4064312

Aircraft Gas Turbine En Air Seal

NSN 2840-01-215-3550

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

012153550

Product Features

T.O. 2j-f100-24, fig 131, in 26

Product Technical Spec.

Overall Length:

0.040 inches

Diameter:

Between 52.850 inches and 52.950 inches

End Application:

Aircraft eng f100-pw-220/125b

Criticality Code Justification:

Abmz and czcj and czbj and abhp

Engine Section Location:

Turbine

Stage Number:

Material:

Nickel alloy

Material Specification:

Ams5587 assn standard single material response

NSN:

2840-01-215-3550

Item Name:

Seal,air,aircraft Gas Turbine En

Cage Code:

31340

Cross Referenced Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

4064312

Cage Code:

77445

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

4064312

Cage Code:

52661

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

4064312

Cage Code:

1J4P3

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:

0.1000lbs

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

Submit this form for current pricing and availability quote on part number 4064312 and/or cross reference parts.

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.