COMPUTER,AIR DATA

Name: COMPUTER,AIR DATA
Brand: Atlas Air Supply
SKU: 6610014328458
Availability: LimitedAvailability

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.

Technical characteristics from the federal item record
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

5 manufacturer part numbers on file for this NSN — each shown against the CAGE code it belongs to.