100636-1

Tur Centrifugal Compressor Rotor

NSN 2835-00-125-4135

DEMIL

Shelf Life

UOM

NIIN

Demil:

Shelf Life:

N/A

UOM:

1 EA

NIIN:

001254135

Product Features

Steel, ams5355, 16 vanes, 5.755 in. Min, 5.765 in. Max od, 0.7784 in.Min, 0.7788 in. Max id, 2.440 in. Min, 2.460 in. Max o/a lg, 3 holes, no. 8, 0.164 in.-32 nc class 3b thd 0.380 in. Max deep, countersunk 110 degrees by0.154 in. Min, 0.174 in. Max dia.

Technical Specifications of NSN

General Description:

NSN:

2835-00-125-4135

Item Name:

Compressor Rotor,centrifugal,tur

Cage Code:

66195

Other Related Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

4503164

Cage Code:

99167

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

100636-1

Cage Code:

55820

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

4503164

Cage Code:

66195

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

60245

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:

Paclk Weight:

3.0000lbs

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:

123270

UFC:

62600

LTL:

RATING VARIABLE

LCL:

WCC:

593

TCC:

SHC:

ACC:

Construction Materials

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Tur Centrifugal Compressor Rotor"

Inc 60245 cancelled/replaced by ,inc 50588, fiig a10700, app-key j ,inc 50587, fiig a10700, app-key j ,on 021513 ~(all except usa). An item consisting of a series of blades on one or both sides of the rotor disk extending from the axis of rotation radially to the rim of the disk. It is designed to centrifugally cause the air between the blades to move outward to the rim of the compressor section of a turbine engine.