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Transcript of VHF Panel-Mount transcei Vers - Aviation Weekawin.aviationweek.com/portals/awin/pdfs/BCA... · VHF...
BCA • ISSUE: May 2009 PAGE: 163 / Version: #1
Business & Commercial Aviation | May 2009 163www.AviationWeek.com/bca
VHF Panel-Mount transceiVers
ManufacturerModel Channels Power Output
(peak W) Units/Weight (lb)Price Remarks
TSO Channel Display Power Required Size (in.)
Garmin international1200 E. 151st St.Olathe, KS 66062(800) 800-1020(913) 397-8200Fax: (913) 397-8282www.garmin.com
SL40 760 10 1/2.0 $1,895 Built-in two-place VOX inter-com and standby frequency monitoring functions.
C37d transmitC38d receive
C128d stuck mic
LED 10-40 VDC 6.25 x 1.3 x 10.5 Auto-leveling; auto-squelch; stuck-mic protection; remote-mic keying and chan-nel call-up.
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Bendix/KingKY 97A
760 7 nominal 1/2.9 $1,809 Same as KY 196A but 14 VDC power input.
C37cC38c
LCD; nvm 14 VDC 6.25 x 1.3 x 10.5
Bendix/King KY 197A
760 11 nominal 1/3.2 $4,773 Same as KY 196A but 2280 channels and 8.33 kHz channel spacing.
C37cC38c
gas discharge; nvm
14 VDC 6.3 x 1.35 x 10.8
Bendix/King KY 196B
2280 18 nominal 1/3.2 $6,316 Includes ACARS, display and VDL-mode 2 internal radio.
C37cC38c
gas discharge; nvm
28 VDC 6.3 x 1.35 x 10.8
VHF reMote-Mount transceiVers
ManufacturerModel Frequency
Display Xmit Power (W)Units/Weight (lb) Price
RemarksTSO Frequency Storage Size or Form Factor Power Required
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Bendix/King KTR 908
gas discharge 20 2/4.3 $19,024 Includes KFS 598A control with digital display of ac-tive/standby frequencies, flip-flop 118.0-151.975 MHz.
C37cC38c
2 (9 channels);118.0 - 151.975
MHz opt.
1.8 x 5.0 x 11.8 28 VDC
RCZ 833K color CRT or LCD 20 1/11.0 $64,527 Price shown is the com portion in the Primus II integrated radio system. Includes Mode S transpon-der.
C37c/C38cC112
Class 3A
2 to 12 depending on function
14.0 x 3.4 x 8.9 28 VDC
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
VHF-22A CTL-22G gas discharge 2x5
serial digital tuning
20 2/5.8 $18,944 Built-in diagnostics; VHF-22B, 118.0-151.975 MHz. Operates in 25 kHz tuning movements; includes CTL-22.C37c
C38c 8 frequencies; nvm 3/8 ATR-SL 28 VDC
VHF-422A CTL-22G gas discharge
20 2/5.8 $18,936 Built-in dignostics.
C37cC38c
8 frequencies; nvm 3/8 ATR-SL 28 VDC
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 164 / Version: #1
164 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
VHF reMote-Mount transceiVers
ManufacturerModel Frequency
Display Xmit Power (W)Units/Weight (lb) Price
RemarksTSO Frequency Storage Size or Form Factor Power Required
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
VHF-22C CTL-22D gas discharge;
2 x 5 serial tuning
20 2/5.8 $21,864 Built-in diagnostics; VHF-22D 118.0-151.975 MHz, $24,036. VHF-22D. 8.33 kHz/25 kHz tuning; includes CTL-22C.C37c, C38c 8 frequencies; nvm 3/8 ATR-SL 28 VDC
VHF-422C CTL-22D gas discharge
20 2/5.8 $23,696 Built-in diagnostics; com-patible only with CSDB or ARINC 429 controls; VHF-422D, 118.0-151.975 MHz, $21,756. 8.33/25 kHz tuning; includes CTL-22C.
C37cC38c
8 frequencies; nvm 3/8 ATR-SL 28 VDC
VHF-4000 CTL-22 gas discharge
20 2/4.7 see remarks Built-in diagnostics; com-patible only with CSDB or ARINC 429 controls. Options: 001 baseline: includes CTL-22.101 adds 8.33: includes CTL-22C. 201 adds Mode A/2 data; includes CTL-22.301 adds 8.33 and Mode A/2 data: includes CTL-22C.Prices range from $13,976 to $21,892.
C37dC38d
8 frequencies; nvm 2.5 MCU 28 VDC
VHF-4000E CTL-22Cgas discharge
20 2/4.7 $21,892-$26,264
Built-in diagnostics; compatible only with CSDB or ARINC 429 controls. Options: 101 adds 118.0-151.975 + 8.33; includes CTL-22C. 301 adds Mode A/2 data; inlcudes CTL-22C.
C37dC38d
8 frequencies; nvm 2.5 MCU 28 VDC
VHF-422D Transceiver
gas discharge 20 2/5.8 $30,168
C37cC38c
8.33/25 kHz 3/8 ATR-SL 28 VDC
VHF-4000 Transceiver
gas discharge 20 24.7 $68,620
8.33/25 kHz 2/5 MCU
Wulfsberg Electronics 6400 Wilkinson Dr.Prescott, AZ 86301 (928) 708-1550(928) 541-7627www.wulfsberg.com
CVC-152 color LCD N/A 1/0.75 $4,347* Gray or black panel.*BCA estimate.
control display 2.50 x 3.15 x 4.29
5 VDC, 5 VAC or 28 VDC
CCN-955 see remarks N/A 1/0.75 $7,643* Optional multi-function display; color LCD displays nav and com data. *BCA estimate.
2.50 x 3.15 x 4.29 5 VDC, 5 VAC, 28 VDC
CVC-151 FliteLine
118-136 MHz118-11.975 MHz
20 1/3.3 $14,040* ARINC 429 bus interface; 8.33 or 25 kHz spacing; FM immunity; auto-tune capability. FMS and radio management interface capability VDL Mode 2 & 3 provisions; color LCD nav and com data. *BCA estimate.
C169 color LCD 4.10 x 2.40 x 13.33
18 - 33 VDC
BCA • ISSUE: May 2009 PAGE: 165 / Version: #1
Business & Commercial Aviation | May 2009 165www.AviationWeek.com/bca
HF transceiVersManufacturer
Model Frequency Range Xmit Power (W)
Units/Weight (lb) PriceRemarks
TSO Channels Size or Form Factor Power Required
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
HF-1050 2-29.999 200 PEP (SSB)
4/29.9 $62,365 Delivers 200 W PEP transmitter power and four squelch options. “Once tuned, always tuned” coupler capability provides <20 millisecond response. PS-440 controller provides 99 user-programmable channels, clarifier func-tional and coupler tune status.
C31dC32d
280,000 KRX 1053 Receiver/Exciter: 5.56 lbs; 10.8
x 3.1 x 5.0
KPA 1052 Power Ampli-fier: 6.67 lbs;
12.7 x 7.2 x 1.8
KAC antenna coupler: 9.87 lbs;
13.0 x 4.7 x 9.87
28 VDC
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
HF 9000 System
2 - 29.9999SSB/AMAM data
selectable power output 10.50,
175 PEP
3/27.5 $99,980* Fiberoptic interface; rapid-tune antenna coupler (40 millisecond computer training); BITE. Includes HF receiver/transmitter antenna coupler and radio-tuning unit.*Special order price and delivery
C31dC32d
280,000;99 operator
programmable; 176 ITU
r/t programmed
controller:2.625 x 5.75 x 5.85
transceiver:7.625 x 5.55 x 12.60
antenna coupler:7.6 x 3.8 x 13.0
28 VDC
Horizontal situation indicators/coMPass systeMsManufacturer
Model GyroAutopilot Outputs
Units/Weight (lb) PriceRemarks
TSO Slave Rate Display Case Power Required
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
KI 825 Color EHSI/MFD
remote extensiveoutputs;
GPS selected discretes, EHSI-ready discretes
1/3.0 $19,224 Integrated EHSI, AMLCD; arc mode; 360 mode; course map; interfaces with numerous navigation systems and WX500 Stormscope. Priced for a new installation and a KCM 100.
C113, C6d, C34e, C36e, C40C, C11a
— 3 ATI 14 - 20 VDC
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
MCS-65 (compass system)
remote analog including autopilot outputs; CSDB
3/6.7 $15,608 Digital interface with EFIS-84 CSDB.
C6c 2.7°/min.;7°/sec.
ATI 28 VDC
Sandel Avionics2401 Dogwood WayVista, CA 92081(877) 726-3357(760) 727-4900Fax: (760) 727-4899www.sandel.com
SN3500 Primary
Navigation Display
remote analog 1/2.9 $10,990 Sunlight readable LED backlit display with 180-degree viewing angle and over 10,000-hour MTBF. Combines HSI, RMI, color moving map and other features. Accepts synchro, stepper motor and ARINC 429 gyro inputs. De-signed to work with a wide variety of digital and analog NAV, GPS/WAAS, DME, ADF and marker beacon receivers. Compatible with the WX-500 Stormscope. Op-tional interfaces for traffic, $714; WSI datalink weather, $714; high-vibration version, $13,800. NVIS compatible version, $17,050.
C113, C6d, C34e, C36e, C40e, C41D,
C118, C119B
N/A 3 ATI 11-33 VDC; 33 W
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 166 / Version: #1
166 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
autoMatic direction Finders
ManufacturerModel Frequencies
Nav Outputs
Units/Weight (lb) PriceRemarksFrequency Storage
TSO Size or Form Factor Power RequiredDisplay
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Bendix/KingKR 87
200-1799 kHz analog 1/6.7P/M
$3,861 Times flight and approaches; slaved indicator and RMIs available as options.nvm
C41c 6.25 x 1.3 x 11.23
11-33 VDCgas discharge
RNZ-850 100-1799.5 kHz;2181-2183 kHz
RS-422 synchro
XYZDC
sin/cos
2/13.6 $49,236 Nav radio for Primus II radio sys-tem. Price includes VOR/ILS and DME; complete built-in diagnostics including the RF.
1 freq; nvmC34d, C35d, C36d, C40b, C41d, C66b
14.0 x 3.4 x 8.9 28 VDCCRT or LCD
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
ADF-60A CTL-62190-1750 kHz(4-kHz steps)
RMI 2/6.0 $18,932* Remote-mount; dual antenna optional. Digital tuning. Includes ANT-60A, CAD-62. *Dual system, $38,088.6 frequencies; nvm
C41c 3⁄8 ATR-SL 28 VDCgas discharge, 2 frequencies
ADF-462 CTL62190-1799 kHz and 2182 kHz
emergency freq.
RMI 3/8.0 $18,936* Built-in diagnostics; compatible only with CSDB or ARINC 429 controls; digital signal processing; dual antenna optional.Includes ANT-462A.*Dual system, $38,056 includes two receivers, two controls, one antenna.
6 frequencies; nvm
C41d 3⁄8 ATR-SL 28 VDCgas discharge
ADF-4000 190-1799 kHz 2182 kHz
emergency freq.
CSDBARINC 429
3/6.4 $18,272* Built-in diagnostics; compatible only with CSDB or ARINC 429 controls; digital signal processing; dual antenna optional. Includes ANT-462A. *Dual system, $36,728.
6 frequencies; nvmC41d 2 MCU 28 VDCgas discharge
Horizontal situation indicators/coMPass systeMsManufacturer
Model Gyro Autopilot Outputs
Units/Weight (lb) PriceRemarks
TSO Slave Rate Display Case Power Required
Sandel Avionics2401 Dogwood WayVista, CA 92081(877) 726-3357(760) 727-4900Fax: (760) 727-4899www.sandel.com
SN4500 Primary Navigation Display remote
analog
1/2.9 $20,950Sunlight readable LED backlit display with 180-degree viewing angle and over 10,000-hour MTBF. Combines HSI, RMI, color moving map and other features. Accepts synchro, stepper motor and ARINC 429 gyro inputs. Designed to work with a wide variety of digital and analog NAV, GPS/WAAS, DME, ADF and marker beacon receivers. Compatible with the WX-500 Stormscope. TACAN interface avail-able. Optional interfaces for traffic, $714; WSI datalink weather, $714; high-vibration version, $23,800. NVIS compatible version, $27,050.
C113, C6d, C34e, C36e, C40e,
C41D,C118, C119B
N/A 4 ATI 22-33 VDC; 40 W
Panel-Mount naV receiVers
ManufacturerModel Channel Display Nav Outputs Units/Weight (lb) Price
RemarksTSO Channel Storage GS/MB Size or Form Factor Power Required
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Bendix/KingKN 53 gas discharge CDI 1/3.0
$5,495, Silver Crown Plus
$5,352, Silver Crown
Displays both active and preset frequency.
C34c, C36c, C40a
2 nav;nvm GS only 6.31 x 1.3 x
9.75 11-33 VDC
KLN 94Color GPS Receiver
colorpenetration phosphor
GPS 1/3.6 $4,804Direct replacement for KLN 89B. Database includes air-ports, VORs, NDBs, intersec-tions and special-use airspace. Quick-tune feature automati-cally loads frequencies into a KX 155A nav/comm. Features roll steering.
C-129A installed data-base none 2.0 x 6.31 x
10.72 11-33 VDC
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 168 / Version: #1
168 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
reMote-Mount naV receiVersManufacturer
Model Channel DisplayNav Outputs
Units/Weight (lb) PriceRemarks
TSO Channel Size or Form Factor Power Required
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
RNZ-850 color CRTOBI; OBS
synchro XYZ RS-22
2/13.6 $49,236 Price shown is for the Primus II radio system. Price includes a VOR/ILS/DME; complete built-in diagnostics including RF; Synchro XYZ mod filter included in unit.
C34d, C35d, C36d, C40b, C41d, C66b
1 to 12depending on function; nvm
14 x 3.4 x 8.9 28 VDC
Bendix/King KNR 634A gas discharge
ARINC 429CDI, HSI, RMI
2/6.5 $32,936Synchro-interface KNI 582 RMI optional. Digital display of active/standby frequencies.C40a, C36c,
C34c, C35d2 nav;nvm 3.0 x 5.0 x 10.0 28 VDC
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
VIR-4000 CTL-32gas discharge
CSDBARINC 429 2/3.9 see remarks Special order item and pricing.
Combines ADF and VOR/ILS/MKR receivers in a single package. Internal diagnostics capability.C34e, C36e,
C40c, C35d6 frequencies;
nvm N/A 2.5 MCU 28 VDC
NAV-4500 CTL-32gas discharge
CSDBARINC 429 2/4.1 $23,560 Built-in diagnostics; compatible
only with CSDB or ARINC 429 con-trols; digital signal processing; includes CTL-32 ($4,904); meets Eurocontrol FM immunity stan-dards only. RTU 4200, $23,880.
C34e, C36e, C40c, C35d
6 frequencies;nvm N/A 2.5 MCU 28 VDC
VIR 32 CTL-32gas discharge
SIN/COSserial digital;
RMIcompatible
2/5.7 $28,400*Replaces VIR-30A directly; includes serial digital control; digital signal processing; built-in diagnostics; rotor modulation filter optional (strap). Includes CTL-32. Meets FM immunity re-quirements. *Other configurations will determine final price.
C34c, C35d, C36d, C40b
6 frequencies;nvm
3⁄8 ATR-SL28 VDC, 26 VAC, 400 Hz
VIR 432 CTL-32gas discharge
serial digital
2/5.7 $31,896*Built-in diagnostics; compatible only with CSDB or ARINC 429 controls; includes CSDB control, digital signal processing. Includes CTL-32. Meets Eurocontrol FM immunity requirements. *Other configurations will determine final price.
3⁄8 ATR-SL28 VDC, 26 VAC, 400 Hz
C34d, C35d, C36d
6 frequencies; nvm
NAV-4000 CTL-32gas discharge
CSDBARINC 429 2/4.7 $32,532*
Built-in ADF; built-in diagnostics; compatible only with CSDB or ARINC 429 controls; digital signal processing; meets Eurocontrol FM immunity standards.*Configuration will determine price.
C34e, C36e, C40c, C35d,
C41d
6 frequencies;nvm N/A 2.5 MCU 28 VDC
Wulfsberg Electronics 6400 Wilkinson Dr.Prescott, AZ 86301 (928) 708-1550(928) 541-7627www.wulfsberg.com
CVN-251 108.0-117.95 MHz
ARINC 429SIN/COS
1/3.314.0 x 2.4 x 13.33 $20,631*
ARINC 429 bus interface; 160 VOR channels; 40 LOC channels; includes glideslope/marker beacon receivers. FM immunity standard. *BCA estimate.1/0.75
2.5 x 3.15 x 4.29 18-33 VDCC40c, C36e, C34c, C35d LCD
CVC-152Control Display
108.0-117.95 MHz
ARINC 429SIN/COS
1/3.314.0 x 2.4 x 13.33 $4,347*
Combines COM and NAV tuning; gray or black panel.*BCA estimate.
LCD 1/0.752.5 x 3.15 x 4.29
5 VDC, 5 VAC or 28 VDC
CCN-955 108.0-117.95 MHz
ARINC 429SIN/COS
1/3.314.0 x 2.4 x 13.33 $7,643*
Combines COM and NAV tuning. *BCA estimate.
LCD 1/0.752.5 x 3.15 x 4.29
5 VDC, 5 VAC or 28 VDC
BCA • ISSUE: May 2009 PAGE: 169 / Version: #1
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distance MeasurinG equiPMent
ManufacturerModel
Channel Display
Nav Outputs Units/Weight (lb) PriceRemarks
TSO Power Outputs (peak W)
Size or Form Factor Power Required
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Bendix/KingKN62A gas
discharge
serial data 1/2.6P/M $7,329 Includes antenna and installation kit;
accepts remote channeling. Distance accuracy: ±0.1 nm nominal to 99 nm, ±1.0 nm, 100 to 389 nm.100 6.3 x 1.3 x 12.3 11-33 VDC
Bendix/KingKN63 gas
discharge
serial data 2/3.6 $11,470 Includes KDI 572 indicator, optional slaved indicator. Distance accuracy: ±0.1 nm nominal to 99 nm, ±1.0 nm, 100 to 389 nm. C66a 100 6.5 x 1.1 x 11.55 11-33 VDC
RNZ-850
LCD
ARINC 568RS-422 2/13.6 $22,936 Price is the DME portion in the Primus
II Integrated Radio System. Includes VOR/ILS; ADF; 4-channel scanning DME; complete built-in diagnostics including the RF; remote mount.
C34d, C35d,C36d, C40b,C41d, C66b
40mV/nm300 N/A 28 VDC
Bendix/KingKDM 706A
gas discharge,
slaved indicators
ARINC 429ARINC 568 2/6.3 $20,291 Includes KDI 572 indicator;
optional slaved indicator; kits/mounts not included.
C66b 250 3.0 x 5.25 x 12.8 28 VDC
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
DME-42 gas discharge,
serial digital 2 x 5 tuning
ARINC 568serial digital 2/6.2 $18,896
Includes two-digit-code diagnostics; directly replaces DME-40; tracks three channels simultaneously when used with CTL-32 and IND-42A (special order only) (CTL-32 controls nav receiver); digital signal processing; echo monitor. IND-42A indicator included. Displays 0-300 nm; 0-999 knots; 0-120 min.
C66b 300 1/2 ATR-SL 28 VDC
DME-442gas
discharge
ARINC 568serial digital
(CSDB)ARINC 429
2/6.2 $22,156
Tracks three channels simultaneously when linked to CTL-32, IND-42A; decodes and displays station ident; digital signal processing; echo monitor; built-in diagnostics; includes IND-42A (special order only).C66b 300 1/2 ATR-SL 28 VDC
DME-4000gas
discharge
CSDBARINC 429 2/4.4 $20,100 Tracks three channels simultane-
ously when linked to CTL-32, IND-42; decodes and displays station ident; digital signal processing; echo monitor; built-in diagnostics; includes IND-42.C66c 300 2.5 MCU 28 VDC
Wulfsberg Electronics 6400 Wilkinson Dr.Prescott, AZ 86301 (928) 708-1550(928) 541-7627www.wulfsberg.com
CDM-451 FliteLine
LCD
3 ARINC 4292 ARINC 5681 40-bit serial
1/3.6 $21,785*Three-channel scanning. ARINC 429 interface; nav frequency display in DME hold mode; six-wire analog continuous self-test. *BCA estimate.
C66B 325 3.87 x 3.27 x 13.33 18-33 VDC
Av i o n i c s
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lonG-ranGe naViGation sensors
Manufacturer
Model Inputs Units/Weight (lb) Price
RemarksSystem TypeOutputs Size or Form Factor Power RequiredTSO
CMC Electronics Esterline600 Dr. Frederick Phillips Blvd. Montreal, Quebeck, Canada 4HM2S9(514) 748-3184Fax: (514) 748-3100www.mcelectronics.ca
CMA-5024 in/ARINC 710 ILS & 709 DME (ARINC
743B)
1/7.0 N/A Provides SBAS-aided GPS; Position-Velocity-Time (PVT); autonomus Localizer Preci-sion with Vertical guidance (LPV) approaches with CMA-5025 GLS control panel or compatible FMS.
GPS Landing System Sensor Unit
(GLSSU) Out/PVT AARINC 429 (743A)
Out/LPV ARINC 429 (743B) ILS & DME
look-a-like
ARINC 743A 28 VDC
C145b Class Beta 3C146b/Delta 4
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Laseref V Micro IRS ARINC 429 2/9.9 $210,197 All digital; passive cooling; automatic mode control; align-in-motion when supplied with ARINC 743A GPS imputs.
Laser Gyro IRS
ARINC 429 6.6 x 6.4 x 6.3 28 VDCC4c, C5e, C6d
GR-550 ARINC 429 1/6.0 $31,380 Complies with ARINC 743A; integral satcom filter, 24 channels.GPS sensor
ARINC 429(ARINC 743A)
2.6 x 8.5 x 9.5 28 VDC115 VACC-129 B1/C1
Laseref IV ARINC 419/429 2/16.9 $293,353 All digital; 4 MCU ARINC 704.
Laser Gyro IRS
ARINC 429/ASCB 4.9 x 7.6 x 13.1 28 VDC or 115 VACC4c, C5e, C6d
Special MissionsLaseref V
ARINC 429 2/9.9 $251,069
N/AARINC 429 6.6 x 6.4 x 6.3 28 VDC
N/A
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
GPS-4000S ARINC 429(complies with ARINC 743A)
N/A $32,576
GPS receiver w SBAS (WAAS)
capability ARINC 429 2 MCU 28 VDC
C145A Class Beta-3
transPonders
ManufacturerModel Modes Units/Weight (lb) Price
RemarksTSO Power Output (W) Size or Form Factor Power Required
ACSS, an L-3 Communications and Thales Company19810 N. 7th Ave.Phoenix. AZ 85027(823) 445-7001www.L-3.com/acss
Mode S RCZ-852
TCAS/Mode S/Fit ID control
panel; RMU (Pri-mus II radios)
3.5 x 4.2 14.1/5.0 $59,952
Elementary and Enhanced Surveillance (ELS/EHS) and DO 260 compliant. Certified on many retional and business jets.
C112 CTL92A/T/E NA
Mode S ATDL XS-950
TCAS/Mode S/Fit ID control
panel; 1/11.5 $67,689
Elementary and Enhanced Surveillance (ELS/EHS) and DO 260 compliant. Certified on many air transport category aircraft.
C112 — 4 MCU N/A
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transPonders
ManufacturerModel Modes Units/Weight (lb) Price
RemarksTSO Power Output (W) Size or Form Factor Power Required
Garmin International1200 E. 151st St.Olathe, KS 66062(800) 800-1020(913) 397-8200Fax: (913) 397-8282www.garmin.com
GTX 330 A, C, S 1/3.0 $4,995 Solid-state Mode-S, keypad entry, remote ident, front-panel entry for flight ident, altitude monitor with vice alert, flight timers. TIS compatible in the United States.
C112 Class 2A 250 1.6 x 6.25 11-33 VDC
GTX 330D A, C, S 1/3.0 $9,995* Diversity Mode-S, solid-state keypad entry, remote ident, front panel entry for flight ident, altitude monitor with voice alert, flight timers. TIS compatible in the United States. *BCA estimate.
C112 Class 2A 250 1.6 x 6.25 x 9.75 11-33 VDC
GTX 32 A, C 1/2.2 $2,645 Remote mount, solid-state, remote ident capability, flight timers.
C74c Class 1A 200 1.71 x 6.30 x 8.78 11-33 VDC
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Bendix/KingKT 76A A, C 1/3.1 $1,848 Automatic reply-light dimmer; system
test; remote ident capability adapter available.
C47c; Class 1B 250 6.25 x 1.6 x 10.0 14 or 28 VDC
Bendix/KingKT 76C A, C 1/3.1 $2,405 Slide-in replacement for KT 76A. Program-
mable VFR code; remote ident capability; gas-discharge digital display; push-button code entry.C47c 250 6.25 x 1.63 x 10.73 11-33 VDC
Bendix/KingKT 71 A, C 1/3.9 $5,653 Gas discharge display;
encoding altimeter output.
C47c; Class 1A 250 6.25 x 1.63 x 10.0 11-33 VDC
Bendix/KingKT 73 A, C, S, TIS 1/3.6 $5,308 Mode S data link with TIS.
Meets European Elementary Surveillance mandate (non-diversity).
C112 200 6.25 x 1.63 x 10.82 10-32 VDC
Bendix/KingKT 70 A, C, S 1/3.9 $5,361 Mode S transponder; non-diversity sur-
veillance only; includes discrete address memory module; displays encoding altim-eter output; gas discharge display.C112; Class 1A 250 6.25 x 1.63 x 10.0 11-33 VDC
Bendix/KingMST 67A A, C, S 2/8.5 $34,343 Mode S diversity transponder
C37c/C38cC74c; Class 3A 250-625 14.0 x 3.0 x 8.9 115 VAC; 400 Hz
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
TDR-94D S 2/9.7 $335,068Mode S transponder; European Elemen-tary and Enhanced Surveillance compli-ant. Compatible with TCAS II Change 6.04 and Change 7.0 systems. DO-260A ADS-B trasmit compliant. Includes CTL-92E flight ID capable control panel.
C112; Class 3 250-625 4.9 x 3.3 x 12.5 28 VDC
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 172 / Version: #1
172 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
WeatHer radar
Manufacturer
ModelRanges Dish Size
& Beam Width
(in./deg.)
Scan Stablztn. Display Interface
Scope (dia./in.)
Units/ Weight Price
RemarksTSO Pulse Width Stabl. Sig.
Power Output
(Peak KW)Colors Indicator
Size RT. Size PowerCircuits Looks/Min. Ant. Tilt
Garmin International1200 E. 151st St.Olathe, KS 66062(800) 800-1020(913) 397-8200Fax: (913) 397-8282www.garmin.com
GWX 68Selectable 2.5, 5, 10, 20, 40, 80,
160 and 320 nm(MX 20;
GMX 200)10/9
12/7.8
20, 40, 60 or 90°
(G1000)±30° Garmin
HSDB and ARINC429/453
N/A
12 in./ 9.1
10 in./ 9.0
$21,995(12 in.)
$20,995(10 in.)
Vertical scan feature: looks horizontally or vertically on bearing line selected by pilot. WATCH feature identifies the shadowing effects of short range cell activity; Automatic Target Alert feature looks ahead for intense cell activity in 80-320 nm range.
C63c20 or 90°
(MX 20 and GMX 200)
30-220 mV/ degreeARINC
429 HSDB
7kW 4 6 in. &10 in. diag.
Width:10.0 in.Depth:6.3 in.
4/28 VDC,60 W
8-28 VAC400 Hz
Vertical scan, ext. STC, WX alert, atten. comp., variable gain - WX and map modes,
WATCH
1 & 4 micro-seconds ±15°
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Bendix/Kingart 2000 10, 20, 40,
80, 16010/1012/815
90° or100° 30° KMD 850
EFIS N/A 1/9.9 $31,199 Vertical profile feature: scans horizontally or vertically on track line selected by pilot. Alpha-numeric display of range, function and tilt angle.
C63c 4 20-220mv/det.
4 4 N/A 10.28 dia.
28 VDC;10, 26,
115 VAC, 400 Hz
Vertical profile, ext. STC, tgt., wx alert, atten., comp.,
variable gain-map mode
ARINC429 ±15°
Bendix/Kingrdr 2100
5, 10, 20, 40, 80,
160, 240, 320
12/810/10
90°, 100°, 120°
±30°pitch & roll KMD 850
EFIS N/A 1/9.9 $42,186 Vertical profile feature: scans horizontally or vertically on track line selected by pilot; Alpha-numeric display of range, function and tilt angle. KMD 850 MFD, $13,440.
C63c range dependent
20/220mv/deg.ARINC429
6.0 5 N/A 10.28 dia.
28 VDC;10, 26,
115 VAC, 400 Hz
Vertical profile; extended STC; wx attenuation com-pensation; variable gain in
map mode; wx alert; autotilt
15 ±15°
Primus 440
2.5, 5, 10, 25, 50,
100, 200 12/7.9
120° ±30° ARINC453/708checklist,data nav,
EFIS, MFD,LSZ-860
4 2/15.8 $47,321Single receiver/transmit-ter/antenna pedestal.
C63c 2
50 or200
mv/deg.ARINC 429
10 4 4.8 x 6.25 x 12.24
5.0 x 7.6 x 15.0 28 VDCREACT; preset &
variable gain 12 ±15°
Primus 660 2.5, 5, 10, 25, 50,
100, 200, 300 12/7.9
18/5.6
60° or 120° ±30° ARINC453/708checklist,data nav,
EFIS, MFD,LSZ-860
4 2/15.8 $62,418Single receiver/transmit-ter/antenna pedestal.
C83c 250 or 200mv/deg. orARINC 429
10 4 4.81 x 6.25 x 12.24
5.0 x 7.6 x 15.0 28 VDCREACT; GMAP target alert,
preset & variable gain 12/24 ±15°
Primus 880 2.5, 5, 10, 25, 50,
100, 200, 300 12/7.9
18/5.624/4
60° or 120° ±30° ARINC453/708checklist,data nav,
EFIS, MFD,LSZ-860
5 2/15.8 $101,956
Single receiver/transmit-ter/antenna pedestal.
C63c 250 or 200mv/deg. orARINC 429
10 5 4.8 x 6.25 x 12.24
5.0 x 7.6 x 15.0 28 VDC
Doppler turb. detec., compensated, tilt, REACT,
GMAP target alert, preset & variable gain
12/24 ±15°
Primus 700a1⁄2, 1, 2.5, 5, 10, 25, 50, 100, 200, 300
10/10,12/7.9,10 x 14/10 x 7.1,18/5.6,
24/4
60° or 120° ±30 ARINC429/708checklist, data nav,
EFIS,lightning sensor
LSZ-860
5 4/37 $154,442
Short-range and high resolution system for special search and surveillance missions, displayed menus. Minimum detect range at 450 ft. Allows full dual-mode operation for pilot and copilot. Price reflects typical system.
C63c 650 or 200mv/deg. orARINC 429
10 5 4.81 x 6.25 x 12.24
5.0 x 7.6 x 15.0
28 VDC;400 Hz
REACT; ground & sea clut-ter red.; turb. detect-preset
& variable gain12/24 ±15°
Primus 701a1⁄2, 1, 2.5, 5, 10, 25, 50, 100, 200, 300
10/10,12/7.9,10 x 14/10 x 7.1,18/5.6,
24/4
60° or 120° ±30°ARINC
429/709checklist, data nav,
EFIS,lightning sensor
5 4/39 $176,376
Short-range and high-resolution system for special search and surviellance missions; displayed menus and AC 90-80A specified clear zones. Allows full dual-mode operation for pilot and copilot. Price reflects typical system.
C63c, C102 650 or 200mv/deg. orARINC 429
10REACT; ground clutter re-duction; turbulence detect-
preset & variable gain12/24 ±15°
64.81 x6.25 x12.24
5.0 x 7.6 x 15.0
28 VDC;115 VAC,400 Hz
BCA • ISSUE: May 2009 PAGE: 173 / Version: #1
Business & Commercial Aviation | May 2009 173www.AviationWeek.com/bca
WeatHer radar
Manufacturer
ModelRanges Dish Size
& Beam Width
(in./deg.)
Scan Stablztn. Display Interface
Scope (dia./in.)
Units/ Weight Price
RemarksTSO Pulse Width Stabl. Sig.
Power Output
(Peak KW)Colors Indicator
Size RT. Size PowerCircuits Looks/Min. Ant. Tilt
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
WXr-8005, 10, 25, 50, 100, 200, 300
12/8
120° ±30° pitch & roll
EFIS-85,EFIS-86,
MFD 2000FlightMax
950
varies byindicator 2/20.4 $46,788
All solid-state Doppler pulse weather avoidance radar; one-piece design; six pluse widths — 1.7° to 28.8°. Separate func-tion switch for each pilot.
C63 seeremarks
digital 429 or 200
mv/deg.
5 4 varies byindicator
15.0 x11.5 28 VDCrange-adjusted contour;
ground clutter suppression 14 ±15°
WXr-8405, 10, 25, 50, 100, 200, 300
12/814/718/6
60° or 120° ±30°pitch & roll
EFIS-85,EFIS-86,
MFD-2000
FlightMax950
varies by indicator 2/20.4 $89,420*
All solid-state Doppler pulse wx avoidance radar. One-piece design. Designed as EFIS wx sensor. Six pulse widths, 1.7 to 28.8. Separate function selection for each pilot (mode, range, gain, tilt and target alert). *Special order pricing.
C63c see remarksdigital 429
or 200 mv/deg.
0.024 4 varies by indicator
15.0 dia. x 11.5
28 VDCrange-adjusted contour;ground clutter suppression 13 ±15°
tWr-8505, 10, 25, 50, 100, 200, 300
12/814/718/6
60° or 120° ±30°pitch & roll
EFIS-85,EFIS-86,
MFD-2000
FlightMax950
varies by indicator 2/20.4
special order
pricing
Solid-state Doppler turbulence detection, pulse wx avoidance radar; designed as EFIS wx sensor; six pulse widths, 1.7 to 28.8; separate function selection for pilot (mode, range, gain, tilt, turbulence and target alert).
C63c see remarksdigital 429
or 200 mv/deg.
0.024 4 varies by indicator
15.0 dia.
x 11.528 VDCrange-adjusted contour;
ground clutter suppression 13 ±15°
radar altiMetersManufacturer
Model Alt. RangeAccuracy Display Units/
Weight (lb)Price
RemarksTSO Pitch/Roll Limits Power Required
FreeFlight Systems3700 Interstate 35 S.Waco, TX 76706(254) 662-0000Fax: ( 254-662-9450www.freeflightsystems.com
RA-4000 and RA-4500
-20-2,000 ft.
0 to 100 ft. ±3 ft.100 to 500 ft. ±3%
500 to 2,000 ft. ±5%
RAD-40 Radar Altim-eter display compatible with the RA-4000 and RA-4500
2/2.27
N/ARA-4000 provides RS 485/422 and RS 232C outputs; RA-4500 provides ARINC 429, RS 485/422 and RS 232 outputs. Two-year warranty. Optional night vision goggle (NVG) compatible display and round faceplate adapter for display. Accepting orders now for RAD-40 indicator; deliveries in 2Q 2009.
C87 ±20°/±30° 28 VDC
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Bendix/KingKRA 405B -20-2,000 ft. 0-100 ft,
34 ft or 3%,whicheveris greater;
500-2,500 ft, ±5%
pointer dial 2/10.7
$25,058 Compatible with Honeywell Mark VI GPWS/EGPWS continuous DH set; tracking to 2,500 ft; expanded heli-copter version available; night-vision goggle version available. Optional built-in tone generator.
C87 ±20°/±25° 28 VDC
AA-300 0-2,500 ft. 0-100 ft, ±3 ft;100-500 ft, ±3%;500-2,000 ft, ±4%
pointerdial 2/6.5
$28,936 Price includes RT300 radio altimeter and RA-315 indicator.
C87 ±20°/±30° 28 VDC
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
ALT-1000 0-2,500 ft±2 ft or 2% Analog only
outputs* 2/6.8$17,988 *Requires separate converter for use
with ARIONC 429 systems.
C87 ±40°/±50° 28 VDC
ALT-4000 0-2,500 ft.
±2 ft or 2%
EFIS(analog version
available)
2/6.8
$30,728 Interfaces to EFIS high-intensity monitor for Cat II/III certification. Includes two ANT-52 antennas.
C87 ±40°/±50° 28 VDC
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 174 / Version: #1
174 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
tHunderstorM detection systeMsManufacturer
Model Search ArcInformation Display
Display Size PriceRemarks
TSO Max Range Units/Weight Power Required
Avidyne Corp.1944 East Sky Old Bedford Rd.Lincoln, MA 01733(781) 402-7400Faz: (781)[email protected]
TWX670 Tactical Weather
Detection Sensor
N/A
AMLCD. Seven RS232 outputs; com-
patible with Avi-dyne MHD300,
EX500, EX5000; also compatible for monochrome
strikes on many RS232-capable light-ning displays
3 ATI$11,995 (non-radar version,
$8,995)
Combines the data of all lightning activity occurring over a running three-minute period, regardless of the number of strikes. “TWXCell mode” hightlights the most intense regions of thunderstorm activity, presesnting a visually contoured color display with dynamic sectors. Eliminates radial spread associated with older technology systems.
C110, C113, C118
TSO-C147NVG compat-
ible
200 nm2/3.1 (sensor and antenna
only)
10-30 VDC, 0.4 A @ 28
VDC
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
LSZ-860 60°, 120°,360°
three unique symbols
represent three rates
of occurence for vertical
lightning in a specific area
displays on Honeywell
EFIS of various sizes
$26,557
Price shown is for typical system.
C110 100 nm 3/10.8 28 VDC
L-3 Avionics Systems5353 52nd St. S.E.Grand Rapids, MI 49588(616) 949-6600Fax: (616) 285-4224 www.L-3com.com
WX-500 360°
—
N/A $5,240*Remote-mount sensor interfaces with OEM MFDs or radar indicator when paired with RGC250 (sold separately). 360° and 120° surveil-lance in 25-200 nm ranges; head-ing stabilization; cell- or strike-mode data selection. *Processor only. Price BCA estimate.
C110a 200 nm 2/3.43 11-32 VDC
WX-950 360°
CRT
3 ATI $6,370*Series II Stormscope: self-contained processor/display unit; 360° and 120° views in 200, 100, 50 and 25 nm ranges; heading stabilization; cell- or strike-mode data selection. *Display/processor only. Price BCA estimate.
C110a 200 nm 2/3.74 11-33 VDC
WX-1000+AN/AMS-2 360°
CRT
3 ATI $13,420* Includes heading stabilization.*Processor only. Price BCA estimate.
C110A 200 nm 3/10.95 10-32 VDC
WX-1000E (429 EFIS) 360°
—
depends on EFIS system $13,460*
Provides output on EFIS display or radar indicator when paired with RGC35C (sold separately); includes three levels of activity, bearing and distance; optional displays for checklists. *Processor only. Price BCA estimate.
C110a 200 nm 1/6.67 10-32 VDC
WX-1000E 360°
—
N/A $10,650* Same as WX-1000+; accepts RS232 input from Loran-C and GPS receivers. *Processor only. Price BCA estimate.C110a 200 nm 2/10.95 10-32 VDC
WX-1000E(429 Navaid) 360°
—
3 ATI $13,460* Navaid option for use with ARINC 429-based nav systems.*Processor only. Price BCA estimate.
C110a 200 nm 2/10.95 10-32 VDC
BCA • ISSUE: May 2009 PAGE: 175 / Version: #1
Business & Commercial Aviation | May 2009 175www.AviationWeek.com/bca
Basic autoPilots
ManufacturerModel Sensor Type Attitude Modes
Nav ModesUnits/Weight
(lb)
PriceRemarksRoll
TSO Servo Type Power RequiredPitch
S-TECOne S-TEC WayMunicipal AirportMineral Wells, TX 76067(800) 872-7832(940) 325-9406Fax: (940) 325-3904www.s-tec.com
S-TEC System ThirtyALT
accelerometer none none 3/4.0 $6,240
C9c DC electric altitude hold 14 or 28 VDC
S-TEC System 40
1 rate gyro command turn VOR/LOC/BC, GPS tracking
3/9, 0 $7,480 Can be upgraded to System 50 or 60-2.
C9c DC electric none 14 or 28 VDC
S-TEC System Twenty
enclosed in rate gyro
command turn VOR/LOC, GPS tracking
2/7.0 $7,320 Can be upgraded to System 30.
C9c DC electric none 14 or 28 VDC
S-TEC System 60-1
1 rate gyro hdg. select VOR/LOC/BC, GPS/Loran capture and
tracking
4/12.0 $9,060 Includes interfaces with all popular HSIs. Variable bank angle with airspeed; automatic three-level radio gain; can upgrade to 60-2.C9c DC electric none 14 or 28 VDC
S-TEC System 60 PSS
no external sensors
none GS capture and track
4/11.0 $9,400 Complements existing single roll-axis autopilot; auto/manual, electric trim optional, $2,195; may be upgraded to 60-2; altitude selector/alerter optional, $3,670.
C9c DC electric vertical speed hold; altitude hold; GS cap-ture and track
14 or 28 VDC
S-TEC System 50
1 rate gyro command turn/hdg. select
optional
VOR/LOC/BC, GPS, Loran
tracking
5/14.0 $11,980 Two-axis, roll and pitch autopilot; trim condition indi-cator std. Manual electric trim optional, $2,630. Can be upgraded to 60-2.
C9c DC electric altitude hold 14 or 28 VDC
S-TEC System Thirty
enclosed in rate gyro plus pitch computer
command turn VOR/LOC/GPS/Loran tracking
5/13.0 $11,660 DG option, $2,495
C9c DC electric altitude hold 14 or 28 VDC
S-TEC System 60-2
1 turn coord., 1 dir. gyro
hdg. select VOR/LOC/BC, Loran track and approach; GS capture and
tracking
7/21.0 $16,040 Interfaces with all popular HSIs. Automatic/manual electric trim optional, $3,520; altitude/vertical speed selector/alerter optional, $3,670; can be upgraded to flight director.
C9c 1 press. transducer
vertical speed and altitude
hold
14 or 28 VDC
S-TEC System FiftyFiveX
1 turn coord. hdg. select VOR/LOC/BC, GPS/Loran
tracking and GS capture
5/17.0 $19,880 Interfaces with all popular HSIs. Automatic/manual electric trim optional, $3,520. Altitude/vertical speed selector/alerter optional, $3,670; can be upgraded to flight director.
C9c 1 press. transducer
digital vertical speed, altitude
hold
14 or 28 VDC
S-TEC System 65
1 turn coord., 1 dir. gyro
hdg. select VOR/LOC/BC, GPS/Loran cap-ture and track-ing; GS capture
and tracking
9/24.0 $36,360
C9c 1 press. transducer
manual and auto. modes
14 or 28 VDC
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 176 / Version: #1
176 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
inteGrated FliGHt control systeMs
Manufacturer ModelAir Data Autopilot
Power
Weight Price
RemarksAP Only AP OnlyAttitude Sensors Flight Director IFCS IFCS
Garmin International1200 E. 151st St.Olathe, KS 66062(800) 800-1020(913) 397-8200Fax: (913) 397-8282www.garmin.com
GFC 700
GDC 74 (B) DADC combined
28 VDC
varies by installation
varies by installation
Digital, dual-channel fail-passive system for Cessna Mustang, Caravan, C-172, -182, -206, -350 and -400; Cirrus SR20 and SR22; Diamond DA40; DA42; Em-braer Phenom 100 and 300; HBC G36 and G58; Mooney M20R and M20S; Socata TBM 850 and HondaJet.
GRS 77 AHRS
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Primus 1000
micro DADC digital AHRS
or IRS IC-6000
28 VDC
varies by installation
varies by version
Digital fail-passive system. CAT II; ARINC 429 interfaces, two-, three-, four- or five-tube, 8 x 7 in. EFIS. Bombardier Learjet 40, 45 and 45XR; Embraer ERJ-135, 140 and 145; Cessna Bravo, Encore, Excel and Ultra.
combined 13.0 varies by version
Primus 1000 CDS
micro DADC IC-61528
VDC
varies by installation
varies by installation
Digital fail-passive system. CAT II; ARINC 429 interfaces; two- to five-tube 10 x 8 in. LCD EFIS. Cessna Citation XLS.Digital AHARS combined varies by
installationvaries by
installation
Primus 2000
micro DADC digital AHRS
or IRSIC-800
28 VDC
varies by installation
varies by version
Digital, dual-channel fail-passive system. CAT II w/optional auto-throttle, dual-sensor monitoring; five- or six-tube 8 x 7 in. CRT EFIS. Global Express and Global 5000; Cessna Citation X; Das-sault Falcon 900EX/C.
combined 15.0 varies by version
Primus Epic CDS
micro DADC digital AHRS
or IRSFZ-800
28 VDC
varies by installation
varies by installation
Digital fail-passive system. CAT II, ARINC 429 interfaces. Two-, three-, four- or five-tube 10 x 8 in. EFIS. Sino Swearingen SJ30-2.
combined varies by installation
varies by installation
Primus Epic
air data module and micro IRS
integrated modular avionics
unit
28 VDC
varies by installation
varies by installation
Integrates all traditional avionics into modular avionics unit. Digital, dual-channel; fail operational system. CAT II capable w/optional auto-throttle and envelope protection. Includes two- to five-tube 10 x 8 in. LCD EFIS or four 13 in. Agusta/Bell AB139; Citation Sover-eign; Dassault Falcon 900EX, 2000EX and 7X; Embraer 170, 175, 190 and 195; Gulfstream G500 and G550; Raytheon Horizon.
varies by installation
varies by installation
Primus Epic Fly-by-Wire
SystemSee remarks
Integrates with Primus Epic System. Scalable architecture, performance and envelope protection. ARJ-21
Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
APS-65
AHC-3000 APS-65
28 VDC
varies by installation
varies by installation
Built-in diagnostics; digital Cat II certificated autopilot. Optional EFIS and AHRS. STC kit installer fabricated. Compatible with EFIS-84. *Typical configuration, $155,976.
remote vertical gyro or dual
AHRS
EFIS-84(two tube) 50.6 *
APS-85
ADS-86 APS-85 28 VDC, 115 VAC, 400 Hz
varies by installation
varies by installation
Available only as full, dual-channel, fail-passive, digital system; digital Cat II autopilot, 4- or 5-tube EFIS optional; ARINC 429 IRS interface available; includes yaw damper; extensive built-in diagnostics. STC kit installer fabricated. Compatible with EFIS-84. *Typical configuration, $290,388.
dual AHRSAHC-3000
EFIS-85(three tube)
varies by installation *
S-TECOne S-TEC WayMunicipal AirportMineral Wells, TX 76067(800) 872-7832Fax: (940) 325-3904www.s-tec.com
Magic 2100 DFCS
digitalADAHARS Magic EFIS
14 or 28
VDC
14.5 see remarks
Dual-side EFIS and 2100 DFCS auto-pilot, $146,700. Single-side EFIS and 2100 DFCS autopilot, $119,800.
N/A N/A
BCA • ISSUE: May 2009 PAGE: 177 / Version: #1
Business & Commercial Aviation | May 2009 177www.AviationWeek.com/bca
collision aVoidance systeMsManufacturer
ModelDisplay Interface Options
Processor SizePrice Remarks
TSO Weight (lb)
ACSS an L-3 Communications & Thales Company19810 N. 7th Ave.Phoenix, AZ 85023(623) 445-7000Fax: (623) 445-7001www.L-3com.com/acss
TAWS+
MFD, EFIS, Weather Radar Display
2 MCU - 7.5 $120,714*
$134,914(with GPS)
*Without GPS. alerts based on standar aircrafat climb capability lus Terrain Advisory Line and Avoid Terrain features.C151B Class A,
C129b2
TCAS 2000RT-950/951
MDFD, EFIS, VSI/TCAS display
4 MCU - 16.06 MCU - 16.8
$168,812
Standard equipment on many regional and business jets including Bombardier, Cessna, Dassault, Embraer, Gulfstream, Raytheon. (SFE selectable on all Airbus and Boeing aircraft.)
C119B
TCAS 3000SP
MFD, EFIS, Weather Radar Display
4 MCU - 7.56 MCU - 16.08
$190,240
TCAS 3000SP is based on ACSS’s TCAS 2000. The new system provided custom-ers the option of adding certified ADS-B “in” capability combined with industry leading Traffic Alert and Collision Advoi-cance system technology.
— —
T2CASMFD, EFIS,
weather radar display VSI/TCAS display
4 MCU - 14.76 MCU - 16.8
$259,128
Combined TCAS and TAWS in 4- or 6-MCU with optional GPS. STCs available on Cessna, Raytheon and Piaggio aircraft.
C119B, C151a Class A, C129b2
Avidyne Corp.55 Old Bedford Rd.Lincoln, MA 01773(800) 284-3963Fax: (614) 885-8307www.avidyne.com
TAS 600
Avidyne EX500, EX5000 and MHD 300
Garmin, Chelton, Honeywell, Sandel,Sagem, Universal,
Meggitt, Rogerson Kratos
3.1 x 7.25 x 11.77.2
top and bottom antennas
3.24 x 2.76 x 5.14 $9,990
Designed for single-engine piston aircraft; seven-nm range, 3,500-foot vertical separation, 18,500-foot ser-vice ceiling. Head-up audible position alerting (“traffic! one o’clock! high! two miles!”); active interrogating, 30-second decision and 1,200-knot closure rate. C-147 22.5 oz. (combined)
TAS 610
Avidyne EX500, EX5000 and MHD 300
Garmin, Chelton, Honeywell, Sandel, Sagem, Universal,
Meggitt, Rogerson Kratos
3.1 x 7.25 x 11.77.2
top and bottom antennas
3.24 x 2.76 x 5.14 $14,990
Designed for mid-performance aircraft and helicopters; 12-nm range; 3,500-foot vertical separation; 25,000-foot service ceiling. Head-up audible position alerting (“traffic! one o’clock! high! two miles!); active interrogating, 30-second decision and 1,200-knot closure rate.C-147 22.5 oz. (combined)
TAS 620
Avidyne EX500, EX5000 and MHD 300
Garmin, Chelton, Honeywell, Sandel,Sagem, Universal,
Meggitt, Rogerson Kratos
3.1 x 7.25 x 11.77.2
top and bottom antennas
3.24 x 2.76 x 5.14 $20,990
Designed for high-performance aircraft and rotorcraft; 21-nm mile range; 9,900-foot vertical separation; 55,000-foot service ceiling. Head-up audible position alerting (“traffic! one o’clock! high! two miles!); active interrogating, 30-second decision and 1,200-knot closure rate.C-147 22.5 oz. (combined)
Garmin International400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com
Collision Avoidance System G1000
G900XGNS 530 (W)GNS 500 (W)
N/A
$10,000
Options feature for Garmin G1000 and G900X Integrated Avionics Systems and 500 Series navigation systems. Visual and aural warnings are provided to warn crew of potential CFIT hazards.
Class BC151a N/A
L-3 Avionics Systems5353 52nd St. S.W.Grand Rapids, MI 49512(616) 949-6600Fax: (616) 285-4224www.L-3com.com
TCAS791ASystem (TCAS I)without display
EFIS, MDFD and IVSI
Also displays wx radar using RGC-350 Radar Graphics Computer
(sold separately)
N/A
$56,460*
Active Traffic Collision Avoidance System (TCAS-I) designed to display on compat-ible EFIS, MFD and IVSI displays. Contact factory for approved interfaces. Fixed wing, top- or bottom-mount antenna or helicopter bottom mount antenna only. In-tallation kit and options separate. Other conditions may apply. *BCA estimate.
C118 N/A
TCAS791ASystem (TCAS I)
with CD-605 display see remarksN/A
$65,870*
Includes TCAS791A System above plus CD-605 Dedicated Color Display: CD-605 3-ATI Display, $11,410 additional. Instal-lation kit, $230 additional. Other condi-tions may apply. *BCA estimate.C118 N/A
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 178 / Version: #1
178 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
collision aVoidance systeMsManufacturer
ModelDisplay Interface Options
Processor SizePrice Remarks
TSO Weight (lb)
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Bendix/KingKGP 560 KMD 550 MFD,
KMD 850 MFD and most MFDs
2.2 x 4.15 x 6.25
$11,356
EGPWS exceeds Class B requirements. Provides aural and visual warnings; Inter-nal GPS; worldwide database by region.
C151Class B 1.5
KGP 860KMD 550 MFD, KMD 850 MFD and most MFDs
2.2 x 4.15 x 6.25
$14,731
EGPWS exceeds Class B requirements. Provides aural and visual warnings; inter-nal GPS; worldwide database by region. EFIS displays additional warning modes.
C151Class B 1.5
Mark XXI KMD 550 MFD, KMD 850 MFD and most MFDs
4.5 x 7.0 x N/A
$15,374
Helicopter EGPWS.
C118Class B 1.5
Bendix/KingKTA 870
KMD 550 MFD, KMD 850 MFD and most MFDs
4.5 x 7.0 x 13.8$21,856
Traffic Advisory System (TAS) is an active system providing aural and visual adviso-ries. Single or dual directional antennas.
C147 8.75
KTA 970 dual-color, flat-panel LCD combined IVSI/TA
display, KMD 550, EFIS, KMD 850 or
weather radar
4.5 x 7.0 x 13.8
$28,540
TCAS I system.
C118 8.75
Bendix/KingKMH 880 KMD 550 MFD,
KMD 850 MFD and most MFDs
4.5 x 7.0 x 13.8
$34,679
Traffic Advisory System (TAS) and EGPWS in one box. Active traffic system providing aural and visual adviories. Single or dual directional antennas.C147, C151,
Class B 8.75
Bendix/KingKMH 980 KMD 550 MFD,
KMD 850 MFDand most MFDs
4.5 x 7.0 x 13.8
$42,116
TCAS I and GA-EGPWS.
C118, C151Class B 9.68
EGPWS MK VIEFIS (select), MFD and
radar indicators
6.2 x 3.0 x 12.1
$34,277
MK VI designed for 10- to 19-passen-ger turboprop operation, interface and display requirements.C151b Class A,
C92C 3.5
EGPWS MK VIIEFIS (select), MFD
and radar indicators
6.2 x 3.0 x 12.1
$50,429
MK VII designed for >30-passsenger light transport operations, small turbofan, business jets.C151b Class A,
C92C 3.5
EGPWS MK XXIIEFIS and MFDs
6.2 x 3.0 x 12.1$51,593
MK XXII is for helicopters with radar altim-eters. Low-altitude mode. Internal GPS.
C151b Class A 3.5
EGPWS MK VEFIS, MFD and radar
indicators
7.9 x 2.4 x 12.8 $91,840 (without internal GPS)*
MK V is standard equipment on turbofan aircraft with digital avionics. *$95.658 with internal GPSC151b Class A,
C92c, C117a 7.5
EGPWS MK VIIEFIS, MFD and radar indicators
7.9 x 2.4 x 12.8 $91,840 (without internal GPS)*
MK VII is for turbofan aircraft equipped with analog avionics.*$95,658 with internal GPSC151a Class A,
C92c, C117a 8.0
CAS 66A Systemdual-color, flat-panel
LCD combined IVSI/TA display, KTA 870, KMH 880, EFIS or
weather radar
1⁄2 ATR-S(4 MCU)
$106,197
TCAS I system. Includes processor, con-trol panel, directional antenna and IVSI/TA display. Does not include installation kits. Upgradable to TCAS II.C118 17.0
CAS 67A System dual-color, flat-panel LCD combined IVSI/TA/RA display (included in price shown). Also can
interface with KMD 550 MFD, KMD 850 MFD, EFIS or weather radar
1⁄2 ATR-S(4 MCU)
$190,000
TCAS II system includes one TTR-4000 TCAS II LRU, one TRE-920 directional antenna, one TVI-920 VSI (TA/RA) display and one CTL-92T TCAS control panel. Does not include: Mode S transponder(s), installation kits/trays or bottom omni-directional TCAS antena. Software upgradeable to Change 7.1.
C119 a/b
BCA • ISSUE: May 2009 PAGE: 179 / Version: #1
Business & Commercial Aviation | May 2009 179www.AviationWeek.com/bca
collision aVoidance systeMsManufacturer
ModelDisplay Interface Options
Processor SizePrice Remarks
TSO Weight (lb)
Rockwell Collins400 Collins Rd. N.E.Cedar Rapids, IA 52498(319) 295-1000Fax: (319) 295-2297www.rockwellcollins.com
TCAS 4000Collins EFIS, MFDTCAS compatible
VSI (RA)
Collins TVI-920(RA, TA)
4 MCU
$422,064(typical
installation)
TCAS II system. European ACAS compat-ible Mode S Level III. AC/DC in one part number includes control panel and two TRE antennas. Displays range/alt. separation from traffic. Max range 3 mi. Two surveillance volumes and MSL of traffic. Top/bottom antennas to optimize coverage. Upgrades to 8800 Gold.
C119(C119a when
issued)17.0
Sandel Avionics2401 Dogwood WayVista, CA 92081(877) 726-3357((760) 727-4900Fax: (760) 727-4899www.sandel.com
ST3400H HTAWSIntegrated rear projec-
tion LCD with LED backlighting
3 ATI panel-mount
$18,900
Designed for mid-performance aircraft Sunlight readable LED backlit display with 180° viewing angle and 10,000+ hour MBF. NVIS compatible version, $22,150
C113, C151b, C194 2.9
ST3400 TAWSIntegrated rear
projection LCD with LED backlighting
3 ATI panel-mount
$22.750
Sunlight readable LED backlit display with 180° viewing angle and 10,000+ hour MBF. Optional interface for traffice, $2,500. Class A version, $37,000.
C113, C151b 2.9
Universal AvionicsSystems Corp.3260 E. Universal WayTucson, AZ 85756(520) 295-2300(800) 321-5253Fax: (520) 295-2395www.uasc.com
TAWS ATAWS B
Universal AvionicsEFI-890R, MFD-640,
UNS FMS (5-in. display)
Honeywellnumerous weather
radar, MFD and EFIS displays
Rockwell Collinsnumerous weather
radar, MFD and EFIS displays
SmithsBAE ATP EFIS
additional display options available
2 MCU LRU
TAWS A$38,500
TAWS B$24,000
Worldwide terrain database with 480+MB data. High-resolution analog video views; 3-D perspective view; profile view; map view. Map view of ter-rain can be output using ARINC 708 or WXPF formats for interface with various existing weather radars.
C151b, C92c 9.6
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 180 / Version: #1
180 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
cocKPit Voice recorders (cVr)/FliGHt data recorders (Fdr)
Manufacturer
Type Recording Medium Size PriceRemarksModel
Duration Weight (lb) Power RequiredTSO
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
CVR solid-state, digital 9.5 x 5.88 x 5.75 $18,872 Non-ARINC size, with underwater loca-tor beacon; control panel and mounting tray not required. ARINC 557 and ARINC 757.
AR 30 CVR980-6023-001 30 min. 8.8 28 VDC
ED 56A, C123a
CVR solid-state, digital 1⁄2 ATR short $26,722 Solid-state CVR with underwater loca-tor beacon; ARINC 557 and ARINC 757.
SSCVR 9806020-011 30 min. 11.5 28 VDC
115 ACED 56A, C123
CVR solid-state, digital 9.5 x 5.88 x 5.75 $23,351 Non-ARINC size with underwater loca-tor beacon; control panel and mounting tray not required. ARINC 557 and ARINC 757.
AR 120 CVR980-6023-002 120 min. 8.8 28 VDC
ED 56A, C123a
CVR solid-state, digital 1⁄2 ATR short $33,373 Solid-state CVR with underwater loca-tor beacon. ARINC 557 and ARINC 757.
SSCVR980-6022-011
120 min. 11.5 28 VDC115 AC
ED 56A, C123
FDR solid-state, digital 9.5 x 5.88 x 5.75 $26,819, to $36,938
Non-ARINC FDR, ARINC 717, 429. Mounting tray not required.
AR FDR980-4710-00X 25 hrs. @ 64,
128, 256 wps8.8 28 VDC
ED 55, C124e
FDR solid-state, digital 1⁄2 ATR long or short
$26,819 to $36,938
Solid-state FDR; ARINC Form Factor; underwater locator beacon. ARINC 747, 573, 717. Fire test to ED 56a.SSFDR
980-4700-0XX 25 hrs. @ 64,128, 256 wps
11.5 (short)13.5 (long)
115 VAC28 VDC
ED 55, C124
CVR/FDR solid-state, digital 9.5 x 5.88 x 5.75 $37,326 Combination CVR/FDR; non-ARINC size. Mounting tray not required. Three or two crew channels; one area mic.AR Combi
980-6021-06X 30 min. voice;25 hr. data @ 64,
128, 256 wps
8.8 28 VDC
ED 55, C124a
CVR/FDR solid-state, digital 9.5 x 5.88 x 5.75 $41,064 Combination CVR/FDR; non-ARINC size. Mounting tray not required. Three or two crew channels; one area mic.AR Combi
980-6021-06X 60 min. voice;10 hr. data @ 64,
128, 256 wps25 hr. data
8.8 28 VDC
ED 55, C124a
DVDR/FDR solid-state, digital 1⁄2 ATR short $41,967 Combination CVR/FDR; ARINC Form Factor. Mounting tray required. Data download through front access PCMCIA.
AR Combi 980-6021-06X 120 min. voice;
25 hr. data @ 64,128, 256 wps
11.5 28 VDC
ED 56A, C123a
L-3 CommunicationsAviation Recorders6000 Fruitville Rd.Sarasota, FL 34232(941) 371-0811www.L-3ar.com
CVR FA2100 solid-state flash memory
1⁄2 ATR short $16,208*$17,972**
ARINC 757, EUROCAE ED-112, four-channel audio.*BCA estimate.2100-1010-00
30 min./120 min.**
9.9 28 VDC or 115 VACC123b
CVR FA2100 solid-state flash memory
1⁄2 ATR short $18,227* ARINC 757, EUROCAE ED-112, four-channel audio. *BCA estimate.
2100-1020-00120 min. 9.9 28 VDC or 115
VACC123b
BCA • ISSUE: May 2009 PAGE: 181 / Version: #1
Business & Commercial Aviation | May 2009 181www.AviationWeek.com/bca
cocKPit Voice recorders (cVr)/FliGHt data recorders (Fdr)
Manufacturer
Type Recording Medium Size PriceRemarksModel
Duration Weight (lb) Power RequiredTSO
L-3 CommunicationsAviation Recorders6000 Fruitville Rd.Sarasota, FL 34232(941) 371-0811www.L-3ar.com
CVR FA2100 solid-state flash memory
1⁄2 ATR short $18,227* ARINC 757, EUROCAE ED-112, four-channel audio. General aviation.*BCA estimate.2100-1020-50
120 min. 9.9 28 VDC or 115 VACC123b
FDR FA2100 solid-state flash memory
1⁄2 ATR short $18,299* ARINC 717, EUROCAE ED-112, 256 wps data rate, short chassis.*BCA estimate.2100-2043-00
25 hr. 9.9 28 VDC or 115 VACC124b
FDR FA2100 solid-state flash memory
1⁄2 ATR short $18,289* ARINC 717, EUROCAE ED-112, 1024 wps data rate, standard chassis.*BCA estimate.2100-4043-00
25 hr. 10.6 28 VDC or 115 VAC—
Combi FA2100 solid-state flash memory
1⁄2 ATR short $19,930* ARINC 717/757, EUROCAE ED-112, 4 channel HQ audio, 256 wps data rate.*BCA estimate.2100-3083-00
120 min./25 hr. 10.6 28 VDC or 115 VACC123a/C124a
Combi FA2100 solid-state flash memory
1⁄2 ATR short $20,248* ARINC 717/757, EUROCAE ED-112, 4 channel HQ audio, 256 wps data rate. General aviation.*BCA estimate.
2100-3083-50
120 min./25 hr. 10.6 28 VDC or 115 VACC123b/C124a
UQAR200-0400 1 Gb flash memory card
1.8 x 2.2 x 1.7 $4,900* ARINC 573/717/747, fixed-media (removable flash card also available); USB download.*BCA estimate.625 hr. to
2,500 hr.0.3 28 VDC or 115
VACN/A
FDR FA2100 solid-state flash memory
1⁄2 ATR short $21,558* ARINC 717, EUROCAE ED-112, 1024 wps data rate, standard chassis.*BCA estimate.
2100-2045-0025 hr. 10.6 28 VDC or 115
VACC124a
FDR F100 solid-state flash memory
1⁄2 ATR short $33,510* ARINC 542A, pneumatic/electric analog I/O, 18-parameter nonimal, legacy aircraft non-FDAU applications.S703-100-00
25 hr. 18.0 28 VDC or 115 VACC123b, C124a
FDAU F3000 solid-stateflash memory
7.6 x 6.2 x 12.5 $49,570* ARINC 542A, pneumatic/electric ana-log I/O, 18-parameter nominal; Legacy aircraft non-FDAU applications.*BCA estimate.
3000-1X00-0XN/A 7.5 28 VDC
N/A
FA2300 Series solid-stateflash memory
1⁄2 ATR short $74,919 to $81,661
(see remarks)
ARINC 404A/757/747, EUROCAE MOPS. ED-56A/ED-55, RTCA/DO-160C RTCA/DO-178B. Models available for King Air 350; Bell 412/212, 430; ALH; Agusta A109; Boeing CH-47; Sikorsky US-60.
MADRAS
25 hr. 16.0 28 VDCC123b/C124a
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 182 / Version: #1
182 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
cocKPit Voice recorders (cVr)/FliGHt data recorders (Fdr)
Manufacturer
Type Recording Medium Size PriceRemarksModel
Duration Weight (lb) Power RequiredTSO
Universal Avionics Systems Corp.3260 E. Universal WayTucson, AZ 85756(520) 295-2300Fax: (520) 295-2395www.uasc.com
Combi CVR/FDR solid-stateflash memory 6.0 x 4.9 x 8.0 $19,5000
No internal batteries. No periodic maintenance. Four channels of cockpit audio data, UTC from ARINC 429 bus, UTC from a Frequency Shift Keying (FSK) signaling source, Rotor Speed for helicopter application. ARINC 717 Flight Data Recording, analog/digital sensor signals via FDAU, ARINC 758 data link information. PC-based ramp testing/diagonstics.
CVFDR-145
120-min. voice & ambient audio +25 hrs. (min.)
Flight data +120 minute data link
messaging
7.0 28 VDCC123b, C124b, C177, C123a,
C124a, EUROCAE ED-112
Combi CVR/FDRw/ embedded
Redorded Inde-pendedt Power Supply (RIPS)
solid-stateflash memory 6.0 x 4.9 x 8.0 $27,500
Embedded RIPS. Solid state memory. No internal batteries. No periodic maintenance. Four channels of cockpit audio data, UTC from ARINC 429 bus, UTC from a Frequency Shift Keying (FSK) signaling source, Rotor Speed for helicopter application. ARINC 717 Flight Data Recording, analog/digital sensor signals via FDAU, ARINC 758 data link information. PC-based ramp testing/diagonstics.
CVFDR-145R
120-min. voice & ambient audio +25 hrs. (min.)
Flight data +120 minute data link
messaging
8.68 28 VDC
C123b, C124b, C155, C177,
C123a, C124a, EUROCAE ED-112
CVR solid-stateflash memory 6.0 x 4.9 x 8.0 $16,500 No internal batteries. No periodic
maintenance. Four channels of cockpit audio data, UTC from ARINC 429 bus, UTC from a Frequency Shift Keying (FSK) signaling source, rotor Speed for helicopter applications, ARINC 758 data link information. PC-based ramp testing/diagonstics.
CVR-120A
120-min. voice & ambient audio 7.9 28 VDCC123b, C177,
C123a, EUROCAE ED-112
CVR w/embed-ded Recorded In-dependent Power
Supply (RIPS)
solid-stateflash memory 6.0 x 4.9 x 8.0 $24,500
Embedded RIPS. Solid-state memory. No internal batteries. No periodic maintenance. Four channels of cockpit audio data, UTC from ARINC 429 bus, UTC from a Frequency Shift Keying (FSK) signaling source, rotor speed for helicopter applications. ARINC 758 data link information. PC-based ramp testing/disgonstics.
CVR-120R
120 min. voice & ambient audio 8.68 28 VDCC123b, C155,
C177, C123a, EU-ROCAE ED-112
FDR solid-stateflash memory 6.0 x 4.9 x 8.0 $16,500
No internal batteries. No periodic maintenance. ARINC 717 Flight Data Recording. Additional data storage beyond 25 hrs., analog/digital sensor signals via FDAU. PC-based ramp test-ing/diagonstics.
FDR-25
25 hrs. (min) Flight data + 120
min. data linkmessaging
7.9 28 VDCC124b, C124a, EUROCAE ED-112
BCA • ISSUE: May 2009 PAGE: 183 / Version: #1
Business & Commercial Aviation | May 2009 183www.AviationWeek.com/bca
Heads uP disPlaysManufacturer Model Inputs & Outputs
Units/Weight (lb) PriceRemarks
Size or Form Factor Power Required
Rockwell Collins (Head UpGuidance Systems)16600 S.W. 72nd Ave.Portland, OR 97224(503) 443-3050www.rockwellcollins.com
HGS-4000ARINC 429, various discretes, enhanced
vision, synthetic vision
48.0 $397,481 Category III HUD available on a number of business and regional jet aircraft. Non-CAT III on Bombardier Challenger 604.NA
aircraFt situation disPlays
ManufacturerModel Display
Inputs OutputsUnits/Weight (lb) Price
RemarksTSO Display Size Size or Form
FactorPower
Required
Aspen Avionics5001 Indian School Rd. NEAlbuquerque, NM 87110(505) 856-5034Fax: (505) 314-5440www.aspenavionics.com
AT300 Hazard
Awareness Display
AMLCD
VSI,GPS
display
pilot sect-able zoom
scales of 5, 10, 20, 40, 60, 80 and
100 nm
1/1.0 $2,995*
Unit can replace the primary Verti-cal Speed Indicator in standard 3-inch instrument cutout. Shows aircraft vertical speed, graphically depicts the current GPS leg and active waypoint on the moving map display, and shows either side view terrain or textual GPS navigation information (current wpt, distance, groundspeed, etc.). The unit also displays airport symbols for all hard surfaced U.S. airports. Continuously displays current aircraft track and current aircraft height above ground (derived from the terrain database and barometric altitude). 15 Arc Second (1/4 mile) resolution full continental U.S. terrain and ob-stacle coverage. *BCA estimate.
C8d,C113 3.0 in. 3.3 x 3.3 x
3.812 or
28 VDC
EFD 1000 Pro Pilot
TFT AM-LCD
(400 x 760) ARINC 429
(5)RS-232 (5)
Pitot/staticquick
connect
ARINC 429 (1)
RS-232 (3)
display:2.6 lb
w/mounting bracket
remote sensor:0.2 lb
$5,995*
Includes integral ADAHRS backup battery and emergency GPS, integral altitude alterter/preselect, GPS flight plan map views: 360° and arc, slaved di-rectional gyro with heading bug. *BCA estimate,
C2d, C3d, C4c, C6d,
C8d, C10b, C106, C113
6.0-in diag.
display:3.50 x 7.0 x
4.15depth:
6.35 in. remote sensor:2.65 x 4.40 x
1.0 in.
14-28 VDC
(provided by PFD)
EFD 1000 Pro
TFT AMLCD(400 x 760) ARINC 429
(5)RS-232 (5)
Pitot/staticquick
connect
ARINC 429 (1)
RS-232 (3)
display:2.6 lb
w/mounting bracket
remote sensor:0.2 lb
$9,995*
Same as EFD 1000, plus full EHSI with dual bearing pointers; dual GPS, dual VHF nav support; sutopilot and flight director integration; integral GPS steer-ing; base map with curved flight paths; (optional) traffic, weather overlays. *BCA estimate,
C2d, C3d, C4c, C6d,
C8d, C10b, C106, C113
6.0-in. diag.
display:3.50 x 7.0 x
4.15depth:
6.35 in.remote sensor:2.65 x 4.40 x
1.0 in.
14-28 VDC
(providedby PFD)
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 184 / Version: #1
184 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
aircraFt situation disPlays
ManufacturerModel Display
Inputs OutputsUnits/Weight (lb) Price
RemarksTSO Display Size Size or Form
FactorPower
Required
Avidyne Corp.55 Old Bedford Rd.Lincoln, MA 01773(800) 284-3963Fax: (614) 885-8307www.avidyne.com
MHD 300 AMLCD RS-232ARINC 429
ARINC 568 (DME)
ARINC 429
2.0/0.9 kg$7,990*$10,990 with NVG
Interface applications with Avidyne TAS600-Series, Stormscope WX-500, Honeywell Class B TAWS (EGPWS), TCAS I, NVG compatible, DME. *BCA estimate.C147, C118 3 ATI 3.26 x 3.26
x 8.510-30 VDC
Chelton Flight Systems1111 West Jefferson Ste. 500Boise, ID 83702(208) 389-9959www.cheltonflight systems.com
EFIS LCD
ARINC 429, Storm-
scope WX-500, TCAS,
TCAD, ARINC,
RMI, ADF, FMS, OAT,
VS, GS deviation, landing
gear, DH, GPS,
RS-232
display, an-nunciators and aural warnings
—
$70,000* one
screen including
all sensors
TAWS moving map display, WSI wx, terrain with waterways, TCAS I/II, lightning, Jeppesen Nav-Data, FAA NACO obstructions availlable by subscription.DO-178B 6.0 software TSOed.*BCA estimate.
C113, C110a,
C151b, C92c
6.4-in. diag.
5.5 x 6.25 x 4.5
11-33 VDC
Eventide, Inc.One Alsan WayLittle Ferry, NJ 07643(201) 641-1200Fax: (201) 641-1640www.eventide.com
ARGUS5000/7000
mono-chrome
CRTARINC, RMI
Storm-scope, ADF, Loran, GPS and FMS
via RS-232 or RS-422*
—
5000: 1/3.57000: 1/4.5
5000:$4,4957000:
$5,495,U.S. &
No. Am. databases;$5,995,
international database
*Optional ARINC 419 and 429 adapter, $995. Optional ARINC weather adapter, $1,990. Other optional adapters, accesso-ries and software available. Database updates via Internet access available at additional cost. Ryan TCAD display soft-ware, $495.
C113
5000:3.2 x 3.2
7000:3.2 x 4.8
5000: 3 ATI3.2 x 3.2 x
10.257000: 3.2 x 4.8 x 10.75
11-33 VDC
ARGUS5000CE/7000CE
four-color CRT ARINC, RMI
Storm-scope, ADF, Loran, GPS and FMS
via RS-232 or RS-422*
—
5000CE: 1/3.5
7000CE: 1/4.5
5000CE:$6,995,
U.S. & No. Am.
databases;$7,495,
international database
7000CE:$8,995,
U.S. & No. Am.
databases;$9,495,
international database
*Optional ARINC 419 and 429 adapter, $995. Optional ARINC weather adapter, $1,990. Other optional adapters, accesso-ries and software available. Database updates via Internet access available at additional cost. Ryan TCAD display soft-ware, $495.
C113
5000CE:3.2 x 3.27000CE:3.2 x 4.8
5000CE:3 ATI short3.2 x 3.2 x
10.257000CE: 3.2 x 4.8 x 10.75
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 186 / Version: #1
186 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
aircraFt situation disPlays
ManufacturerModel Display
Inputs OutputsUnits/Weight (lb) Price
RemarksTSO Display Size Size or Form
FactorPower
Required
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
Bendix/KingKMD 150
LCD RS-232,WX-500
— 1/3.3 $5,638 with GPS
$4,484without
GPS
Includes GPS and internal terrain database.
none 5-in. diag. 4.0 x 6.25 x 6.9
11-33 VDC
Bendix/KingKMD 550
LCD RS-232, ARINC 429,
datalink, EGPWS, traffic,
NTSC video & WX-500
display 1/5.0 $9,308 Multi-function display for IHAS 5000 (Integrated Hazard Aware-ness System). Can be interfaced to display GPS, TIS, TAS, FIS, EGPWS, Wx radar 500 and NTSC video. Includes internal terrain and obstacle database.
C113, C63, C110a
5-in. diag. 4.0 x 6.2 x 10.0
11-33 VDC
Bendix/KingKMD 850
LCD RS-232, ARINC
429, radar, datalink, EGPWS, traffic,
NTSC video & WX-500
display 1/5.0 $15,736 Multi-function display for IHAS 8000 (Integrated Hazard Aware-ness System). Can be interfaced to display GPS, TIS, TAS, FIS, EGPWS, Wx radar 500 and NTSC video. Includes internal terrain and obstacle database.
C113, C63a, C110a
5-in. diag. 4.0 x 6.2 x 10.0
11-33 VDC
KDR 610XM Weather
Receiver
seeremarks
weather displays via XM satellite
interfaced to Bendix/King KMD 250, KMD 550 and KMD 850
MFDs
1/1.5 $4,401 Part of an MFD system; data link weather receiver provides high- speed textual and graphical weather to the cockpit. Available weather products include com-posite NEXRAD radar, graphical METARs, AIRMETS and SIGMETS. The active flight plan can be overlaid on all graphical weather images. System enables user to pan, zoom and interrogate areas of interest via joystick.
C157 seeremarks
see remarks 10-32 VDC
HoneywellMFRD
LCD RS-232 ARINC
429, radar, datalink,EGPWS, traffic,
NTSC video
display 1/7.0 $47,816 Multi-function display of weather radar, traffic, terrain, navigation maps.
C63c, C110a,
C113, C196
6 in. diag. 4.8 x 6.2 x 8.4
NA
Rogerson-Kratos403 S. RaymondPasadena, CA 91109(626) 449-3090www.rogersonkratos.com
5 ATI EFIS AMLCD flat panel
analog synchro
(XYZ, Sin/Cos) vari-
able AC/DC discretes & digital
ARINC 429, 419, 453, 735, RS-
232
analog synchro
(XYZ, Sin/Cos) vari-
able AC/DC discretes & digital
ARINC 429, 419, 453, 735, RS-
232
1/7.75 $42,000* One, two or four programmable, self-contained flat-panel AMLCD EADI and EHSIs. Radio altimeter functions such as DH, expanded scale for landing helicopter operations, TCAS I and II, and EGPWS display capability, in addition to standard ADI, HSI, bearing pointers, CDI, autopilot annunciation, flight director cross bars or ‘V’ bars. Upgrade packages available. *BCA estimate.
C3d, C4c, C5e, C6d, C8d, C9c,
C34e, C35d, C36e, C40c, C41d, C52b, C63c, C66c,
C67, C87, C92c, C113, C117a, C118,
C119b, C129a, C147,
C161a
5 ATIor 6.4-in. diagonal
5 ATI or 6.4 dia.
28 VDC44 W max
BCA • ISSUE: May 2009 PAGE: 187 / Version: #1
Business & Commercial Aviation | May 2009 187www.AviationWeek.com/bca
aircraFt situation disPlays
ManufacturerModel Display
Inputs OutputsUnits/Weight (lb) Price
RemarksTSO Display Size Size or Form
FactorPower
Required
Sandel Avionics2401 Dogwood WayVista, CA 92081(877) 726-3357(760) 727-4900Fax: (760) 727-4899www.sandel.com
SA4550 Primary Attitude Display
rear projection
LCD w/LED back-lighting
analog: attitude
glideslope, locai-
izer, flight director
command inputs,
radar altim-eter mode annuncia-
tors
N/A 1/3.4 $20,950* Designed to upgrade legacy ADIs. Incorporates flight director command bars, glideslope/ localizer deviation scale, fast/ slow indicator and mode annun-ciations. Selectable single-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 20-33 VDC40 W
Universal AvionicsSystems Corp.3260 E. Universal WayTucson, AZ 85756(520) 295-2300Fax: (520) 295-2395www.uasc.com
EFI-550 AMLCD ARINC6 - 429/4191 - 561/568
2 - 453/708A2 - RS 4224 - analog30 - dis-cretes*
ARINC429/49 (2)RS 422 (2)6 - analog
8 - dis-cretes
1/7.1 $35,000* *Depending on configuration.
C3d, C4c, C5e, C6d,
C52b, C105, C113
3.35 x 4.36
5.5-in. dia.
(EFIS-85 std.)4.8 x 5.18 x
7.90(from front mount sur-
face)
28 VDC
EFI-640 AMLCD ARINC6 - 429/4191 - 561/5682 - 453/708A2 - RS 4224 - analog30 - dis-cretes*
ARINC429/49 (2)RS 422 (2)6 - analog
8 - dis-cretes
1/7.8 $36,000* Horizontal viewing angles of +/-60°.; electronically adjusted vertical viewing 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 ATI5.18 x 6.18
x 7.9(from front
mount surface)
28 VDC
EFI-890R active matrix
color LCD
Analog:6 - ARINC 429
5 - CSDB2 - ARINC 7083 - Manchester
bus ports2 - VGA or
1 - RDR-1E/F & 1 - VGS,
2 - RS-170 or2 - NTSC
comp. or 18:1 1 - RS-232
(maint.)
Digital:28 GND/OPN
discretes14 - 28 VDC/
OPN4 - ARINC 407
with 2 ref. inputs
15 - analog DC
Analog:2 - ARINC
4292 - CSDB1 - Man-
hester bus port
Digital:5 - GND/OPN
discretes3 - 28
VDC/OPN discretes6 - analog resolvers2 - DC dif-ferential
2 - DC single ended
1/12.0 $60,000* 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 dim-ming range. *Depending on configuration.
C2d, C3d, C4c, C5e, C6d, C8d,
C10b, C34e, C35d, C36c, C40c, C41d, C52b, C63c, C66c, C87, C92c, C95,
C105, C113, C115b, C118, C119a, C129a, C151a
6.3 x 6.3(8.0 in dia.)
bezel:7.84 h x 7.42 w
depth:9.79
(back of bezel to rear of con-
nector)
28 VDC
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 188 / Version: #1
188 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
electronic FliGHt BaGs
ManufacturerModel Display
Inputs OutputsUnits/Weight (lb) Price
RemarksClass Display Size Size Power
Required
Advanced DataResearch Florida1765 Star Batt Dr.Rochester Hills, MI 48309(248) 299-5300, Ext. 235Fax: (248) 299-5319www.adrsoft.com
FG 7100EFB Kit
WXGA transmissive
LCD with vertical por-trait screen
(1280 x 768)
2 USB 2.0, ex-ternal monitor, PCMCIA card slot, secure Digital (SD)
card, modem (RJ-11), eth-
ernet (RJ-45), headphone, mic, docking
port
VGA, sound 2 serial (with PC-MCIA adapter)
1/2.21$4,995
Fujitsu Lifebook P1630 coputer with 1.2 GHz Intel Core 2 Duo VLV processor, 1 GB memory (2 GB) optional), 80 GB hard drive (120 GB and 64 GB solid-state drive optional); integrated 802.11 a/b/gDraft N and Bluetooth wireless LAN, PCMCIA and SD drives; Windows XP Tablet Edition, DVD + RW drive and cable, AC adapter, FCS software. Optional TSO’d power supply, plus many other options.
Class II 8.9-in. diagonal
9.3 x 6.6 x 1.5 16 VCDC
FG6000RR EFB Kit
SVGA LCD with touch
screen(800 x 600)
1 USBmodem
(RJ-11), Eth-ernet (RJ-45), one PCMCIA
port, 802-11b wireless
headphone microphone, docking port
1 USB modem (RJ-11), Ethernet
(RJ-45), one PCMCIA port, headphone microphone, docking port
3.5 lb with battery pack $5,950
A re-manufactured 4000 series Fujitsu P-866 pen-based computer modified by ADR for use in the cockpit. Fujitsu based High-Bright com-puter. This is a mission specific legacy product used with existing STC mounts. Includes Fujitsu LT-P867 computer with Windows 2000, FCS Software and Advanced Help Desk, high-bright screen, dimming enhancements, USB CD-ROM, AC adapter, DC adapter, slipcase and six pens, keyboard, battery, one-year warranty, one-year loaner protection plan.
8.4-in. diagonal
8.3 x 6.3 x 1.51 16 VCDC
CMC Esterline600 Dr. FrederickPhillips Blvd.Montreal, Quebec, CanadaH4M2S9(514) 748-3184Fax: (514) 748-3100www.cmcelectronics.ca
Pilot-ViewCMA-1100
(8.4 in.) or
CMA-141 (10.4 in.)
touch-screenXGA AMLCD1024 x 768
Intel 1.4 GHZ 16 GB stor-age memory
EEMU: 28 VDC, ARINC 429 (1 Rx); Ethernet 10/100, USB 2.0 (2), RS 232/422,
RS-170/NTSC; video, descrete
I/O (4xl)
EDU: condi-tioned 18 VDC USa 2.0 (2); PCMCIA Type
II wireless 802.11 a/b/g
EEMU: condi-tion 18 VDCARINC 429
(2Tx)Discrete I/O
(2 x O)video GPS position
EDU: sunlight readable,
fully dimmable display (0.5 -
800 nits)
8.4-in. EDU: 3.510.4-in. EDU: 4.0
EEMU: 2.0
8.4-in. units:
$25,88010.4-in. units:
$28,880
Touch-sensitive screen and line select keys with intuitive pilot interface. Applications include: electronic charts (Jeppesen, Lido, EAG, etc.), checklists, performance calcula-tion, e-documents, e-techlog, moving maps and weather. EFB system comprises Electronic Display/Processor Unit (EDU), Enhanced Expansion Module Unit (EEMU).
Class 28.4-in. or 10.4-in. diagonal
8.4-in. EDU: 8.5 x 6.1
x 1.5
10.4-in. EDU: 8.0 x 9.6
x 1.6EEMU: 1.9 x
6.9 5.1
22-33 VDC
L-3 Communications Display Systems1355 Bluegrass Lakes Pkwy.Alphareta, GA 30004(770) 752-7000Fax: (770) 752-5525www.L-3com.com
Crewmate EFB XGA-AMLCD
ARINC 429, WSI weather module, RS-
232/422 serial USB 2.0, Ether-net 10/100 (3), RS-170a NTSC, IEEE 802.11,
Wi-Fi, Bluetooth
sunlight read-able touch
screen
3.9 $80,869* Includes two display units and two aircraft interface units. One-hour battery and univer-sal charger included. Microsoft Windows OS.*BCA estimate.
Class 2 8.4-in. diagonal
6.0 x 9.0 x 2.62
input from AIU or
external universal charger;
30 W max; voltage
protection
BCA • ISSUE: May 2009 PAGE: 189 / Version: #1
Business & Commercial Aviation | May 2009 189www.AviationWeek.com/bca
electronic FliGHt BaGs
ManufacturerModel Display
Inputs OutputsUnits/Weight (lb) Price
RemarksClass Display Size Size Power
Required
Flight Deck resources16 Technology Dr.Ste. 142Irvine, CA 92618-2324(949) 679-9900www.flightdeck.aero
Sky Tab 3200 EFB LED
2 USB 2.0 PCMCIA, SD slot, 802.11 wireless, Blu-
etooth
N/A
802.11 wireless, Bluetooth
1/3.0 N/A 1 GB RAM, Microsoft Windows XP Pro OS, Linux compatible; 8 GB standard solid state hard drive (up to 64 GB optional). No stylus required; full dimmin dunctionality.
Class 1
8.4-in. diag, 800 x 600 dpi touch-
screen
162 x 210.5 x 35 mm 13.5
Sky Tab 2500 EFB LCD
3 USB 2.0, PCMCIA,
earphone, microphone, VGA, 802.11 wireless, Blu-
etooth, 10/100 Ethernet
AC-97 audio, 16 bit stereo, built-in speak-ers, 802.11
wireless, Bluetooth
1 3.0 N/A 1 GB RAM, Microsoft Windows XP Pro OS, 1.2 GHz CPU, 160 GB hard drive (optional solid state hard drive up to 32 GB); front panel buttons include six hot key quick access, one multi-directional, one select. No stylus required.
Class 1
10.2-in. in TFT LC SVGA 1024 x 600 dpi; portrait or landscape
resistive touchscreen
10.23 x 7.87 0.98
removalble Li-ion bat-
tery (4 hrs.)
Sky Tab 1500 EFB LCD 3 USB 2.0, 1 -
IrDA port, PCM-CIA, earphone, microphone, 802.11 wire-
less, Bluetoth, 10/100 Ether-net, 56K mo-dem, miniVGA
AC-97 audio, 16 bit stereo, built-in speak-ers, 802.11
wireless, Bluetooth
1/2.62 N/A 1 GB RAM, Microsoft Windows XP Pro OS, 1/2 GHZ CPU, 40 GB hard drive (optional upgrade to 120 GB), optional solid state hard drive. No stylus required.Class 1
8.4-in. TFT LCD SVGA 800 x 600 dpi portrait
or landscape resistive
touchscreen
9.09 x 7.55 x 9.0
removalble Li-ion bat-
tery (4 hrs.)
Sky Tab 1300 LCD
2 USB 2.0 ports, 1
PCMICA port, headphone, microphone, 802.11 wire-
less, Bluetooth
VGA display, 802.11
wireless, Bluetooth
1/2.05 NA 30 GB standard hard drive, optional 8 GB solid-state flassh drive. No stylus required. AC/DC adapter.
Class 1
10.0-in. TFT LCD, resistive
touchscreen, 1024 x 768 dpi resolu-
tion
8.3 x 10.10.3 x 0.8
14 W inter-nal battery (est. two-hr.
typical run time),
optional 28 W external battery (hot swappable), optional 72 W tethered pouch bat-
tery.
Sky Tab 2300 LCD
1 USB 2.0 port, 1 PCMCIA port,
headphone, microphone, 802.11 wire-
less, Bluetooth
802.11 wireless, Bluetooth
1/1.9 NA Microsoft Windows XP Tablet PC OS, 30 GB standard hard drive, optional 8 GB solid state flash drive. No stylus requried. AC/DC adapter.
Class 1
8.4-in. TFT LCD, nced di-rect sunlight
readable, 800 x 600 dpi resolu-
tion
7.9 x 9.6 x 0.8
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 190 / Version: #1
190 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
electronic FliGHt BaGs
ManufacturerModel Display
Inputs OutputsUnits/Weight (lb) Price
RemarksClass Display Size Size Power
Required
Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, AZ 85034(800) 601-3099 Fax: (602) 365-3343www.honeywell.com
AV 8012 Tablet PC
Bluetooth, 2 x USB, RJ-45 IrDa port DC
power in
—
2/2.4
From $4,449
(one year database
and software subscrip-
tion, $299
Portable multifunction-like display features D synthetic vision system with EFB capabilities, weather, traffic and can host flight planning applications. The Mobile Computer Platform (MCP) is a tablet PC that draws power from the aircraft’s power supply. The WAAS/GPS-enabled INU is a 3-D solid-state gyro inertial navigation sensor, Baro pressure sensor, battery backup, andBluetooth wireless interface. Optional Satel-lite Weather Receiver Unit provides NEXRAD, TAFs, METARS, TFRs and NOTAMs. The receiver communicates with the MCP via a wireless Blu-etooth connection.
Class I7.0-in. WS VGA touch screen LCD
8.9 x 4.8 x 9.0
INV: 7.4 x 1.6 x 5.3
12-32 VDC
NavAero9-15 W. Hubbard St.5th FloorChicago, IL 60610(866) 628-2376Fax: (312) 423-9966www.navaero.com
t-BagC2e EFBcolor TFT
LCD resistive touch screen
CPU: 1 USB slotConnectors: 61
pin sealed cradle connector, tPad
interface,3 USB,
1 RS-2321 LAN
CPU: 1 USB slotConnectors:
61 pin sealed cradle con-nector, tPad interface,3 USB,
1 RS-2321 LAN
1/NA
$3,495* with 8.4-in.
display$3,995*
with 10.4-in. display
*Installation kit extra. Class 2 EFB can be used to store, retrieve, display and use a wide variety of required documents and procedures such as opera-tions specifications, per-formance data, operations manuals, MELs, control documents and video sur-veillance. CPU: 1 GHz pro-cessor, 40GB hard drive, 512MB memory, Windows XP Professional OS. Removable CPU module computer system contains CPU, power supply and emergency battery backup nickel cadmium power pack. *BCA estimate.
Class 2 8.4 in. or 10.4 in.
93.8 x 113.8 x 23.8 excluding
connectors and mounting
hardware
13.8-30 VDC60 W maxi-
mum
Universal Avionics Systems Corp.3260 E. Universal WayTucson, AZ 85756(520) 295-2300Fax: (520) 295-2395www.uasc.com
ASU(Application Server Unit)
UCDT IIItouch screen
terminal display
4 ARINC 429, 8 discrete,
2 NTSC video1 S video
10/100 base T network capability
1 ARINC 4294 discrete,
10/100 base T network capability
Remote ASU1/8.9
1/ MCU$30,000
Provides supplementary display for viewing elec-tronic charts, checklists and external video sources. As an electronic flight bag (EFB), the ASU supports a terminal area chart database via Jeppesen, Inc. Charts, NOTAMs and airport infor-mation downloaded from CD-ROM and stored in flash memory within ASU. Flight plan departure and arrival airport information from FMS prompts dis-plays of departure, arrival and approach charts and airport diagrams. Manual searches accomplished via pull-down menu and touch-screen keyboard. Two user-defined zoom levels. System overlays aircraft position onto ap-proach charts and airport diagrams.
Class 2 5.0 x 6.50 in.
8.4-in. diag
UCD terminal III1/2.8
6.45 x 8.43 x 1.48
powered by UCD
BCA • ISSUE: May 2009 PAGE: 191 / Version: #1
Business & Commercial Aviation | May 2009 191www.AviationWeek.com/bca
enHanced Vision systeMs (eVs)Manufacturer
Model DisplayInputs Outputs
Units/Weight (lb) PriceRemarks
TSO Display Size Size Power Required
EMS SATCOM400 Maple Grove Rd.Ottawa, OntarioK2V 1B8 Canada(800) 600-9759Worldwide +1 613 591 1043www.emastcom.com
CMA-2600 SureSight I-seriesEVS-IR Sensor
HUD and head down
display (HDD)
single, dual-band sensor operating
in the short to me-
dium wave-lengths, 1-5
micronsARINC 429
RS 422 descretes
2-ANSI/SMPTE 170M
ARINC 429 RS 422
descretes
1/LRU21.0 $278,900*
When used with a HUD as part of a certified EVS, infrared sensor provides situ-ational awareness to pilot for night and low-visibility situations.*BCA estimate.Transport
Canada AP-55
dependent on HUD/
HDDNA 28 VDC 70 W
(nominal)
SureSight M-Series EVS-IR sensor
head-down display
single infra-red sensor operating in the long wavelength from 8-14 microns
1-ANS/SMPTE 170M
1/LRU2.5 $57,200*
Infrared sensor pro-vides situation aware-ness to pilots for night and low-visibility situation.*BCA estimate.
DO-160 dependent on HDD
2.54 x 2.4 x 6.0
28 VDC
Elbit Systems of AmericaCommercial Aviation Systems - Kollsman220 Daniel Webster Hwy.Merrimack, NH 03054 (603) 889-2500www.kollsman.com
All Weather Window
Enhanced Vision
System II (EVSII)
HUD/HDD 1-5 micron forward-
looking in-frared (FLIR)
sensor; ARINC 429 discretes, RS-232, RS-422
RS-170 analog video; SMPTE 259; digital
video-output to any raster ca-
pable; head-up or head-down display, like a CRT or LCD
RS-422RS-232
ARINC 429SMPTE 170MSMPTE 259M
3/21.0 (available from Gulfstream)
Certified for FAR 91.175 (I) and (m) operational credit. Comprises three components and pro-vides both analog and digital video outputs for aircraft interface flexibility.
seeremarks N/A 1/2 ATR 28 VDC
General Aviation Vision System (GAVIS)
any RS-170 SMPTE,
170M video capable
head
8-14 micron forward
looking in-frared (FLIR) sensor; no
inputs to the system are
needed
RS-170 AND SMPTE ES
170M
1/3.5 $92,500*
*BCA estimate.
28 VDC
MAX-VIZ, Inc.16165 S.W. 72nd Ave.Portland, OR 97224(503) 968-3036www.Max-Viz.com
EVS-1000
head-down enhanced
vision system
single long wave infra-red sensor; ARINC 429
opt.
raster capable head-up dis-
play; indepen-dent cockpit LCD; video compatible
FMS CDU: vid-eo compatible MFD; ARINC
429 opt.RS-170 output with RS-232
interface
sensor head:2.8-in. dia. x 6.8 long/
2.5lb.
$83,400*
Tail/nose mounted infrared camera that provides a 40° field of view to a cockpit display for viewing by the cockpit crew. Installation kit and harness not included. Resolution 320 x 240 pixels. Independent cockpit LCD; video compatible FMS CDU; video vompatible MFD. Field of view (FOV) Head-down display 53° x 40° typical; special FOVs on request. *BCA estimate.
N/A 2.77 dia.
Power module:
3.75 x 5.0 x 2.5/2.5lb
electronics:10 W ypical
25 W peak at 28 VDC;
environmental:<50 W avg;125 W max(with heater)
EVS-2200Dual Sen-sor IR EVS
head-up or head-down enhanced
vision system dual long
wave infra-red sensor; ARINC 429
opt.
raster capable head-up dis-
play; indepen-dent cockpit LCD; video
compatible FMS CDU; analog video per RS-
170; ARINC 429 opt.
sensor unit:1/10.0
11,0 x 6.88 x 6.27
processor:1/5.0
1/4 ATR
$350,000* Dual sensor version of above. Field of view (FOV): 53° x 40° or 30° x 22.5°; others avail-able on request. Reso-lution 320 x 240 pixels. Includes wiring harness and connectors. *BCA estimate.
electronics: 50 W typical;
75 W peak at 28 VDC per DO-160 category Z
environmental: 225 W typical; 275 W peak;with window deicer on
N/A
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 192 / Version: #1
192 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
flight management systemsmanufacturer avidyne Chelton
flight systems CmC electronics freeflight systems, ltd.
freeflight systems, ltd.
model FMS900w efis Cma-9000 2101 approach Plus
2101 i/O approach Plus
CDU (See Legend) Display (See Legend) ACD215 F P LCD-C F C, LCD D LED D LED
Data entry format (See Legend) F | M, LCD* D S D D
RnP Certification RNP-0.3, -5, -10, BRNAV RNP-0.3 RNP-0.3, -10, BRNAV,
PRNAV BRNAV BRNAV
lateral modes
SIDs/STARs Airways Std. Std. Std. Std. Std. Std. Std. — Std. —# ARINC 424 Procedure Legs 23 23 23 4 4
Auto. FMS-to-NAV Direct-to-Resume Std. Std. — — — Std. — — — —Vertical nav modes (See Legend) M A M M, A* A A
Performance management Remote Radio tuning — Std. — Std. — Std. — — — —
tsOed nav sensors
(Internal or Remote)
C129 GPS C146 WAAS — Std. Std. * Std. A1 Std. A1 Std. A1VOR DME INS Std. — — Std. Opt. — Std. Std. Std. — — — — — —IRS Loran-C TACAN Std. — — Opt. — Opt. Std. — Std. — — — — — —
available # aRinC 429 (in/out) — 8/4 24/8 4/0 4/0
specific interfaces
ARINC 429 GPS — — Std. — Std.
S422A CSDB DME ARINC 429 DME — — — — — Std. — — — —
BENDIX 429 VOR ARINC 429 VOR — — — Std. — Std. — — — —ARINC 429 INS — Std. Std. * — —
aRinC Radar (in) Opt. — — — —
air Data (ADC in)
ARINC 565 ARINC 575 — — Opt. — * Std. — — Std. Std.Coarse/Fine A407 Synchro Std. Opt. * — Std.
ARINC 545 TAS Std. — * — Std.ARINC 429 ADC RS-232 ADC — — Std. Std. Std. — — Std. Std. Std.
fuel flow (in) (a) ARINC (B) RS-232 (C) Other B, C B, C A, 4-engine B B
aRinC 429 (out)
RS-232 Display Output — Std. — Std. Std.ARINC 429 LO-Xmtr (std./opt.) — 4/4 * —/— 2/0ARINC 429 HI-Xmtr (std./opt.) — 4/4 8/0* —/— 2/0
efis (out)
(a) ARINC 429 (B) ARINC 561 — A A —/— A/BARINC INS Format (out) — 429 429 — —
ARINC Long-Range Nav Format (out) — 429 429. 702 — 429
hsi format (out)
ARINC 429 HSI — — Std. — Std.ARINC 561 Course/Bearing — — Opt. — Std.
Course/Bearing A407 Synchro — — Opt. — Std.Analog L/R-U/D-T/F DC — Std. (no T/F) Opt. — Std.
a/P steering format (out)
ARINC 429R/S 429P/S Std. Std. Std. Std. Std. Opt. — — Std. —Analog Roll Steering Analog Pitch Steering — — Opt. Opt. Opt. Opt. — — Opt. —aRinC Dist. format (out) — 429 429, 561, 568 — A
afis/aRinC format (in/out) — — 429/429 — RS-422
Database/ Route
storage
# User Defined WPTs 200 500 500 250 250# Flight Plans # WPTs per Flight Plan 100 128 100 99 400 99 40 40 40 40
(D) Data Card, (C) Cartridge, (R) Disc Reader USB Mem. Stick D R D DCom. Freq’s Special Use Airspace Alerts Std. Std. Std. Std. Std. — — — Std. Std.
navaid frequencies (e) En Route (a) Approach E, A E, A E, A E E
Weight, Dimensions
& Power
Weight (lb) — 4.5 8.0 3.65 3.65CDU Height x Width x Length (in.) — 5.5 x 6.25 x 4.5 6.75 x 5.75 x 7.15 3.0 x 5.75 x 7.68 3.0 x 5.75 x 7.68
Power B A, B B A, B A, BRemote Computer Size (MCU) Weight (lb) — — — — — — — — — —
Power (std./opt.) (volts AC &/or DC) B A, B/DC B — —
Price $70,000* $70,000** TBD $7,245* $11,500*
Remarks
Integrated into Avidyne Entegra Release 9 Flight Deck System. *Included FMS900w, dual IFD500 diaplsys, dual VHF Comm/Nav and dual WAAS GPS sensors and ACD215 control panel
HUD symbology, 3-D synthetic vision, conformal terrain, Class A, B, C TAWS integral GPS/WAAS. *WAAS 145A/146. **Two screens, $95,200.
NVG display. *Advisory VNAV for climb, cruise,
descent, approach. Per-formance table based.
All ARINC 429 I/O configurable for speed/function. Converter units
available. VNAV ap-proaches. Enhanced
version available.
Price includes receiver, datacard, installation kit (with antenna), instal-lation manual and pilot guide. Unit also avail-able with night vision goggle compatibility.
*BCA estimate.
Price includes receiver, datacard, installation
kit (with antenna), installation manual and pilot guide. Sole means
oceanic approval; interfaces with EGPWS.
*BCA estimate.
COntROl DisPlay UnitP = Panel Mount CDU
f = Full Apha Keyboarda = Alpha KeyboardD = Other Dzus CDU
DisPlay C = Color m = MonochromeP = Penetration Phosphor Color
lCD = Liquid Crystal DisplayleD = Light Emitting Diode
Data entRy fORmatD = Direct
s = Scratchpad
VeRtiCal naV mODesm = Multi Waypoint
a = Advisorys = Single Waypoint
POWeRa = 10-19 VDCB = 20-40 VDC
C = 115 VAC
BCA • ISSUE: May 2009 PAGE: 193 / Version: #1
Business & Commercial Aviation | May 2009 193www.AviationWeek.com/bca
flight management systemsmanufacturer garmin
internationalgarmin
internationalgarmin
internationalgarmin
internationalgarmin
international
model gPs 500W gPs 155 Xl tsO gnC 300 Xl tsO gPs 165 tsO gPs 400W
CDU (See Legend) Display (See Legend) P C P LCD P LCD Rmks. Rmks. P C
Data entry format (See Legend) D D D D D
RnP Certification RNP-10, BRNAV BRNAV BRNAV BRNAV RNP-10, BRNAV
lateral modes
SIDs/STARs Airways Std. — Std. — Std. — Std. — Std. —# ARINC 424 Procedure Legs 19 — — — 19
Auto. FMS-to-NAV Direct-to-Resume — — — — — — — — — —Vertical nav modes (See Legend) A A A A A
Performance management Remote Radio tuning — — — — — — — — — —
tsOed nav sensors
(Internal or Remote)
C129 GPS C146 WAAS Std. * — — Std. A1 Std. A1 Std. *VOR DME INS — — — — — — — — — — — — — — —IRS Loran-C TACAN — — — — — — — — — — — — — — —
available # aRinC 429 (in/out) 2/0 1 1 2/0 2/0
specific interfaces
ARINC 429 GPS Std. Std. Std. Std. Std.
S422A CSDB DME ARINC 429 DME — — — — — — — — — —
BENDIX 429 VOR ARINC 429 VOR — — — — — — — — — —ARINC 429 INS — — — — —
aRinC Radar (in) — — — — —
air Data (ADC in)
ARINC 565 ARINC 575 Opt. Opt. — — — — — — Opt. Opt.Coarse/Fine A407 Synchro Opt. — — — Opt.
ARINC 545 TAS Opt. — — — Opt.ARINC 429 ADC RS-232 ADC Std. Std. — Std. — Std. — Std. Std. Std.
fuel flow (in) (a) ARINC (B) RS-232 (C) Other A, B B B B A, B
aRinC 429 (out)
RS-232 Display Output Std. Std. Std. Std. Std.ARINC 429 LO-Xmtr (std./opt.) 2/0 1/0 1/0 1/0 2/0ARINC 429 HI-Xmtr (std./opt.) 2/0 1/0 1/0 1/0 2/0
efis (out)
(a) ARINC 429 (B) ARINC 561 Std./Opt. Std./Opt. Std./Opt. Std./Opt Std./Opt.ARINC INS Format (out) — — — — —
ARINC Long-Range Nav Format (out) 429 429 429 429 429
hsi format (out)
ARINC 429 HSI Std. Std. Std. Std. Std.ARINC 561 Course/Bearing Opt. Opt. Opt. Opt. Opt.
Course/Bearing A407 Synchro Opt. Opt. Opt. Opt. Opt.Analog L/R-U/D-T/F DC Std. Std. Std. Std. Std.
a/P steering format (out)
ARINC 429R/S 429P/S Std. — — Std. Std. — Std. — Std. —Analog Roll Steering Analog Pitch Steering Opt. — Opt. — Opt. — Opt. — Opt. —aRinC Dist. format (out) 429 429 429 429 429
afis/aRinC format (in/out) — — — — —
Database/ Route
storage
# User Defined WPTs 1,000 1,000 1,000 1,000 1,000# Flight Plans # WPTs per Flight Plan 20 31 20 31 20 31 20 31 20 31
(D) Data Card, (C) Cartridge, (R) Disc Reader D D D D DCom. Freq’s Special Use Airspace Alerts Std. Std. Std. Std. Std. Std. — Std. Std. Std.
navaid frequencies (e) En Route (a) Approach E, A E, A E, A E, A E, A
Weight, Dimensions
& Power
Weight (lb) 6.9 2.4 2.4 2.0 4.9CDU Height x Width x Length (in.) 4.6 x 6.25 x 11.0 2.0 x 6.25 x 5.8 2.0 x 6.25 x 5.8 2.25 x 5.75 x 5.65 2.65 x 6.25 x 11.0
Power A, B A, B A, B A, B A, BRemote Computer Size (MCU) Weight (lb) — — — — — — — — — —
Power (std./opt.) (volts AC &/or DC) — — — — —
Price $14,000 $4,695 $5,595 $7,495 $8,795
Remarks
Fifteen-channel GPS with color moving map. New model from this OEM. FDE primary means remote and
oceanic. Terrain adviso-ries/TAWS-B. *C146a
WAAS approved for LPV approaches.
Fifteen-channel parallel GPS receiver with mov-
ing map display.
Fifteen-channel parallel GPS receiver with mov-ing map display. Five-
watt comm transmitter.
Display: vacuum fluorescent; comes
with a MultiTrac8 GPS receiver.
Fifteen-channel GPS with color moving map.
FDE primary means remote and oceanic.
*C146a WAAS approved for LPV approaches.
COntROl DisPlay UnitP = Panel Mount CDU
f = Full Apha Keyboarda = Alpha KeyboardD = Other Dzus CDU
DisPlay C = Color m = MonochromeP = Penetration Phosphor Color
lCD = Liquid Crystal DisplayleD = Light Emitting Diode
Data entRy fORmatD = Direct
s = Scratchpad
VeRtiCal naV mODesm = Multi Waypoint
a = Advisorys = Single Waypoint
POWeRa = 10-19 VDCB = 20-40 VDC
C = 115 VAC
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 194 / Version: #1
194 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
flight management systemsmanufacturer garmin
internationalgarmin
internationalgarmin
internationalhoneywell aerospace
honeywell aerospace
model gnC 420W/420aW* gnC 430W/430aW* gns 530W/530aW* Kln 94 gns-Xls
CDU (See Legend) Display (See Legend) P C P C P C D M F LCD
Data entry format (See Legend) D D D D D
RnP Certification RNP-10, BRNAV RNP-10, BRNAV RNP-10, BRNAV RNP-5, BRNAV RNP-0.3, -10.5, BRNAV
lateral modes
SIDs/STARs Airways Std. — Std. — Std. — Std. — Std. Std.# ARINC 424 Procedure Legs 19 19 19 — 10
Auto. FMS-to-NAV Direct-to-Resume — — Std. — Std. — — Std. — Std.Vertical nav modes (See Legend) A A A A A
Performance management Remote Radio tuning — — — — — — — — — Std.
tsOed nav sensors
(Internal or Remote)
C129 GPS C146 WAAS Std. ** Std. ** Std. ** Std. A1 Std. A1, B1, C1VOR DME INS — — — Std. — — Std. — — — — — Opt. Opt. Opt.IRS Loran-C TACAN — — — — — — — — — — — — Opt. — —
available # aRinC 429 (in/out) 2/0 2/0 2/0 3/0 13/0
specific interfaces
ARINC 429 GPS Std. Std. Std. — Std.
S422A CSDB DME ARINC 429 DME — — — — — — — — Std. Std.
BENDIX 429 VOR ARINC 429 VOR — — — Std. — Std. — — Std. Std.ARINC 429 INS — — — — Std.
aRinC Radar (in) — — — — Std.
air Data (ADC in)
ARINC 565 ARINC 575 Opt. Opt. Opt. Opt. Opt. Opt. Std. — Std. Std.Coarse/Fine A407 Synchro Opt. Opt. Opt. — Std.
ARINC 545 TAS Opt. Opt. Opt. — Std.ARINC 429 ADC RS-232 ADC Std. Std. Std. Std. Std. Std. Std. Std. Std. —
fuel flow (in) (a) ARINC (B) RS-232 (C) Other A, B A, B A, B B, C C
aRinC 429 (out)
RS-232 Display Output Std. Std. Std. Std. —ARINC 429 LO-Xmtr (std./opt.) 2/0 2/0 2/0 1/0 7/0ARINC 429 HI-Xmtr (std./opt.) 2/0 2/0 2/0 0/1 7/0
efis (out)
(a) ARINC 429 (B) ARINC 561 Std./Opt. Std./Opt. Std./Opt. A, B A, BARINC INS Format (out) — — — — 429, 571
ARINC Long-Range Nav Format (out) 429 429 429 429, 561 429
hsi format (out)
ARINC 429 HSI Std. Std. Std. Std. Std.ARINC 561 Course/Bearing Opt. Opt. Opt. Std. Std.
Course/Bearing A407 Synchro Opt. Opt. Opt. Opt. Std.Analog L/R-U/D-T/F DC Std. Std. Std. Std. Std.
a/P steering format (out)
ARINC 429R/S 429P/S Opt. — Std. — Std. — Std. — Std. —Analog Roll Steering Analog Pitch Steering Std. — Opt. — Opt. — Std. — Std. —aRinC Dist. format (out) 429 429 429 429, 561, 568 429, 561, 571
afis/aRinC format (in/out) — — — — RS-422
Database/ Route
storage
# User Defined WPTs 1,000 1,000 1,000 1,000 999# Flight Plans # WPTs per Flight Plan 20 31 20 31 20 31 25 30 56 50
(D) Data Card, (C) Cartridge, (R) Disc Reader D D D D DCom. Freq’s Special Use Airspace Alerts Std. Std. Std. Std. Std. Std. Std. Std. — —
navaid frequencies (e) En Route (a) Approach E, A E, A E, A E E
Weight, Dimensions
& Power
Weight (lb) 5.8 6.6 8.4 4.5 7CDU Height x Width x Length (in.) 2.65 x 6.25 x 11.0 2.65 x 6.25 x 11.0 4.6 x 6.25 x 11.0 3.75 x 5.75 x 9.46 4.5 x 5.75 x 7.62
Power A, B A, B A, B B BRemote Computer Size (MCU) Weight (lb) — — — — — — — — — —
Power (std./opt.) (volts AC &/or DC) — — — — —
Price $9,995 $11,295 $16,495 $5,883 $46,290
Remarks
Fifteen-channel GPS with color moving map and 8.33-kHz VHF comm. FDE primary means remote and oceanic.
*GNC 420AW, $14,495; incl. 16-watt min. comm TX. Terrain advisories/
TAWS-B. **C146a WAAS approved for LPV
approaches.
GPS and VOR/ILS receiver and 8.33-kHz
VHF comm. FDE primary means remote and oce-anic. Terrain advisories. *GNS 430AW, $15,750; incl. 16-watt min. comm
TX. **C146a WAAS approved for LPV
approaches.
GPS and VOR/ILS receiver and 8.33-kHz
VHF comm. FDE primary means remote and oceanic. Terrain
advisories/TAWS-B opt., $10,000. *GNS 530AW, $21,495; incl. 16-watt
min. comm TX. **C146a WAAS approved for LPV
approaches.
Add $1,000 for KA90 HSI adapter. BRNAV and primary means oceanic version available. RAIM
and FDE prediction. Database update via
Internet available.
Enhanced version avail-able. Optional RPU will display wx and EGPWS
graphics.
COntROl DisPlay UnitP = Panel Mount CDU
f = Full Apha Keyboarda = Alpha KeyboardD = Other Dzus CDU
DisPlay C = Color m = MonochromeP = Penetration Phosphor Color
lCD = Liquid Crystal DisplayleD = Light Emitting Diode
Data entRy fORmatD = Direct
s = Scratchpad
VeRtiCal naV mODesm = Multi Waypoint
a = Advisorys = Single Waypoint
POWeRa = 10-19 VDCB = 20-40 VDC
C = 115 VAC
BCA • ISSUE: May 2009 PAGE: 195 / Version: #1
Business & Commercial Aviation | May 2009 195www.AviationWeek.com/bca
flight management systemsmanufacturer honeywell
aerospaceRockwell Collins Rockwell Collins Rockwell Collins
model fmZ-2000 fms 3000/5000 fms 4200/6000 fms 6100
CDU (See Legend) Display (See Legend) F LCD, C F C/LCD F C/CRT F C/LCD
Data entry format (See Legend) Std. Std. Std. Std.
RnP Certification RNP-0.3 RNP-0.3, -10, BRNAV RNP-0.3, -10, BRNAV RNP-0.3, -10, BRNAV
lateral modes
SIDs/STARs Airways Std. Std. Std. Std. Std. Std. Std. Std.# ARINC 424 Procedure Legs 23 23 23 23
Auto. FMS-to-NAV Direct-to-Resume Std. Std. Std. — Std. — Std. —Vertical nav modes (See Legend) M, A M M M
Performance management Remote Radio tuning Rmks. Std. Std. Std. Std. Std. Std. Std.
tsOed nav sensors
(Internal or Remote)
C129 GPS C146 WAAS Std. B1, C1 Std. B1, C1 Std. B1, C1 Std. B1, C1VOR DME INS Std. Std. Std. — Std. Std. — Std. Std. Std. Std. —IRS Loran-C TACAN Std. — Opt. — Std. — — Std. — — Std. —
available # aRinC 429 (in/out) 21/0 4/3 4/3 4/3
specific interfaces
ARINC 429 GPS Std. * * *
S422A CSDB DME ARINC 429 DME Std. Std. * * * * * *
BENDIX 429 VOR ARINC 429 VOR — Std. * * * * * *ARINC 429 INS Std. * * *
aRinC Radar (in) Std. * * *
air Data (ADC in)
ARINC 565 ARINC 575 — — * * * * * *Coarse/Fine A407 Synchro — * * *
ARINC 545 TAS — * * *ARINC 429 ADC RS-232 ADC Std. — * * * * * *
fuel flow (in) (a) ARINC (B) RS-232 (C) Other A, C * * *
aRinC 429 (out)
RS-232 Display Output 6/0 — — —ARINC 429 LO-Xmtr (std./opt.) * 0/0 0/0 0/0ARINC 429 HI-Xmtr (std./opt.) * 0/0 0/0 0/0
efis (out)
(a) ARINC 429 (B) ARINC 561 A, B A A AARINC INS Format (out) — * * *
ARINC Long-Range Nav Format (out) 429 * * *
hsi format (out)
ARINC 429 HSI Std. * * *ARINC 561 Course/Bearing Std. * * *
Course/Bearing A407 Synchro Std. — — —Analog L/R-U/D-T/F DC Std. — — —
a/P steering format (out)
ARINC 429R/S 429P/S Std. — Std. Std. Std. Std. Std. Std.Analog Roll Steering Analog Pitch Steering — — — — — — — —aRinC Dist. format (out) 429, ASCB — — —
afis/aRinC format (in/out) 429 — — —
Database/ Route
storage
# User Defined WPTs 1,000 100 100 100# Flight Plans # WPTs per Flight Plan 3,000 100 1,000 100 1,000 100 1,000 100
(D) Data Card, (C) Cartridge, (R) Disc Reader R R R RCom. Freq’s Special Use Airspace Alerts — — — — — — — —
navaid frequencies (e) En Route (a) Approach E, A E, A E, A E, A
Weight, Dimensions
& Power
Weight (lb) 7 8.9 4 4CDU Height x Width x Length (in.) 7.13 x 5.75 x 6.75 6.375 x 5.75 x 6.33 6.375 x 5.75 x 6.33 6.375 x 5.75 x 6.33
Power B/B B B BRemote Computer Size (MCU) Weight (lb) 2 7.9 Rmks. 1.9 Rmks. 1.9 Rmks. 1.9
Power (std./opt.) (volts AC &/or DC) B/- — — —
Price $134,022 NA NA NA
Remarks
Performance management uses Honeywell SmartPerf as standard; Gulfstream IV/IV-SP
uses table-based performance. *HI/LO configurable.
LPV approach capability and RF legs are available on some air-craft types. *FMS I/O provided via 4 redundant concentrators. Remote computer dimensions
1.7 x 8.74 x 6.06 in.; FMS 5000 requires radio tuning unit. FMS 3000 radio tuning is internal.
LPV approach capability and RF legs are available on some air-craft types. *FMS I/O provided via 4 redundant concentrators. See FMS 3000 remarks. FMS 4200 has advisory VNAV but not FMS to ILS auto transfer. Coupled VNAV available on
FMS 6000.
*FMS I/O from the FMS via 4 redundant concentrators. See FMS 3000 remarks for
remote computer. WAAS/SBAS capable
COntROl DisPlay UnitP = Panel Mount CDU
f = Full Apha Keyboarda = Alpha KeyboardD = Other Dzus CDU
DisPlay C = Color m = MonochromeP = Penetration Phosphor Color
lCD = Liquid Crystal DisplayleD = Light Emitting Diode
Data entRy fORmatD = Direct
s = Scratchpad
VeRtiCal naV mODesm = Multi Waypoint
a = Advisorys = Single Waypoint
POWeRa = 10-19 VDCB = 20-40 VDC
C = 115 VAC
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 196 / Version: #1
196 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
flight management systemsmanufacturer Universal
avionics systemsUniversal
avionics systemsUniversal
avionics systemsUniversal
avionics systems
model Uns-1lw Uns-1ew Uns-1espw Uns-1fw
CDU (See Legend) Display (See Legend) F LCD-C F LCD-C F LCD-C F LCD-C
Data entry format (See Legend) D D D D
RnP Certification RNP-0.3, -5, -10 RNP-0.3, -5, -10 RNP-0.3, -5, -10 RNP-0.3, -5, -10
lateral modes
SIDs/STARs Airways Std. Std. Std. Std. Std. Std. Std. Std.# ARINC 424 Procedure Legs 23 23 23 23
Auto. FMS-to-NAV Direct-to-Resume Std. Std. Std. Std. Std. Std. Std. Std.Vertical nav modes (See Legend) M M M M
Performance management Remote Radio tuning Opt. Opt. Opt. Opt. Opt. Opt. Opt. Opt.
tsOed nav sensors
(Internal or Remote)
C129 GPS C146 WAAS Std. C146B Gamma Std. C146B
Gamma Std. C146B Gamma Std. C146B
GammaVOR DME INS Opt. Opt. Opt. Opt. Opt. Opt. Opt. Opt. Opt. Opt. Opt. Opt.IRS Loran-C TACAN Opt. Opt. Opt. Opt. Opt. Opt. Opt. Opt. Opt. Opt. Opt. Opt.
available # aRinC 429 (in/out) 8/5 Analog: 8/5; Digital: 16/8 8/5 Analog: 8/5; Digital: 16/8
specific interfaces
ARINC 429 GPS Std. Std. Std. Std.
S422A CSDB DME ARINC 429 DME Std. Std. Std. Std. Std. Std. Std. Std.
BENDIX 429 VOR ARINC 429 VOR Std. Std. Std. Std. Std. Std. Std. Std.ARINC 429 INS Std. Std. Std. Std.
aRinC Radar (in) Std. Std. Std. Std.
air Data (ADC in)
ARINC 565 ARINC 575 Opt. Std. Rmks. Std. Rmks. Std. Opt. Std.Coarse/Fine A407 Synchro Opt. Rmks. Rmks. Opt.
ARINC 545 TAS Opt. Rmks. Rmks. Opt.ARINC 429 ADC RS-232 ADC Std. — Std. — Std. — Std. —
fuel flow (in) (a) ARINC (B) RS-232 (C) Other A, C A, C A, C A, C
aRinC 429 (out)
RS-232 Display Output — — — —ARINC 429 LO-Xmtr (std./opt.) 3/3 3/3 1/1 3/3ARINC 429 HI-Xmtr (std./opt.) 2/2 2/2 1/1 2/2
efis (out)
(a) ARINC 429 (B) ARINC 561 A, B A, B A, B A, BARINC INS Format (out) 429, 571 429, 571 429, 571 429, 571
ARINC Long-Range Nav Format (out) 429, 561, 571 429, 561, 571 429, 561, 571 429, 561, 571
hsi format (out)
ARINC 429 HSI Std. Std. Std. Std.ARINC 561 Course/Bearing Std. Std. Std. Std.
Course/Bearing A407 Synchro Std. Std. Std. Std.Analog L/R-U/D-T/F DC Std. Std. Std. Std.
a/P steering format (out)
ARINC 429R/S 429P/S Std. Std. Std. Std. Std. Std. Std. Std.Analog Roll Steering Analog Pitch Steering Std. Std. Std. Std. Std. Std. Std. Std.aRinC Dist. format (out) 429, 561, 571 429, 561, 571 429, 561, 571 429, 561, 571
afis/aRinC format (in/out) 429 429 429 429
Database/ Route
storage
# User Defined WPTs 200 200 200 200# Flight Plans # WPTs per Flight Plan 200 2,000+ 200 2,000+ 200 2,000+ 200 2,000+
(D) Data Card, (C) Cartridge, (R) Disc Reader R R R RCom. Freq’s Special Use Airspace Alerts — — — — — — — —
navaid frequencies (e) En Route (a) Approach E, A E, A E, A E, A
Weight, Dimensions
& Power
Weight (lb) 2.9 7.86 7.25 4.1CDU Height x Width x Length (in.) 4.5 x 5.75 x 6.33 6.38 x 5.75 x 8.98 6.38 x 5.75 x 7.62 6.38 x 7.5 x 3.5
Power — — — —Remote Computer Size (MCU) Weight (lb) 2 7.5 — — — — 2 —
Power (std./opt.) (volts AC &/or DC) B/DC B/DC B/DC B/DC
Price $54,500 $69,000 $68,000 $81,500
Remarks
Air data converter unit avail-able; 3-D coupled approach
mode; PC program for remote/oceanic ops; UniLink text
compatible.WAAS/SBAS capable
200 pilot routes, 2,000 com-pany routes, air data
converter available; 3-D ap-proach; UniLink compatible; displays video and graphics.
WAAS/SBAS capable.
200 pilot routes, 2,000 company routes, air data con-verter available; 3-D approach; UniLink compatible; displays video and graphics. WAAS/
SBAS capable.
200 routes, 2,000 company routes, air data converter avail-
able; 3-D approach; UniLink compatible; displays video and graphics. WAAS/SBAS capable.
COntROl DisPlay UnitP = Panel Mount CDU
f = Full Apha Keyboarda = Alpha KeyboardD = Other Dzus CDU
DisPlay C = Color m = MonochromeP = Penetration Phosphor Color
lCD = Liquid Crystal DisplayleD = Light Emitting Diode
Data entRy fORmatD = Direct
s = Scratchpad
VeRtiCal naV mODesm = Multi Waypoint
a = Advisorys = Single Waypoint
POWeRa = 10-19 VDCB = 20-40 VDC
C = 115 VAC
BCA • ISSUE: May 2009 PAGE: 197 / Version: #1
Business & Commercial Aviation | May 2009 197www.AviationWeek.com/bca
Integrated avIonIcs systemsManufacturer Operational Capabilities Remarks
Avidyne Corp.55 Old Bedford Rd.Lincoln, MA 01773www.avidyne.com
FMS X PFD/MFD X Integrates primary flight information, navigation, ter-rain, wweather, traffic on two or three large-formate displays. Selectable IAS and V-speed ranges to suit aircraft installations. Dual-PFD version features Cross Compare System that monitors cross-side PFD and ADAHRS signals 30 times per sectond. Works with S-TEC 55X autopilot and 3rd-party GPS/NAV/COMs for position information.
EFIS X CAS/TAWS X
AP/IFCS RMU
EVS SVS
Model Certifications & TSOs
Entegra Release 8 FAR Part 23 X C113
Inputs/Type(s) Far Part 25 C115b
C3d X C117a
C4c X C118
C5e C119b
C6d X C129a
Outputs/Type(s) C8d X C145a
C9c C146a
C31d C147 X
C34e/C35d/C36e C151b X
CDU Type/Size(s) C40c C153 Price
C41d C154a
C52b C157 X
C63c X C158
C66c C159
Power Required C74c C161
C102 C162
C105 C163
Units/Weight (lb) C106 X C165
18.75 lb (two displays) C109 C166
C110a X C2d X
C112 C43c X
Integrated avIonIcs systemsManufacturer Operational Capabilities Remarks
Avidyne Corp.55 Old Bedford Rd.Lincoln, MA 01773www.avidyne.com
FMS X PFD/MFD X Integrates primary flight information, communication, navigation, WAAS GPS/FMS, terrain, weather, traffic on 2, 3 or 4 large-formate displays. Displays sizes include 8, 10, 12 and 15 inches. Modular design includes dual VHF NAV/COM, dual WAAS GPS, dual FMS90w, dual ADHARS, remote transponder tuning. ADC 215 aplha-numeric FMS keypad with display. Optional SVS and EVS. TSO’s include TSO C146b.
EFIS X CAS/TAWS X
AP/IFCS X RMU X
EVS SVS X
Model Certifications & TSOs
Entegra Release 9 FAR Part 23 X C113 X
Inputs/Type(s) Far Part 25 C115b
C3d XX C117a
C4c C118
C5e C119b
C6d X C129a
Outputs/Type(s) C8d X C145a
C9c C146a
C31d C147 X
C34e/C35d/C36e X C151b
CDU Type/Size(s) C40c X C153 Price
C41d X C154a
C52b X C157 X
C63c X C158
C66c C159
Power Required C74c C161
28 VDC C102 C162
C105 C163
Units/Weight (lb) C106 X C165
18.75 lb (two displays) C109 C2D X
C110a X C43C X
C112 C10b X
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 198 / Version: #1
198 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
Integrated avIonIcs systemsManufacturer Operational Capabilities Remarks
Chelton Flight Systems1109 Main St., 5th Fl.Boise ID 83702www.cheltonflightsystems.com
FMS PFD/MFD Provides “Highway-in-the-Sky” navigation; digital flight performance recorder; HUD symbology; 3-D terrain, traffic and towers; Integral GPS WAAS, Class A, B, or C TAWS; Class A or B HTAWS; color-coded airspace; Jeppesen NavData, 3 arc second terrain worldwide. Also certified to DO 170B, Level A, DO 160D, C2d FAR 27 and FAR 29.
EFIS CAS/TAWS
AP/IFCS RMU
EVS SVS
Model Certifications & TSOs
Chelton Flight Systems EFIS FAR Part 23 C113
Inputs/Type(s) Far Part 25 C115b
WX500, ADF, TCAS I/II, TCAD, ADS-B, TIS-B, RAD ALT, 8 RX ARINC 429, 20 RS 232, 4 RS 422, 10 programmable
discretes
C3d C117a
C4c C118
C5e C119b
C6d C129a
Outputs/Type(s) C8d C145a
4 TX ARINC 429, 12 TX RS 232, 4 TX RS 422, 2 programmable discretes, 2+
autopilot models
C9c C146a
C31d C147
C34e/C35d/C36e C151b
CDU Type/Size(s) C40c C153 Price
6.25 in. x 5.5 in. X 4.5 in.; full color, high resolution; 1,000 nit LCD with fully adjustable brightness; NVG com-patible, 4/5 lb
C41d C154a Two Screens: $95,000 (includes sensors, not installation)
Four Screen: $150,000 (includes sensors, not installation)
C52b C157
C63c C158
C66c C159
Power Required C74c C161
10 to 32 VDC; 1.4 amps @ 28 VDC (40 W max)
C102 C162
C105 C163
Units/Weight (lb) C106 C165
two-screen system, 2 lb; 4-screen system, 50 lb
C109 C166
C110a C169
C112
Integrated avIonIcs systemsManufacturer Operational Capabilities Remarks
Garmin International 1200 E. 151st St. Olathe, KS 66062www.garmin.com
FMS PFD/MFD Garmin G600 includes CDU (dual 6.5 in VGA LCD), digital AHRS, ADC, magnetometer, temperature probe. Also certified to C2d, C10b and C34c.
EFIS CAS/TAWS
AP/IFCS RMU
EVS SVS
Model Certifications & TSOs
G600 FAR Part 23 C113
Inputs/Type(s) Far Part 25 C115b
RS 232, RS 422, RS 485; ARINC 429, ARINC 708; Ethernet,
ADF (DC Sin/Cos)
C3d C117a
C4c C118
C5e C119b
C6d C129a
Outputs/Type(s) C8d C145a
RS 232, RS 422, RS 485; ARINC 429; HDG/CRS output, CDI/VDI flags
C9c C146a
C31d C147
C34e/C35d/C36e C151b
CDU Type/Size(s) C40c C153 Price
10.0 in x 6.75 in. (bezel) x 3.25 in. (depth)
C41d C154a $29,995 C52b C157
C63c C158
C66c C159
Power Required C74c C161
9-33 VDC C102 C162
C105 C163
Units/Weight (lb) C106 C165
6.4 lb C109 C166
C110a C169
C112
BCA • ISSUE: May 2009 PAGE: 199 / Version: #1
Business & Commercial Aviation | May 2009 199www.AviationWeek.com/bca
BCA • ISSUE: May 2009 PAGE: 199 / Version: #1
Integrated avIonIcs systemsManufacturer Operational Capabilities Remarks
Garmin International 1200 E. 151st St. Olathe, KS 66062www.garmin.com
FMS x PFD/MFD Integrates primary flight information, navigation, com-munication, weather, terrain and traffic data on two or three large-format displays. It is tailored to specific OEM requirements and includes features like three-axis, all-digital automatic flight control system; Synthetic Vision Pathway navigation; dual solid-state AHRS; dual integrated radio modules with WAAS certified IFR oceanic-approved GPS, VHF navigation with ILS and VHF communication with 16-watt transceivers and 8.33-kHz channel spacing; dual RVSM-compliant digital air-data computer; EICAS; Mode S transponder with TIS; Class B TAWS; XM Wx and/or digital weather radar; Garmin FliteCharts; and Garmin SafeTaxi. Sys-tem also available for King Air 200 and C90.
EFIS x CAS/TAWS
AP/IFCS x RMU
EVS SVS
Model Certifications & TSOs
G1000 FAR Part 23 x C113 x
Inputs/Type(s) Far Part 25 C115b
C3d x C117a
C4c x C118
C5e C119b
C6d x C129a
Outputs/Type(s) C8d x C145a x
C9c x C146a
C31d C147
C34e/C35d/C36e x C151b x
CDU Type/Size(s) C40c x C153 Price
Av i o n i c s
BCA • ISSUE: May 2009 PAGE: 200 / Version: #1
200 Business & Commercial Aviation | May 2009 www.AviationWeek.com/bca
Multifunction DisplaysManufacturer Avidyne FlightMax Avidyne FlightMax Chelton FlightLogic
Model EX500 EX5000 Synthetic Vision EFIS
MfD features
Dimensions (HxWxD in Inches) 4.35 x 6.25 x 10.75 8.50 x 10.70 x 3.80 6.25 x 5.5 x 4.5
Resolution (i.e. pixels) 616 x 350 800 x 600 640 x 480 (256 colors)
Boot-Up Time (Seconds) 52 52 2.3
FAR Part 23 Yes Yes Yes
FAR Part 25 No No Pending
Do 178 Software Integrity Level D D C, A
TSO C113 MFD Yes Yes Yes
TSO C63c Wx Radar Yes No Pending
TSO C110a Lightning Yes Yes Yes
interfaces
ARINC 407 Synchro I/F Yes No No
ARINC 429 GAMA I/F Yes Yes Generic
ARINC 429 Generic I/F Yes Yes Yes
ARINC TCAS I/F Yes No Yes
ARINC 561/568 INS No No No
ARINC 708/453 Wx Radar I/F Yes No Pending
ARINC 735 TCAS I/F Yes No Yes
Video No Opt. Yes
RS 232 Yes Yes Yes
Honeywell KCPB Yes Yes No
Honeywell WXPB No No No
situational awareness functions
Position Awareness
F/P Waypoints/Legs Yes Yes 40/40
Proximate Navaids Yes Yes Yes
Proximates Airports Yes Yes Yes
Proximate Intersections Yes Yes Yes
Special-Use Airspace Yes Yes Yes
Weather Awareness
Wx: Onboard Radar Yes No Pending
Wx: Onbard Lightning Sensor Yes Yes Yes
Wx: Air/Ground FIS-B Downloads No No Pending
Wx: Air/Ground Other Downloads Yes Yes No
Wx: Satcom Data Link Low Rate Yes Yes Pending
Wx: Satcom Data Link High Rate Yes Yes No
Traffic Awareness
TIS-B via Mode S Data Link Yes Yes Yes
TAS: TSO C147 Yes Yes Yes
TCAS I: TSO C118 Yes Yes Yes
TCAS II: TSO C119 No No Yes
Terrain Awareness
Basic Topography Yes Yes Yes
Basic Cartography Yes Yes Yes
TAWS: TSO C151 Class B Opt. Opt. Yes
TAWS: TSO C151 Class A No No Yes
price $11,995* $13,995 $70,000*
Remarks
Price includes radar and traffic interface and integrated data link transceiver. Non-radar version, $8,995. Available options: Cmax, TCAS-1 and EGPWS. *BCA esti-mate.
Includes integrated data link. Available options: CMax, TCAS-1, EGPWS and radar.
HUD symbology; 3-D modeling; Class A,B,C TAWS w/threat diff.; integral GPS/WAAS; Jeppesen Nav-Data; on-screen full-function FMS; inertial AHRS; unusual attitude recovery mode. *One screen.
BCA • ISSUE: May 2009 PAGE: 201 / Version: #1
Business & Commercial Aviation | May 2009 201www.AviationWeek.com/bca
Multifunction DisplaysManufacturer Garmin International Honeywell Universal Avionics
Model GMX 200 MFRD/80-5204 MFD-640
MfD features
Dimensions (HxWxD in Inches) 5.0 x 6.25 x 8.0 6.242 x 4.815 x 8.378 5.18 x 6.68 x 7.1*
Resolution (i.e. pixels) 640 x 480 1024 x 768 640 x 480
Boot-Up Time (Seconds) 3.5 10 15
FAR Part 23 Y Yes Yes
FAR Part 25 Y Yes Yes
Do 178 Software Integrity Level C, D B C
TSO C113 MFD Yes Yes Yes
TSO C63c Wx Radar Yes Yes Yes
TSO C110a Lightning Yes Yes Yes
interfaces
ARINC 407 Synchro I/F No No Yes
ARINC 429 GAMA I/F Pending Yes Yes
ARINC 429 Generic I/F Yes Yes Yes
ARINC TCAS I/F Yes No Yes
ARINC 561/568 INS No No No**
ARINC 708/453 Wx Radar I/F Yes Yes Yes
ARINC 735 TCAS I/F No Yes Yes
Video Pending No Yes
RS 232 Yes Yes No
Honeywell KCPB No Yes Yes
Honeywell WXPB No Yes Yes
situational awareness functions
Position Awareness
F/P Waypoints/Legs Yes Yes Yes
Proximate Navaids Yes Yes Yes
Proximates Airports Yes Yes Yes
Proximate Intersections Yes Yes No
Special-Use Airspace Yes No No
Weather Awareness
Wx: Onboard Radar Yes Yes Yes
Wx: Onbard Lightning Sensor Yes Yes Yes
Wx: Air/Ground FIS-B Downloads Yes No No
Wx: Air/Ground Other Downloads Yes No Yes
Wx: Satcom Data Link Low Rate NA No NA
Wx: Satcom Data Link High Rate NA No NA
Traffic Awareness
TIS-B via Mode S Data Link Yes No No
TAS: TSO C147 Yes No No
TCAS I: TSO C118 Yes Yes Yes
TCAS II: TSO C119 No Yes Yes
Terrain Awareness
Basic Topography Yes Yes NA
Basic Cartography Yes Yes NA
TAWS: TSO C151 Class B Yes No Yes
TAWS: TSO C151 Class A No No Yes
price $8,995 $44,595 $41,500
Remarks
$10,995 Traffic Model; $12,995 Radar Model; $14,995 Traffic and Radar Model; Chartview, SafeTaxi and Flite Chart std.
Combines weather radar, traffic, terrain, navigation maps and other data into a single display unit.
*6.4-inch display; C105 and C119b interfaces; compatible with legacy radar systems, supports Universal TAWS with 3-D video display. **Displays ARINC 419 INS from LTD-92.