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


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


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


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



HF transceiVersManufacturer

Model Frequency Range Xmit Power (W)

Units/Weight (lb) PriceRemarks

TSO Channels Size or Form Factor Power Required


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


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


TSO Slave Rate Display Case Power Required


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


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



autoMatic direction Finders

ManufacturerModel Frequencies

Nav Outputs

Units/Weight (lb) PriceRemarksFrequency Storage

TSO Size or Form Factor Power RequiredDisplay


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


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


TSO Slave Rate Display Case Power Required


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


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



reMote-Mount naV receiVersManufacturer

Model Channel DisplayNav Outputs


TSO Channel Size or Form Factor Power Required


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


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


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


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




distance MeasurinG equiPMent

ManufacturerModel

Channel Display

Nav Outputs Units/Weight (lb) PriceRemarks

TSO Power Outputs (peak W)

Size or Form Factor Power Required


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


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


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



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


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


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



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


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


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



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


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°


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.


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.


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



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


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


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


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



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


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



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.


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


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.


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


manual and auto. modes

14 or 28 VDC

Av i o n i c s



inteGrated FliGHt control systeMs

Manufacturer ModelAir Data Autopilot

Power

Weight Price

RemarksAP Only AP OnlyAttitude Sensors Flight Director IFCS IFCS


GFC 700

GDC 74 (B) DADC combined

28 VDC

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


Primus 1000

micro DADC digital AHRS

or IRS IC-6000

28 VDC


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



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


or IRSIC-800

28 VDC


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


or IRSFZ-800

28 VDC



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


Primus Epic

air data module and micro IRS

integrated modular avionics

unit

28 VDC



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.



Primus Epic Fly-by-Wire

SystemSee remarks

Integrates with Primus Epic System. Scalable architecture, performance and envelope protection. ARJ-21


APS-65

AHC-3000 APS-65

28 VDC



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



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



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


Garmin, Chelton, Honeywell, Sandel, Sagem, Universal,


3.1 x 7.25 x 11.77.2


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


Garmin, Chelton, Honeywell, Sandel,Sagem, Universal,


3.1 x 7.25 x 11.77.2


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






TSO Weight (lb)


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






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



cocKPit Voice recorders (cVr)/FliGHt data recorders (Fdr)

Manufacturer

Type Recording Medium Size PriceRemarksModel

Duration Weight (lb) Power RequiredTSO


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


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




Manufacturer



L-3 CommunicationsAviation Recorders6000 Fruitville Rd.Sarasota, FL 34232(941) 371-0811www.L-3ar.com


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


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


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




Manufacturer



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



Heads uP disPlaysManufacturer Model Inputs & Outputs


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







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,


7000CE:$8,995,

U.S. & No. Am.

databases;$9,495,


*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







FactorPower

Required


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







FactorPower

Required


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



electronic FliGHt BaGs



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







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







Required


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



enHanced Vision systeMs (eVs)Manufacturer

Model DisplayInputs Outputs


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



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



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


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.


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.






s = Scratchpad




C = 115 VAC

Av i o n i c s



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


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.


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.






s = Scratchpad




C = 115 VAC



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


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. — — —


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






s = Scratchpad




C = 115 VAC

Av i o n i c s



flight management systemsmanufacturer Universal

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


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.


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.






s = Scratchpad




C = 115 VAC



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


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


Entegra Release 9 FAR Part 23 X C113 X


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


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




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


Chelton Flight Systems EFIS FAR Part 23 C113


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


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


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


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


G600 FAR Part 23 C113


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


10.0 in x 6.75 in. (bezel) x 3.25 in. (depth)

C41d C154a $29,995 C52b C157

C63c C158

C66c C159


9-33 VDC C102 C162

C105 C163

Units/Weight (lb) C106 C165

6.4 lb C109 C166

C110a C169

C112





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


G1000 FAR Part 23 x C113 x


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



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.



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.

vhf panel-mount transcei vers - aviation weekawin.aviationweek.com/portals/awin/pdfs/bca... · vhf...

Documents