9526M64G17

Aircraft Gas Tur Compressor Vane

NSN 2840-01-259-0609

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

012590609

Product Features

Original name vane, compressor stator, turbine engine

Product Technical Spec.

End Application:

Acft.Eng. F110

Criticality Code Justification:

Agav

Engine Section Location:

Compressor

Stage Number:

NSN:

2840-01-259-0609

Item Name:

Compressor Stator Half Assembly

Cage Code:

07482

Cross Referenced Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

9526M64G11

Cage Code:

07482

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9526M64G11

Cage Code:

33617

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9526M64G11

Cage Code:

50595

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9526M64G11

Cage Code:

58828

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9526M64G11

Cage Code:

93596

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

50611

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:

0.7000lbs

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:

85.0

WCC:

593

TCC:

SHC:

ACC:

Equipment for Aircraft

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Compressor Stator Half Assembly"

A component of a vane assembly, compressor, aircraft gas turbine engine. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.