534463

Aircraft Gas Tur Compressor Vane

NSN 2840-01-160-3183

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

011603183

Product Features

Was vane, compressor stator, turbine engine

Technical Specifications of NSN

Overall Length:

Between 2.647 inches and 2.657 inches

Overall Width:

Between 0.766 inches and 0.784 inches

End Application:

Aircraft eng tf33

Design Type:

Compressor

Criticality Code Justification:

Agav

Engine Section Location:

Compressor

Stage Number:

Material:

Steel comp 410 vane

Material Specification:

Ams5504 assn standard 1st material response vane and ams5613 assn standard 2nd material response vane

NSN:

2840-01-160-3183

Item Name:

Compressor Stator Half Assembly

Cage Code:

77445

Other Related Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

534463

Cage Code:

2B972

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

534463

Cage Code:

33617

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

534463

Cage Code:

55282

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

446063

Cage Code:

77445

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:

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:

120800

UFC:

61410

LTL:

RATING VARIABLE

LCL:

WCC:

590

TCC:

SHC:

ACC:

Trailers/Vehicles

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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.