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Predicted MTBF of 5,000 hours ARW / 7000 hours AIC
15-minute MTTR
Built-In Test (BIT)
95% probability of fault detection
Power-on, continuous and commanded BIT
Height |
7.125 inches |
Width |
5.75 inches |
Depth |
822-2538-001: 8.0 inches 822-2654-010: 6.5 inches |
Weight |
10.9 lbs maximum |
Operating Temperatures |
-40° C to +55° C (Intermittent to +71 C) |
Cooling |
Forced convection with internal fan |
Input Power: 28 V dc, 70 W (maximum) with heater or fan
Dual IEEE 802.3 Ethernet (10/100 BaseT selectable)
MIL-STD-1553B: dual/dual
ARINC 429: 12 input, 6 output (low/high speed)
RS-232: 2 input, 2 output
Discrete I/O: 17 input, 8 output (ground open)
ARINC-743A-1 GPS time mark input
Keyboard Lighting: 5 V ac, 5 V dc or 28 V dc
Shock |
MIL-STD-810 Method 516.5 Procedure I, V, VI, 20 g/11 ms |
Acceleration |
MIL-STD-810 Method 513.5 Procedure I, II |
Vibration |
MIL-STD-810 Method 514.5 (Helicopter) |
Undamped Resonance |
MIL-STD-810 Method 514.5 Procedure I, Category 14 |
Continuous Vibration |
MIL-STD-810 Method 514.5 |
Gunfire |
MIL-STD-810 Method 519.5 |
Sand and Dust |
MIL-STD-810 Method 510.4 |
Fungus |
MIL-STD-810, Method 508.5 |
Salt Atmosphere |
MIL-STD-810, Method 509.4 |
Explosive Atmosphere |
MIL-STD-810, Method 511.4 |
Solar Radiation |
MIL-STD-810, Method 505.4 |
Rain |
MIL-STD-810, Method 506.4, Procedure III (drip test) |
Temperature, Humidity, Altitude |
MIL-STD-810, Method 520.2 Procedures I, II, III. Max altitude 6000 meters |
Temperature Shock |
MIL-STD-810, Method 503.4 |
High Temperature Storage |
MIL-STD-810, Method 501.4 Procedure I, 85°C |
Low Temperature Storage |
MIL-STD-810, Method 502.4 Procedure I, -55°C |
Predicted MTBF of 5,000 hours ARW / 7000 hours AIC
15-minute MTTR
Built-In Test (BIT)
95% probability of fault detection
Power-on, continuous and commanded BIT
Height |
7.125 inches |
Width |
5.75 inches |
Depth |
822-2538-001: 8.0 inches 822-2654-010: 6.5 inches |
Weight |
10.9 lbs maximum |
Operating Temperatures |
-40° C to +55° C (Intermittent to +71 C) |
Cooling |
Forced convection with internal fan |
Input Power: 28 V dc, 70 W (maximum) with heater or fan
Dual IEEE 802.3 Ethernet (10/100 BaseT selectable)
MIL-STD-1553B: dual/dual
ARINC 429: 12 input, 6 output (low/high speed)
RS-232: 2 input, 2 output
Discrete I/O: 17 input, 8 output (ground open)
ARINC-743A-1 GPS time mark input
Keyboard Lighting: 5 V ac, 5 V dc or 28 V dc
Shock |
MIL-STD-810 Method 516.5 Procedure I, V, VI, 20 g/11 ms |
Acceleration |
MIL-STD-810 Method 513.5 Procedure I, II |
Vibration |
MIL-STD-810 Method 514.5 (Helicopter) |
Undamped Resonance |
MIL-STD-810 Method 514.5 Procedure I, Category 14 |
Continuous Vibration |
MIL-STD-810 Method 514.5 |
Gunfire |
MIL-STD-810 Method 519.5 |
Sand and Dust |
MIL-STD-810 Method 510.4 |
Fungus |
MIL-STD-810, Method 508.5 |
Salt Atmosphere |
MIL-STD-810, Method 509.4 |
Explosive Atmosphere |
MIL-STD-810, Method 511.4 |
Solar Radiation |
MIL-STD-810, Method 505.4 |
Rain |
MIL-STD-810, Method 506.4, Procedure III (drip test) |
Temperature, Humidity, Altitude |
MIL-STD-810, Method 520.2 Procedures I, II, III. Max altitude 6000 meters |
Temperature Shock |
MIL-STD-810, Method 503.4 |
High Temperature Storage |
MIL-STD-810, Method 501.4 Procedure I, 85°C |
Low Temperature Storage |
MIL-STD-810, Method 502.4 Procedure I, -55°C |