Support Software Equipment - Honeywell PRIMUS 1000 Pilot's Manual

R
PRIMUS 1000 Integrated Avionics System
Model
AZ–850 Micro Air Data Computer
(MADC) with RVSM (Reduced
Vertical Separation Minimums)
RG–204 Rate Gyro
AG–222 Accelerometer
RNZ–850 Integrated Navigation (NAV)
Unit
RNZ–850B
RCZ–833E Communications Unit with
Diversity Transponder, 8.33
kHz. (See Note 3, following)
RCZ–833F Communications Unit without
Diversity Transponder (See
Note 3, following)
Table 1–2 lists support software equipment.
Model
ECP–800 Programmable Checklist
NOTES: 1. This manual describes all system capabilities. The
2. The artwork shown in this manual is typical. Specific
3. Two communication units will be installed on the
Introduction
1-4
Unit
Equipment List
Table 1–1
Unit

Support Software Equipment

Table 1–2
items noted as optional are not necessarily included in
the standard offering.
installations may vary.
aircraft, but specific configuration will be at owner's
discretion. Possibilities include:
- Both with 8.33 kHz
- Neither with 8.33 kHz
- Pilot's side only with 8.33 kHz
- Copilot's side only with 8.33 kHz.
Qty Part No.
2 7014700–601
1 7007453–903
2 7000992
1 7510100–931
1 7510100–933
2 7510700–866
2 7510700–867
Qty Part No.
1 7021060–901
A28–1146–134
REV 1 Jan/03