EFI-650
LCD Plug-and-Play Solution
Legacy ED-800 CRT Displays ATR42/ 72, Dash 8 and others
Key Benefits
- Form, fit, and function replacement for legacy ED-800 CRT displays
- Fully interchangeable with legacy displays
- True plug-and-play with existing CRT units
- Instant conversion – install on overnights or at gate
- No changes to cockpit panels or wiring
- No flight crew or maintenance retraining
- Captures LCD technology benefits – higher MTBF at a lower cost of ownership over CRT displays
- Advanced THOMAS ADA 2.0™ Adaptive Display Architecture adds functionality and capacity to support emerging requirements
- Eliminates threat of CRT obsolescence
Practical Innovation
L3’s EFI-650 Electronic Flight Instrument System (EFIS) display upgrade provides a plug-and-play replacement for the Cathode Ray Tube (CRT) displays installed on a large number of business and regional aircraft. The EFI-650 uses the latest-generation Active Matrix Liquid Crystal Display (AMLCD) technology and solid-state LED backlighting to eliminate the maintenance cost and obsolescence concerns associated with legacy CRTs.
The EFI-650 displays provide higher reliability, reduced weight and lower life-cycle cost.
Please Contact Us for further information.
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| OPTICAL PERFORMANCE | |
| Viewable Area | 3.4” (h) x 4.53” (w) |
| Addressability | 6-bits per color |
| Resolution | 640 x 480 (VGA) |
| Color | 262,144 possible; Video interface supports palette of 13 colors + black |
| Luminance | 0.1 fL to ~150 fL |
| Viewing Angles | ±45° horizontal; +45°, -23° vertical |
| High Amb. Contrast Ratio | >3:1 across viewing envelope |
| PHYSICAL DESCRIPTION | |
| Dimensions (H x W x D) | w/inclinometer: 5.1” x 6.1” x 11.0” w/out inclinometer: 5.1” x 6.1” x 10.5 |
| Weight | Approx. 5 lb. |
| Cooling | Passive convective |
| Heating | Integrated heater |
| Primary Power | 28VDC per DO-160G, Sec. 16, Cat. B; Operate thru 200 ms power interrupt |
| Power Consumption | <20 Watts <35 Watts w/heater on |
| Bezel Configuration | Photosensors for automatic dimming in response to ambient light |
| FUNCTIONAL DESCRIPTION | |
| Video Interfaces | Analog (stroke and raster) video |
| Video Out | Analog (stroke and raster) |
| Signal Interfaces | Analog and discrete |
| Other (i.e. inclinometer) | Inclinometer is dimmable under control of aircraft lighting bus |
| ENVIRONMENTAL PERFORMANCE (DO-160G) | |
| Temperature & Altitude | Sec. 4, Cat. A2 |
| Low Operating Temp: | Sec. 4.5.2, -20 °C |
| Low Short-Term Operating Temp | Sec. 4.5.1, -40 °C |
| High Short-Term Operating Temp | Sec. 4.5.3, +70 °C |
| High Operating Temp | Sec. 4.5.4, +70 °C |
| Loss of Cooling Test | Sec. 4.5.5, 240 min @ 40 °C |
| Ground Survival Low Temp | Sec. 4.5.1, -55 °C |
| Ground Survival High Temp | Sec. 4.5.3, +85 °C |
| Altitude | Sec. 4.6.1, 55,000 ft. |
| Decompression Test | Sec. 4.6.2, 55,000 ft. |
| Overpressure Test | Sec. 4.6.3, -15,000 ft. |
| Temperature Variation | Sec. 5, Cat. C |
| Humidity | Sec. 6, Cat. A |
| Operational Shocks & Crash Safety | Sec. 7, Cat. B |
| Vibration | Sec. 8, Cat. S(M), R(BB1) |
| Explosion Proofness | Sec. 9, Cat. X |
| Waterproofness | Sec. 10, Cat. W |
| Fluids Susceptibility | Sec. 11, Cat. F |
| Sand and Dust | Sec. 12, Cat. X |
| Fungus Resistance | Sec. 13, Cat. X |
| Salt Fog | Sec. 14, Cat. X |
| Magnetic Effect | Sec. 15, Cat. Z |
| Power Input: | Sec. 16, Cat. BRX |
| Voltage Spike | Sec. 17, Cat. A |
| Aud. Freq. Conducted Susceptibility Power Inputs | Sec. 18, Cat. Z |
| Induced Signal Susceptibility | Sec. 19, Cat. ZC/CC |
| Radio Frequency Susceptibility | Sec. 20, Cat. MD |
| Emission of Radio Freq. Energy | Sec. 21, Cat. M |
| Lightning Induced Transient Susceptibility | Sec. 22
Power Bundle: A4G3L3 Signal Wiring: A3J3L3 |
| Lightning Direct Effects | Sec. 23, Cat. X |
| Icing | Sec. 24, Cat. X |
| Electrostatic Discharge | Sec. 25, Cat. A |
| Fire Flammability | Sec. 26, Cat. C |