5149T71P02

Aircraft Gas Turbine Fan Shroud

NSN 2840-01-388-7482

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

013887482

Product Features

Shroud, fan vane-stage 3

Product Technical Spec.

End Application:

Engine model f404

Part Name Assigned By Controlling Agency:

Shroud, fan vane

Stage Number:

NSN:

2840-01-388-7482

Item Name:

Shroud,fan,aircraft Gas Turbine

Cage Code:

51992

Cross Referenced Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

5049T71P02

Cage Code:

99207

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

5049T71P02

Cage Code:

8U485

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

5049T71P02

Cage Code:

28884

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

5049T71P02

Cage Code:

51992

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

10183341

Cage Code:

A486G

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

52546

FIIG:

A10700

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:

Paclk Weight:

0.2000lbs

Item Weight:

Item Dim:

OPI

SPI No.

SPI Rev.

SPC Mkg.

LVL A

LVL B

OPI:

SPI No.:

SPI Rev.:

SPC Mkg:

LVL_A:

LVL_B:

Freight Classification

NMFC

UFC

LTL

LCL

WCC

TCC

SHC

ACC

NMFC:

133300

UFC:

63220

LTL:

RATING VARIABLE

LCL:

RATING VARIABLE

WCC:

593

TCC:

SHC:

ACC:

Trailers/Vehicles

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Aircraft Gas Turbine Fan Shroud"

An item within a case, fan, aircraft gas turbine engine, designed to surround or partially surround a rotor, fan, aircraft gas turbine engine. It's primary purpose is to protect other components of the engine in the event of an impeller or rotor break up.