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May 2013 71x
A v i o n i c s
AIRCRAFT SITUATION DISPLAYS
Manufacturerz
Model Display
Inputs Outputs
Units/Weight (lb.) Price
Remarks
TSO Display Size Size or Form Factor Power Required
Honeywell Aerospace
Bendix/King Avionics
9201 San Mateo Blvd. NE
Albuquerque, NM 87113
(855) 250-7027
www.bendixking.com
KDR 610
XM Weather
Receiver
see
rem arks
weather
displays via
XM satellite
interfaced to
Bendix/King
KMD 250,
KMD 550
and KMD
850 MFDs
1/1.5
$7,408
10-32 VDC
Part of an MFD system; data link
weather receiver provides high- speed
textual and graphical weather to the
coc kpit. Available weather products in-
clude composite NEXR AD radar, graphi
-
cal METARs, AIRMETS and SIGMETS.
The active ight plan ca n be overl aid on
all graphical weather images. System
enables user to pan, zoom and inter-
rogate areas of interest via joystick.
C157
see
rem arks
see remarks
Honeywell
MFRD
LCD
RS-232
ARINC
429, radar,
datalink,
EGPWS,
tr afc, NTSC
video
display
1/7.5
$52,327
28 VCD or
115 VAC
400 Hz
Multi-function display of weather
radar, trafc, terrain, navigation maps,
checklists.
C63c, C110a,
C113, C196
6 in. diag.
6.24 (w) x 4.82
(h) x 8.38 (panel
depth)
L-3 Avionics Systems
5353 52nd St. S.W.
Grand Rapids, MI 49512
(616) 949-660 0
Fax: (616) 285-4224
www.L-3avionics.com
Trilogy
ESI-1000
AMLCD;
optional NVG
com pat ibility
N/A N/A
1/2.22
$14,995
14 - 28 VDC
Electronic standby instrument designed
to level “A” software and hardware
compliances, the Trilogy ESI replaces
traditional standby instrumen ts and
combines at titude, altitude and
airspeed infomation into a compact
3.8-in. diagonal display while maintain-
ing a 3-ATI chassis design. Heading
is available when coupled with the
optional magnetometer. For xed-wing
and helicop ter applications.
C2d, C3e, C4c,
C6e, C10b,
C46a, C113,
C179
4.0 x 3.0
3-ATI chassis 4.0
x. 3.35 x 7.66
Trilogy
ESI-2000
AMLCD;
optional NVG
com pat ibility
N/A N/A
1/2.56
$15,700
14 - 28 VDC
Electronic standby instrument incorpo-
rates an internal battery to meet the
requirements for indepe ndent , dedi-
cated back-up power for aircraft without
dual elec trical system. The lithium ion
battery is integrated into the ESI-2000
hardware with a triple redundant safety
design and provides a minimum of 1 hr.
and up to 4 hr. of standby power. Head
-
ing is available when coupled with the
optional magnetometer. For xed-wing
and helicop ter applications.
C2d, C3e, C4c,
C6e, C10b,
C46a, C113,
C179
4.0 x 3.0.
3-ATI chassis 4.0
x. 3.00 x 6.7
GH-3900 ESIS
Active matri x
LCD
ARINC 429,
RS-232,
discrete and
analog
ARINC 429,
RS-232,
discrete and
analog
1/ 3.0
$41,000
Dua l 28 VDC
imputs (18
VD C emer-
gency power
Feat ures a lighter and shorter chassis
than previous models and allows
the inst a ller to dene multiple I/O
interfaces ., SSEC and VMO values. An
Aircraft co nguration PC Software Tool
simplies the setup of the unit, allowing
installers to dene and customize the
presentation of colors, ight cues and
navigation data. Designed for FAR Part
25, Part 23 (Class III & IV). Part 27 and
Part 29. Variety of air data and headiing
inpu t options as well as built-in acceler
-
ometers. Classied as Non-ITAR.
C2d, C3e, C4c,
C6e, C8e,
C10b, C34e,
C35d, C36e,
C40c, C46a,
C66c, C95a,
C106, C113,
C115b, C145c
3 ATI
8.33 x 3.19 x
3.19 x
GH-39RSU
ESIS
DU-42 Display
Acitve Matr ix
LCD
DU-42
Display:
3 ARINC
429; 1 USB
Serial Bus; 1
RS-232 Se-
rial Bus; 12C
Serial Bus; 1
Analog
Remote Sen-
sor Unit:
7 ARINC 429;
1 RS-232
Serial Bus; 6
Discrete
Pneumatic
pressure
ports
DU-42
Display:
1 ARINC 429
Remote Sen-
sor Unit:
3 ARINC 429;
2 Discrete; 2
Analog
DU-42 Display:
1.5
Remo te Sensor
Unit: 3.0
Call
manufactu rer
+28 VDC
nomi nal
Feat ures a 4.2-in. diagon a l igh-resolu-
tion display (DU-42) and a separate Re
-
mote Sensor Unitt (RSU). 1.5-in.-deep
display allows installation in aircraft
with limited space behind the panel.
Congura ble I/O interfaces and SSEC
and VMO values, as well as display
parameters. Designed for FAR Part 25
and Part 23 (Class III & IV aircraft, and
Part 27 and Part 29 helicopters.
DU-42 Display:
C2d, C3e, C4c,
C6e, C8e,
C10b, C34e,
C35d, C36e,
C40c, C46a,
C66c, C95a,
C106, C113a
Remo te Sensor
Unit: C2d, C3e,
C4c, C6e, C8 e,
C10b, C46a,
C95a, C106
1.50 (l) x 5.25
(w) x 3.0 (h)
null
—
AIRCRAFT SITUATION DISPLAYS
Manufacturerz
Model Display
Inputs Outputs
Units/Weight (lb.) Price
Remarks
TSO Display Size Size or Form Factor Power Required
Rogerson-Kratos
403 S. Raymond
Pasadena, CA 91109
(626) 449-3090
www.rogersonkratos.
com
5 ATI EFIS
AMLCD
at panel
analog
synchro
(XYZ, Sin/
Cos) variable
AC/DC
discretes &
digital ARINC
429, 419,
453, 735,
RS-232
analog syn-
chro (XYZ ,
Sin/Cos)
variable AC/
DC discretes
& digital
ARINC 429,
419, 453,
735, RS-232
1/7.75
$42,000*
28 VDC
44 W max
One, two or four programmable, self-
contained at-panel AMLCD EADI and
EHSIs. Radio altimeter functions such
as DH, expanded scale for landing he-
licopter operations, TCAS I and II, and
EGPWS display capability, in addition
to standard ADI, HSI, bearing pointers,
CDI, autopilot annunciation, ight
director cross bars or ‘V’ bars. Upgrade
packages available. *BCA estimate.
C3d, C4c, C5e,
C6d, C8d, C9c,
C3 4e, C35d,
C36e, C40c,
C41d, C52b,
C63c, C66c,
C67, C87, C92c,
C113, C117a,
C118, C119b,
C129a, C147,
C161a
5 ATI
or 6.4-in.
diagonal
5 ATI or
6.4 dia.
Sandel Avionics
2401 Dogwood Way
Vista, CA 92081
(877) 726-3357
(760) 727-4900
Fax: (760) 727-4899
www.sandel.com
SA4550 Pri-
mary Attitude
Display
rear projection
LCD w/LED
bac klighting
analog:
attitude
glideslope,
locaiizer,
ight director
comman d
inputs, radar
alti meter
mode an-
nunciators
N/A
1/3.4
$20,950*
28 VDC
40 W
Designed to upgrade legacy ADIs. Incor-
porates ight director command bars,
glideslope/ localizer devia tion scale,
fast/ slow indicator and mode annunci-
ations. Selectable sing le-cue/split-cue
display option. Sunlight readable LED
backlit display with 180- degree viewing
angle and over 10,000-hour MTBF.
*High -vibration version, $23,800. NVIS
compatible version, $27,050
C113, C3d,
C4c, C34e,
C36e, C52b
4 ATI 4 ATI
Universal Avionics
Systems Corp.
3260 E. Universal Way
Tucson, AZ 85756
(520) 295-2300
Fax: (520) 295-2395
www.uasc.com
EFI-550
AMLCD,;
optional NVG
com pat ibility
ARINC
6 - 429/419
1 - 561/568
2 - 453/708A
2 - RS 422
4 - analog
30 - dis-
cretes*
ARINC
429/49 (2)
RS 422 (2)
6 - analog
8 - discretes
1/7.1
$14,995
28 VDC
*Depending on conguration.
C3d, C4e, C5e,
C6d, C52b,
C105, C113
3.35 x 4.36
5.5-in. dia.
(EFI S-85 std.)
4.8 x 5.18 x 7.90
(from front mo unt
surface)
EFI-640 AMLCD
ARINC
6 - 429/419
1 - 561/568
2 - 453/708A
2 - RS 422
4 - analog
30 - dis-
cretes*
ARINC
429/49 (2)
RS 422 (2)
6 - analog
8 - discretes
1/7.8
$36,000*
28 VDC
Horizontal viewing angles of +/-60°.;
elec troni cally adjusted vertical viewin g
angle; sunlight readability with greater
than 10,000/1 dimming range.
*Depending on configuration.
C3d, C4c, C5e,
C6d, C52b,
C105, C113
3.86 x 5.14
6.4-in. dia.
5 x 6 ATI
5.18 x 6.18 x 7.9
(from front mo unt
surface)
EFI-890R
C2d, C3d, C4c,
C52, C6d, C8d,
C10b, C34e,
C35d, C36c,
C40c,C41d,
C52,b, C63c,
C66c, C87,
C92c, C95,
C105, C113,
C115b, C118,
C119a, C129a,
C151a
active matrix
color LCD
6.3 c 63
(8.0-om. dia.)
Analog:
6 - ARINC
429
5 - CSDB
2 - ARINC708
3 -Manches-
ter bus ports
2 VGA or
1-RDR-1E/F
& 1 -VGS,
2 - RS-170
or 2 - NTSC
com p. or
18:1
1 - RS-232
(maint.)
Dig ital:
28 GND/OPN
discretes
14 - 28 VDC/
opn
4- ARINC 407
with 2 ref.
inputs
15- analog
DC
Analog: 2
ARINC 429
2 - CSDB
1 - Manches-
ter bus port
Dig ital:
5 - GND/OPN
discretes
3 - 28 VDC/
OPN dis-
cretes
6 - analog
resolvers
2 - DC dif-
ferential
2 - DC single
end ed
1/ 12.0
Bezel:
7.84 h x 7.42 w
depth:
9.79
(back of bezel to
read of connector)
$60,000*
28 VDC
Horizontal viewing angle
+60°/-60°, vertical viewing angle
+45°/-10°; resolution: 780 x 780 pixels;
124.5 color groups per inch (CGPI);
sunlight readability with greater than
10,000/1 dimming range.
*Depending on configuration.
Avionics Charts_0513_working_Zinio_Only.indd 24 4/22/13 10:18 AM
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