4075741-01

Aircraft Gas Turbine En Air Seal

NSN 2840-01-320-5344

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

013205344

Product Technical Spec.

Overall Length:

Between 1.866 inches and 1.906 inches

Diameter:

Between 18.335 inches and 18.345 inches

Material Thickness:

Between 0.040 inches and 0.050 inches

End Application:

F100pw0229 engine/fdt mod

Hardness Rating:

34.0 rockwell c and 44.0 rockwell c

Criticality Code Justification:

Agav

Engine Section Location:

Turbine

Stage Number:

Material:

Nickel alloy

Material Specification:

Ams5536 assn standard 1st material response and ams5544 assn standard 2nd material response

NSN:

2840-01-320-5344

Item Name:

Seal,air,aircraft Gas Turbine En

Cage Code:

16126

Cross Referenced Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

4075741-01

Cage Code:

77445

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

4075741-01

Cage Code:

52661

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

4075741-01

Cage Code:

1645F

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

50595

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:

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:

WCC:

713

TCC:

SHC:

ACC:

Equipment for Aircraft

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Aircraft Gas Turbine En Air Seal"

A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an engine, gas turbine, aircraft. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal.