Model: CF6-80C2A2

Aircraft Gas Turbine Engine

Special Features:

106 in. Max. Dia.; high-bypass turbofan; 53.500 max power at sea level

Properties:

Mounting Type
Aircraft
Overall Length
168.000 inches
End Application
A310 transport aircraft
Fuel Type
Jet fuel
NSN
2840-01-529-1291
Part Number
CF6-80C2A2
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 CF6-80C2A2 NSN 2840-01-529-1291

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:
A
ESD:
A
MMAC:
CRITL:
X

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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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