4071453

Aircraft Turbine Shroud Segment

NSN 2840-01-322-2051

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

013222051

Product Features

T.O. 2j-f100-54; 35 holes eq sp 0.520-0.540

Product Technical Spec.

Overall Length:

Between 0.532 inches and 0.542 inches

Overall Width:

3.825 inches

Diameter:

Between 20.480 inches and 20.500 inches

Material Thickness:

Between 0.050 inches and 0.060 inches

End Application:

F100pw0229 aircraft engine

Design Type:

Axial compressor

Criticality Code Justification:

Agav

Engine Section Location:

Compressor

Stage Number:

Material:

Titanium alloy

Material Specification:

Ams4928 assn standard single material response

NSN:

2840-01-322-2051

Item Name:

Shroud Segment,turbine,aircraft

Cage Code:

1645F

Cross Referenced Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

4071453

Cage Code:

77445

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:

22.6 X 22.6 X 3.4

Paclk Weight:

4.5000lbs

Item Weight:

1.0000lbs

Item Dim:

020502050010

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:

118150

UFC:

64090

LTL:

70.0

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 4071453 and/or cross reference parts.

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.