Model: 9545M10G01

Aircraft Gas Turbine Engine

Properties:

Mounting Type
Any acceptable
End Application
F118-100 engine
Power Output For Which Designed
Pneumatic/shaft
Criticality Code Justification
Agav
Fuel Type
Jet fuel
Reference Data And Literature
2j-f118-4
NSN
2840-01-475-2554
Part Number
9545M10G01
Description
Engine,gas Turbine,aircraft
CAGE
07482

A continuous combustion type engine. consists primarily of a compressor, aircraft gas turbine engine, chamber, combustion, aircraft gas turbine engine and a turbine assembly, aircraft gas turbine engine. it may have an afterburner, turbine engine and/or a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft, pneumatic power or thrust power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.

Part 9545M10G01 NSN 2840-01-475-2554

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50488
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:
IN
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
671
TCC:
Z
SHC:
9
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8411124050
  • 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 exceeding 25 kn

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