9992M65G06

Aircraft Turbine Shroud Segment

NSN 2840-01-147-0559

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

011470559

Detail Specifications

Overall Length:

Between 1.019 inches and 1.029 inches

End Application:

Aircraft eng f101, f108-cf-100, and f110-ge-100

Criticality Code Justification:

Agav

Engine Section Location:

Turbine

Material:

Aluminum alloy

NSN:

2840-01-147-0559

Item Name:

Shroud Segment,turbine,aircraft

Cage Code:

8U485

Manufacturer Part Numbers

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

9992M65G06

Cage Code:

07482

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9992M65G06

Cage Code:

T0545

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9992M65G06

Cage Code:

02GZ1

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9992M65G06

Cage Code:

08244

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9992M65G06

Cage Code:

28884

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

9992M65G06

Cage Code:

51992

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

50603

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:

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:

133300

UFC:

63220

LTL:

RATING VARIABLE

LCL:

85.0

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): "Aircraft Turbine Shroud Segment"

A stationary arched metal segment used to establish clearance and a seal for the tip of a blade, turbine rotor, aircraft gas turbine engine. The inner dimension may have open honeycomb or composition filled surface or may be formed by the knife edge metal protrusions of a seal ring, labyrinth, aircraft gas turbine engine.