Honeywell SPZ-8000 Pilot's Manual page 290

T
Takeoff using go--around mode, 4-15
Target alert warning, activation, B--4
Technical support, 9-1
Traffic alert and collision avoidance
system (TCAS II) (optional), 2-10
EADI, 4-9
TCAS messages and failure
annunciators, 4-36
TCAS resolution advisory, 4-14
TCAS--equipped aircraft
display, 4-21
EHSI, 4-38
arc mode with TCAS traffic
display, 4-57
TCAS failure, 4-63
TCAS submodes, 4-58
mode traffic display (optional),
5-18
Troubleshooting, 9-1
commonly used terms, 9-13
digital avionics, 9-2
flight fault summary, 9-8
flight guidance system typical
problems, 9-3
combined vertical and lateral
mode problems, 9-8
lateral mode problems, 9-3
vertical mode problems, 9-6
pilot writeup, 9-10
technical support, 9-1
Turn pitch controller, 6-5
pitch wheel, 6-5
TURN knob, 6-5
V
Vertical mode problems, 9-6
Vertical navigation mode, 8-50
vertical altitude hold , 8-50
vertical altitude select, 8-50
vertical flight level change, 8-50
A28--1146--055
REV 2
SPZ--8000 Digital Integrated Flight Control System
Index (cont)
vertical path mode, 8-51
Vertical speed hold mode, 8-41
Vertical speed indicator, 3-5
VOR (NAV) mode, 8-4
approach mode, 8-11
DIRECT TO function, 8-12
over station operation, 8-11
W
Weather radar controllers
PRIMUS
PRIMUS
Weather radar systems
PRIMUS
650, B--3
R
GAIN knob, B--7
LSS knob, B--5
RADAR mode select switch,
B--6
RANGE buttons, B--3
RCT button, B--3
SECT button, B--5
SLV annunciator, B--5
STAB button, B--4
TGT button, B--4
TILT knob, B--5
870, C--3
R
GAIN knob, C--11
GCR button, C--4
LSS select switch, C--7
mode select switch, C--7
RANGE buttons, C--3
SECT button, C--6
SLV annunciator, C--7
TGT button, C--5
TILT knob, C--6
TRB button, C--3
650 , B--1
R
description, B--2
in--flight compensation
adjustment, B--12
introduction, B--1
maximum permissible
exposure level, B--14
operating procedures, B--8
powerup, B--8
Index
Index--9