111R218P2

Aircraft Gas Tur Compressor Disk

NSN 2840-00-872-1697

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

008721697

Product Features

Original name disk, axial compressor, turbine engine

Technical Specifications of NSN

End Application:

J-47, j-79, t-58, t-64 aircraft eng

Design Type:

Axial compressor

Criticality Code Justification:

Agav

Engine Section Location:

Compressor

NSN:

2840-00-872-1697

Item Name:

Disk,compressor,aircraft Gas Tur

Cage Code:

07482

Other Related Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

111R218P2

Cage Code:

T0545

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

111R218P1

Cage Code:

07482

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

111R218P1

Cage Code:

24446

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

50567

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:

18.0000lbs

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:

011790

UFC:

04720

LTL:

RATING VARIABLE

LCL:

WCC:

671

TCC:

SHC:

ACC:

Equipment for Aircraft

We Guarantee with Every Order

100% Genuine Manufacturers Parts
Every Product thoroughly Inspected
Sales Record Retention of 7 years
Fast Delivery
HAZMAT Certified
Global Shipping

Pricing & Availability

Submit this form for current pricing and availability quote on part number 111r218p2 and/or cross reference parts.

Definition Definition of approved item name (AIN): "Aircraft Gas Tur Compressor Disk"

An item having provisions on the outer periphery for attaching a designated number of blade, compressor, aircraft gas turbine engine. it also has provisions for attachment to a hub, compressor, aircraft gas turbine engine and/or a shaft, turbine, aircraft gas turbine engine.