 Ant~;na Coupler Unit, 1 7011100
Blade E-Field
Oc)tionalLSZ-850 Licthtninq Sensor System Com~onents
LP-850 Lightning Sensor Processor 1 7011822-903
LU-860- Lightning Sensor Controller 1 7012738-905/-906*
N/A
141
142
142
142
145
146
System Components
22-14-00
Table 1 (cent) Page 4
Apr 15/93
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