Part Number 17B1U6001-571

Flight Control Processor

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Part Number
DEMIL
Shelf Life
UOM
NIIN
Part:
17b1u6001-571
Demil:
No
Shelf Life:
UOM:
NIIN:
014649820

Part Information
Mfg name computer, flight control, operating temp -40 to 131 degrees f; altitude up to 50k ft; memory 314k; basicprocessor unit without software is p/n103e4151g103; p/n 17b1u6001-571 is thebasic unit w/software version 6.1 installeld

NSN
National Stock Number:
6615-01-464-9820 6615014649820
TXT
Description:
Flight Control Processor
INC
INC
Item Name Code:
53048
MRC:
The direct current voltage for which the item is rated,expressed in volts.ACUR
Direct Current Voltage Rating In Volts:
28.0
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
C-17 acft
MRC:
A measurement of the longest dimension of an item unencumbered by packaging or packing,in distinction from width.AJAF
Unpackaged Unit Length:
16.30 inches
MRC:
A measurement taken at right angles to the length of an item unencumbered by packaging or packing,in distinction from thickness.AJAG
Unpackaged Unit Width:
10.10 inches
MRC:
A measurement from the bottom to the top of an item unencumbered by packaging or packing,in distinction from depth.AJAH
Unpackaged Unit Height:
7.60 inches
MRC:
The source of power which provides the energy required for the operation of the item.AWZJ
Power Source:
External
MRC:
The means used to input the intelligence.AXQJ
Intelligence Input Method:
Electrical
MRC:
Those features,not otherwise specified,which may be required for proper functioning of the item.CBBL
Features Provided:
Electrostatic sensitive
MRC:
The master requirement codes of those requirements which are technically critical by reason of tolerance,fit,performance,or other characteristics which affect identification of the item.CRTL
Criticality Code Justification:
Cbbl
MRC:
Describes the capabilities,intended use,and/or purpose for which the item is provided.FTLD
Functional Description:
Used to compute primary flight control, stability and control augmentation and automatic flight control functions; performs all calculations necessary to implement functions of the stability and control augmentation system, autopilot, autothrottle, flight director, heads up display control and ground proximity warning system

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