12402-1AB1

Attitude-headi Gyroscope Control

NSN 6615-00-224-7411

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

002247411

Product Technical Spec.

Maximum Voltage Rating In Volts:

26.0 ac

Power Source:

External

Mounting Method:

Flush panel

Terminal Type And Quantity:

3 pin

Maximumlength:

8.358 inches

Maximumwidth:

3.438 inches

Maximumheight:

3.438 inches

Intelligence Data Handling Capability:

Gyroscope-altitude data transmitting automatic and pitch-roll signal data transmitting automatic

Indication Method:

Transmitting dial

Phase:

Three

Frequency In Hertz:

400.0

Reference Number Differentiating Characteristics:

As differentiated by the with ivory-fluorescent dial finish

NSN:

6615-00-224-7411

Item Name:

Computer,yaw And Lateral Augmentation

Cage Code:

55972

Cross Referenced Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

12402-1AB1

Cage Code:

19315

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

37254

FIIG:

A31700

Concept No.:

App. Key:

Cond. Code:

Status:

Part Materials

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators

HMIC

PMIC

ESD/EMI

ENAC

MMAC

CRITL

HMIC:

PMIC:

ESD:

MMAC:

CRITL:

Freight Classification

NMFC

UFC

LTL

LCL

WCC

TCC

SHC

ACC

NMFC:

061480

UFC:

34500

LTL:

77.5

LCL:

77.5

WCC:

658

TCC:

SHC:

ACC:

Instruments/Radio

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Yaw And Lateral Augmentation Computer"

A control designed for use with automatic pilots and/or remote attitude indicators consisting primarily of a gyroscope which provides signals for controlling an aircraft about its lateral and longitudinal axis and/or signals for providing a visual presentation of attitude to the pilot.