762952

Aircraft Gas Tur Compressor Vane

NSN 2840-00-878-6170

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

008786170

Product Features

Original name vane, compressor stator, turbine engine

Product Technical Spec.

End Application:

Tf-33 aircraft engine

Design Type:

Compressor

Criticality Code Justification:

Agav

Engine Section Location:

Compressor

NSN:

2840-00-878-6170

Item Name:

Compressor Stator Half Assembly

Cage Code:

77445

Cross Referenced Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

625652

Cage Code:

77445

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

762952

Cage Code:

52661

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

762952

Cage Code:

33617

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

762952

Cage Code:

55282

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:

133300

UFC:

63220

LTL:

RATING VARIABLE

LCL:

WCC:

593

TCC:

SHC:

ACC:

Equipment for Aircraft

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Pricing & Availability

Submit this form for current pricing and availability quote on part number 762952 and/or cross reference parts.

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.