AFI4700 Product Specifications - Astronautics

AFI4700 Product Specifications

The Fastest Way to Upgrade. The Astronautics AFI 4700 RoadRunner Electronic Flight Instrument (EFI) is a form-fit-function EFI that is designed as a replacement for Attitude Director Indicator and Horizontal Situation Indicator primary flight instruments.

The RoadRunner EFI offers enhanced safety, reduced operating costs, and minimized installation downtime, and is capable of displaying terrain awareness, traffic, weather, and synthetic vision.

Cost Effective. Eliminates unplanned and expensive repair of primary flight displays.

Perfect Fit. Directly replaces ADI/HSI electromechanicals or outdated CRT EFIS.

Minimal Downtime. Installs in two days with no panel modifications.

Enhanced Safety. Increases operational capability by enabling LPV approaches.

Next-Gen Ready. Approved for single-pilot IFR.

Future Proof. Planned field-loadable software upgrades including SVS and HTAWS.

Intuitive Control. Provides familiar, easy-to-use controls.

Weight Reduction. 16lbs. installed, a weight reduction of 20lbs.

AFI4700 RoadRunner EFI Product Specifications

I/O SPECIFICATIONS

DimensionsElectronics Unit 5.0”H x 4.6”W x 6.9”DDisplay Head 9.7”H x 5.2”W x 1.5”D

Weight 8.1lbs

Display 4” x 7” AMLCD with a viewable are of 4.1” x 6.8”

Display Resolution 480 x 800

Luminance >800 cd.m2

GENERAL SPECIFICATIONS

ARINC 429 Inputs 8

ARINC 429 Outputs 4

3-wire Synchro/Resolver 6Inputs (XYZ)

Synchro/Resolver Reference 5(26VAC or 115VAC) Inputs

ARINC 568 DME Inputs 1

4-wire Resolver Outputs 1

Low Range Analog Inputs 6

High Range Analog Inputs 8

RS-422 (crosslink) Inputs 1

RS-422 (crosslink) Outputs 1

RS-232 Inputs 2

RS-232 Outputs 2

Ethernet Ports 1

Operating Temperature -40°C (short term) -20°C (long term) to 55°C

Storage Temperature -55°C to +85°C

Input Voltage +18vDC to +32vDC

Normal Operating Power 30W

Maximum Current 1.3 Amps @28vDC (heater not enabled)

2.4 Amps @28vDC (heater enabled)

OPERATIONAL SPECIFICATIONS

FAA Technical Standard C209, C3e, C165aOrders (TSO)

Software RTCA DO-178C Level A

Firmware RTCA DO-254 Level A

CERTIFICATION SPECIFICATIONS

DISPLAYS & COCKPIT INTEGRATION

AFI4700 RoadRunner EFI Product Specifications

Sensor Quantity Interface Equipment

Vertical Gyro 1 or 2 26VAC ARINC-407• BF Goodrich VG-208• Tarsyn-333• Tarsyn-H

Directional Gyro 1 or 2 26VAC ARINC-407 • Honeywell C-14A• Tarsyn-333

AHRS 1 or 2 ARINC-429

• Litef LCR-92/93/100• Collins AHS-3000• Genesys ADAHRS• Garmin GRS-77

Flight Director 1 Analog• Honeywell FZ-702• Honeywell SPZ-7600• Astronautics CP-2036A

Radar Altimeter 1 or 2Analog ARINC-552

ARINC-429

• Honeywell AA-300• Honeywell RX-220• Honeywell APN-209• Collins ALT-55A/55B• Collins ALT-1000• Bendix/King KRA-405B• Collins ALT-4000• FreeFlight RA-4000

Traffic 1 ARINC-429• BF Goodrich TCAS-791• Avidyne TAS-600/605A/615A/620A• Garmin GTX-8X5

Lightning Detection 1 ARINC-429• L-3 Stormscope WX-1000E• Avidyne TWX670• Garmin

Weather RADAR 1 ARINC-429 and ARINC-453• Bendix/King RDR-2000• Honeywell RT-1401B• Garmin GWX-70

DME 1ARINC-568

ARINC-429

• Bendix/King KMD-706/A• Cobham CMD-451• Collins DME-442

NAV (VOR/ILS) 1 or 2

Analog

ARINC-429

• Bendix/King KX-155A/165A (requires KN-40)• Bendix/King KN-53 (requires KN-40)• Collins VIR-32• Bendix/King KNR-630• Bendix/King KNR-634A• Collins VIR-432• Cobham CVN-251• Garmin GNS-4XX/5XX

NAV/GPS/FMS 1 or 2 ARINC-429

• Garmin GNS-430(W)/530(W)• Garmin GTN-650/750• Avidyne IFD-4XX/5XX• Universal UNS-1C

1 Analog

• Avidyne AMX240• Bendix/King KMR-675• PS Engineering MB-10• PS Engineering PMA-450B• PS Engineering PMA-6000B/7000/8000• Becker Avionics MKR3300

ADF

1 or 21 or 2

1 or 2

26VAC ARINC-407DC SIN/COS

ARINC-429

• Collins ADF-60A/B• Bendix/King KR-87• Bendix/King KFD-806• Collins ADF-462/A/B• Cobham DFS-43A

DF 1 ARINC-429 • Cobham DF-931

HTAWS 1 ARINC-429 and ARINC-453 • Honeywell MX-XXII

SUPPORTED EQUIPMENT

Contact [email protected] +1.414.449.4000 roadrunner.astronautics.com dealers.astronautics.com

DISPLAYS & COCKPIT INTEGRATION