Catalog item

COMPUTER,AIR DATA

6610FSC
01NCB code
432-8458Item number
NIIN 01-432-8458
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Unit price
$26,000.00
Unit of issue
EA
Source of supply
F2U
DEMIL code
D

Identification

Item name code
30742
PINC
0030742
Criticality code
X
II
0
DEMIL code
D
DEMIL integrity code
1
NIIN assigned
17-JUN-96
Precious metals indicator
A
ADP equipment code
0
Hazardous material indicator
N
Schedule B export code
9014900000

Management

Effective date
01-OCT-2017
Major organizational entity
DF
Acquisition advice code
P
Source of supply
F2U
Unit of issue
EA
Unit of measure quantity
0.0000
Unit price
$26,000.00
Quantity per unit pack
1
Controlled inventory item code
7
Shelf-life code
0
Recoverability code
T
Management control
VUNXZ-E
Net price
$0.00
USC
F

Part numbers

Part numberCAGECAGE statusRNCCRNVCDocument availability codeRNAACRNSC
2118952-464547
HONEYWELL INTERNATIONAL, INC
A325ZZ
2118952-364547
HONEYWELL INTERNATIONAL, INC
A322ZZ
2118952-164547
HONEYWELL INTERNATIONAL, INC
A592ZZB
CPU-194/A80058
JOINT ELECTRONICS TYPE DESIGNATION SYSTEM
A512ZZ
68-870241-20188277
THE BOEING COMPANY
A722ZZ

Characteristics

ALTERNATING CURRENT VOLTAGE RATING IN VOLTS115.0
DIRECT CURRENT VOLTAGE RATING IN VOLTS26.0
END ITEM IDENTIFICATIONF-15S
UNPACKAGED UNIT LENGTHINCHES NOMINAL 9.50
UNPACKAGED UNIT WIDTHINCHES NOMINAL 6.20
UNPACKAGED UNIT HEIGHTINCHES NOMINAL 6.50
POWER SOURCEEXTERNAL
INPUT INTELLIGENCE TYPEAIR PRESSURE AND ANGLE OF ATTACK AND AIR TEMPERATURE AND ALTITUDE, GENERAL DATA
INTELLIGENCE INPUT METHODAIR OR ELECTRICAL
OUTPUT INTELLIGENCE TYPEAIR DATA
PHASESINGLE
SPECIAL FEATURESTHERE ARE 2 DIFFERENT MECHANICAL MOUNTS, 1 USED IN THE EAIC LOCATION AND 1 USED IN THE ADC LOCATION.
FREQUENCY IN HERTZ400.0
FUNCTIONAL DESCRIPTIONPROCESSOR 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.
SUPPLEMENTARY FEATURESTECH 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.
TYPE/MODEL DESIGNATIONCPU194/A

MOE rules

MOE ruleMOE CDAMCAMSCDate assignedIMCPICAPICA LOAAuth collab
YS01YS01-FEB-15YS81YS
FMSGDF0001-JUN-96ETG99TU

Service data

Air Force

Fund
VU
Budget
N
MMAC
XZ
PVC
E
ERRC
T

Freight

ACTY CD
TK

Related items

Standardization

Item standardization code
3
Orig stdzn dec
TU
Dt stdzn dec
22-JUL-1998
NIIN status code
0

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