Model: 642AS0237

Turbo-jet Engine

Special Features:

Mgeneral characteristics item description: item consists of turbojet engine j402-ca-400 plus installation components, has a new or reworked fuel control electronics unit p/n 722070-3 and 722825 or 722068 and 722070

Properties:

NSN
2840-01-135-2555
Part Number
642AS0237
Description
Engine,turbo-jet
CAGE

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.

Part 642AS0237 NSN 2840-01-135-2555

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
02007
FIIG:
A526A0
Concept No.:
App. Key:
Cond. Code:
1
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
120800
UFC:
61410
LTL:
RATING VARIABLE
LCL:
100.0
WCC:
672
TCC:
Z
SHC:
R
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8411114050
  • SITC: 71441
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Turbojet aircraft turbines (engines) other than for civil aircraft, of a thrust not exceeding 25 kn

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