9688M08P01

Aircraft Turbine Nozzle Retainer

NSN 2840-00-115-9510

DEMIL

Shelf Life

UOM

NIIN

Demil:

Shelf Life:

N/A

UOM:

1 EA

NIIN:

001159510

Technical Specifications of NSN

End Application:

5arleigh burke class ddg; engine, marine gas turbine lm-2500; aircraft, galaxy c-5; spruance class dd (963); engine, aircraft, tf39-ge-1 (c-5a); supply class aoe; ticonderoga class cg (47); oliver perry class ffg; fms - build frigates class ships

Criticality Code Justification:

Agav

Stage Number:

Material:

Steel

NSN:

2840-00-115-9510

Item Name:

Ring,segment Set

Cage Code:

08244

Other Related Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

9688M08P02

Cage Code:

07482

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9688M08P01

Cage Code:

07482

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9688M08P01

Cage Code:

03350

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9688M08P01

Cage Code:

28884

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

52405

FIIG:

A522S0

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:

0.2000lbs

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:

194120

UFC:

95100

LTL:

RATING VARIABLE

LCL:

WCC:

671

TCC:

SHC:

ACC:

Equipment for Aircraft

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Segment Set Ring"

An item specifically designed to position and/or restrain the movement of one or more nozzle, nozzle segment, or nozzle assembly, turbine, aircraft gas turbine engine. It may be the full 360 degrees required for one turbine stage or a segment thereof.