Model: 9318M95G01

Aircraft Gas Turbine Heat Shield

Properties:

Overall Length
Between 26.420 inches and 26.460 inches
Material Thickness
Between 0.017 inches and 0.023 inches
End Application
Aircraft eng tf-39
Criticality Code Justification
Agav
Engine Section Location
Turbine
Material
Steel comp 630 shield and steel comp 631 shield
Material Specification
Ams5643 assn standard 1st material response shield and ams5528 assn standard 2nd material response shield
NSN
2840-01-111-9731
Part Number
9318M95G01
Description
Shield,heat,aircraft Gas Turbine
CAGE
07482

A rigid item, fabricated from a heat resistant allow, with or without insulation material added. designed to protect parts, areas or systems of an engine, gas turbine, aircraft from excessive heat damage. see also insulation blanket, thermal, aircraft gas turbine engine.

Part 9318M95G01 NSN 2840-01-111-9731

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50356
FIIG:
A530F0
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:
NY
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
30.5 X 16.5 X 16.5
Paclk Weight:
10.0000lbs
Item Weight:
4.5000lbs
Item Dim:
027001100110
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000002E85
SPI Rev.:
SPC Mkg:
17
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
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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