3-0137-12

Turbine En Axial Compressor Disk

NSN 2840-00-570-9822

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

005709822

Product Features

Steel ams6415, 4.428 in. Min, 4.430 in. Max od, 0.900 in. Min, 0.920 in. Max bore dia, 0.588 in. Min, 0.590 in. Max w, 32 slots on the od, rockwell hardness c scale 35 to 40, 6 mtg holes 0.333 in. Min, 0.335 in. Max diameter on a 3.000 in. Bolt circle dia.

Product Technical Spec.

End Application:

Engine pt6a

General Description:

0steel ams6415, 4.428 in. Min, 4.430 in. Max od, 0.900 in. Min, 0.920 in. Max bore dia, 0.588 in. Min, 0.590 in. Max w, 32 slots on the od, rockwell hardness c scale 35 to 40, 6 mtg holes 0.333 in. Min, 0.335 in. Max diameter on a 3.000 in. Bolt circle dia

NSN:

2840-00-570-9822

Item Name:

Disk,axial Compressor,turbine En

Cage Code:

00198

Cross Referenced Parts

No other part numbers with same form, fit, and function found.

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

61685

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:

6.0 X 6.0 X 1.2

Paclk Weight:

1.2000lbs

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:

Equipment for Aircraft

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Turbine En Axial Compressor Disk"

Inc 61685 cancelled/replaced by ,inc 50568, fiig a10700, app-key g ,inc 50567, fiig a10700, app-key g ,on 021513 ~(all except usa). An item having provisions (generally machined slots) on the outer periph ery for attaching compressor blades, having features for assembling individu al disks on a hub or shaft in a designated arrangement.