Honeywell SPZ-8000 - Page 16

SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
Table of Contents
TC--7
Table of Contents (cont)
List of Illu strations
Figure Page
1--1 Challenger CL--601--3A Cockpit 1-5................
2--1 SPZ--8000 DIFCS Block Diagram 2-13..............
3--1 ADS Controls and Indicators 3-1...................
3--2 Mach/Airspeed Indicator 3-2......................
3--3 Barometric Altimeter 3-3..........................
3--4 Vertical Speed Indicator 3-5.......................
4--1 EFIS Components 4-1............................
4--2 Display Controller 4-2............................
4--3 Instrument Remote Controllers 4-5.................
4--4 Typical EADI Display 4-6.........................
4--5 EADI Displays and Annunciators 4-7...............
4--6 Takeoff Using Go--Around Mode 4-15................
4--7 Climb To Initial Altitude 4-16........................
4--8 Enroute Cruise 4-17...............................
4--9 Setup For Approach 4-18..........................
4--10 Approach Capture Tracking Below DH 4-19..........
4--11 Cockpit Reversion Switching Locations 4-20..........
4--12 EADI Reversion Annunciators 4-21..................
4--13 EADI Reversion Annunciators --
TCAS--Equipped Aircraft 4-21.....................
4--14 Source--Side IRS Reversion 4-22...................
4--15 Cross--Side IRS Reversion 4-23....................
4--16 No. 3 IRS Reversion 4-23..........................
4--17 Symbol Generator Reversionary Mode,
Cross--Side 4-24................................
4--18 MFD Symbol Generator Reversion 4-25.............
4--19 Symbol Generator Reversion Annunciator Location
for TCAS--Equipped Aircraft 4-26...................
4--20 Flight Director Reversionary Mode,
Couple Arrow 4-27..............................
4--21 CAT 2 Failure Annunciator Location 4-28.............
4--22 EADI Comparison Monitoring 4-29..................
4--23 Excessive Attitude Display 4-31.....................
4--24 EADI Failure Warning Flags 4-32...................
4--25 Attitude Failure Flag 4-33..........................