WGU-28B

Gui Guidance And Control Section

NSN 1427-01-285-9800

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

012859800

Detail Specifications

End Application:

Agm-65d missile

Functional Description:

2provides sensing and signal proceessing functions; houses the guidance subsystem and contains the digital aut0pilo (dap) with flight control sensors and electrical power conversion electronics to accomodate the pneumatic actuation system(pas)

General Description:

12 in. Diameter; 98 in. Long; 28.5 in wing and control surface span; weight 108.0 lbs.

NSN:

1427-01-285-9800

Item Name:

Guidance And Control Section,gui

Cage Code:

07878

Manufacturer Part Numbers

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

3647115-101

Cage Code:

82577

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

3647115-101

Cage Code:

04164

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

1427-RY08

Cage Code:

99999

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

62090

FIIG:

A23900

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:

Packaging & Shipping

Est. Pack Size

Est. Pack Weight

Est. Item Weight

Est. Item Dim.

Pack Size:

25.0 X 25.0 X 42.5

Paclk Weight:

159.0000lbs

Item Weight:

88.0000lbs

Item Dim:

030001200120

OPI

SPI No.

SPI Rev.

SPC Mkg.

LVL A

LVL B

OPI:

SPI No.:

F010200694

SPI Rev.:

SPC Mkg:

LVL_A:

LVL_B:

Freight Classification

NMFC

UFC

LTL

LCL

WCC

TCC

SHC

ACC

NMFC:

162812

UFC:

73210

LTL:

85.0

LCL:

WCC:

778

TCC:

SHC:

ACC:

Equipment for Aircraft

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Gui Guidance And Control Section"

An item which includes the components necessary to effect guidance and control of a guided missile in flight. It forms a portion of the outer case of the missile.