NSN: 5841-01-594-5244
Price | Condition | Status | Part Info | |
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REQUEST | NEW OUTRIGHT | REQUEST |
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Price | Condition | Status | Part Info | |
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REQUEST | NEW OUTRIGHT | REQUEST |
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Price | Condition | Status | Part Info | |
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REQUEST | SV OUTRIGHT | REQUEST |
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NSN: 5841-01-552-1997
Size: | 4.98"W x 7.70"H x 15.16"D; 1/2 ATR short per ARINC 404A | Weight: | 17.20 lbs. |
Form factor: | 4 MCU ARINC 600 | Primary Power: | +28VDC (22-30VDC), 70 watts max |
Reference Power: | 26 VAC synchro reference power (ARINC 413A) | Temp Range: | -55 to 70C (operating) |
TSO: | C119a (-0101,0201); C119b (-1111,-1211) | Environmental: | A2F2/B/A/YNB/E1/XXXXXABZABATAXXX (-0101,-1111) A2F2/B/A/YNB/E1/XXXXXABZABATAZZE3XX (-0201,-1211) |
Surveillance: | 45 aircraft | Cooling: | Convection |
Part Number | TCAS II Processor Description: |
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066-01146-0101 | Basic unit without ext. environ. protection, w/o secondary att/hdg input (see details above) |
066-01146-0201 | With ext. environ. protection but w/o secondary att/hdg input (see details above) |
066-01146-1111 | ACAS II unit without ext. environ. protection, w/o secondary att/hdg input (see details above) |
066-01146-1211 | ACAS II unit with ext. environ. protection, with secondary att/hdg input (see details above) |
NSN: 5841-01-552-1997
Price | Condition | Status |
---|---|---|
$14,250.00 | SV OUTRIGHT | 2 IN STOCK |
NSN: 5841-01-594-5244
Price | Condition | Status |
---|---|---|
REQUEST | NEW OUTRIGHT | REQUEST |
Price | Condition | Status |
---|---|---|
REQUEST | NEW OUTRIGHT | REQUEST |
Price | Condition | Status |
---|---|---|
REQUEST | SV OUTRIGHT | REQUEST |
Click on a question below to see the answer. If you have a question about this model that is not answered below, please contact questions@seaerospace.com
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TCAS II is a system used for detecting and tracking aircraft in the area of an aircraft. TCAS interrogates transponders in other aircraft and analyzes the replies to determine range, bearing, and relative altitude (if reporting) of the intruder aircraft. When the TCAS II processor determines that a potential collision hazard exists, it will issue visual and audio advisories to the pilot/copilot for appropriate vertical avoidance maneuvers. TCAS is not able to detect aircraft without an operating ATCRBS transponder (operating in Mode A and C) or a Mode S transponder. |
TCAS II utilizes two types of cockpit displays, Resolution Advisory (RA) and Traffic Advisory (TA) display. The RA is incorporated into the vertical speed indicator (VSI). With illuminating red and green arcs around the dial, the VSI displays the required rate, or limitation of climb or descent, to avoid a collision. The TA display shows the intruding aircraft’s relative position and altitude with a trend arrow to indicate if it is climbing or descending greater than 500 feet per minute. The TA display may be presented on compatible weather radar indicator or MFD, dedicated TCAS display or a TA/VSI display. The TA display uses symbols and colors to identify the relative threat of each intruder. Supplementing the displays, TCAS II provides appropriate synthesized voice announcements. |
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