Model: 9397M40

Aircraft Gas Turbine En Fan Case

Special Features:

2nd stage; 1 piece extruded case replaced p/n 1288m61g01 and reworked to p/n 9397m40g02

Properties:

Overall Length
Between 23.433 inches and 23.453 inches
Diameter
Between 95.930 inches and 95.950 inches
End Application
Aircraft eng tf39
Design Type
Axial compressor
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Original name case and nozzle assembly, turbine, aircraft
Engine Section Location
Fan
Material
Aluminum alloy
Material Specification
Ams4150 assn standard single material response
Reference Data And Literature
T.O. 2j-tf39-4, fig 38, ind 3
NSN
2840-01-167-2923
Part Number
9397M40
Description
Case,fan,aircraft Gas Turbine En
CAGE
07482

A case that is an integral part of an engine, gas turbine, aircraft, designed to surround and protect a fan, aircraft gas turbine engine.

Part 9397M40 NSN 2840-01-167-2923

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50551
FIIG:
A10700
Concept No.:
3
App. Key:
D
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:
NY
CRITL:
Y

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
593
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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