NSN 6610-01-432-8458 · NIIN 014328458 · FSC 6610
NO DASHES 6610014328458
In Stock
COMPUTER,AIR DATA
Flight Instruments
Application: F-15S
Technical characteristics
16 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ACUQ | ALTERNATING CURRENT VOLTAGE RATING IN VOLTS | 115.0 |
| ACUR | DIRECT CURRENT VOLTAGE RATING IN VOLTS | 26.0 |
| AGAV | END ITEM IDENTIFICATION | F-15S |
| AJAF | UNPACKAGED UNIT LENGTH | INCHES NOMINAL 9.50 |
| AJAG | UNPACKAGED UNIT WIDTH | INCHES NOMINAL 6.20 |
| AJAH | UNPACKAGED UNIT HEIGHT | INCHES NOMINAL 6.50 |
| AWZJ | POWER SOURCE | EXTERNAL |
| AXQH | INPUT INTELLIGENCE TYPE | AIR PRESSURE AND ANGLE OF ATTACK AND AIR TEMPERATURE AND ALTITUDE, GENERAL DATA |
| AXQJ | INTELLIGENCE INPUT METHOD | AIR OR ELECTRICAL |
| AXQK | OUTPUT INTELLIGENCE TYPE | AIR DATA |
| FAAZ | PHASE | SINGLE |
| FEAT | SPECIAL FEATURES | THERE ARE 2 DIFFERENT MECHANICAL MOUNTS, 1 USED IN THE EAIC LOCATION AND 1 USED IN THE ADC LOCATION. |
| FREQ | FREQUENCY IN HERTZ | 400.0 |
| FTLD | FUNCTIONAL DESCRIPTION | PROCESSOR ACCEPTS INPUTS FROM AIRCRAFT FREESTREAM PITOT-STATIC PRESSURE SYSTEM, ANGLE OF ATTACK SENSORS, AIRCRAFT TOTAL TEMPERATURE SENSORS, ENGINE AIR INLET DUCT PITOT-STATIC PRESSURE SYSTEM AND THE ALTIMETER BAROMETRIC SETTING. CORRECTED INPUTS ARE USED TO 1) COMPUTE ACCURATE AIR DATA FOR PRIMARY FLIGHT INSTRUMENTS 2) GENERATE COMMANDS NECESSARY TO CONTROL THE VARIABLE ENGINE INLET GEOMETRY, 3) PROVIDE THE AFCS WITH PITOT PRESSURE, STATIC PRESSURE, AND IMPACT PRESSURE. |
| SUPP | SUPPLEMENTARY FEATURES | TECH CHARACTERISTICS: MIL-STD-1750A PROCESSOR, CONTAINS 1553 BUS, BUILT-IN-TEST/3 EXTERNAL FAIL INDICATORS, REQUIRES NO COOLING AIR, PROVIDES PRESSURE SIGNAL OUTPUTS, PROVIDES AIR DATA TO OTHER AIRCRAFT SYSTEMS. |
| TMDN | TYPE/MODEL DESIGNATION | CPU194/A |