719401-2

Turbo-jet Engine

NSN 2840-01-279-1323

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

012791323

Product Features

Net explosive wt.Shipboard 1.340 lb, explosive storage wt.1.340 lb, explosive transportation wt.1.340 lb; 1.4 dept of defense hazard class; 00 inhabited building distance; class i firefighting group; storage comp.Code s; i coast guard class; j402-ca-400 f/harpoon; white, c/o rear frame 724695-101, control assembly fuel 722825-2, fuel pump and metering 722986-4; pkg.1 per foam container 722758

Technical Specifications of NSN

Overall Length:

42.500 inches

Overall Height:

18.500 inches

Overall Width:

20.000 inches

Fuel Type:

Jet fuel

NSN:

2840-01-279-1323

Item Name:

Engine,turbo-jet

Cage Code:

03104

Other Related Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

J402-CA-400

Cage Code:

30003

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Number:

J402-CA-400

Cage Code:

30003

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

02007

FIIG:

A526A0

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:

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

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Turbo-jet Engine"

A continuous-combustion type power unit, may be with or without container, designed to exert thrust. It's prime physical characteristics include air compressor(s), combustion chamber(s) and gas turbine. The operating principle is as follows: atmospheric air is inducted into the unit at its front, compressed, heated by combustion of a fuel, expanded through the gas turbine, and ejected at high velocity. It may incorporate features to vary direction of the thrust.