Model: 9340M95G07

Aircraft Gas Turbine Heat Shield

Properties:

Overall Length
Between 13.360 inches and 13.400 inches
Overall Width
1.400 inches
Material Thickness
Between 0.030 inches and 0.034 inches
End Application
Aircraft eng f110
Criticality Code Justification
Agav
Engine Section Location
Exhaust
Material
Nickel alloy shield
Material Specification
Ams5540 assn standard single material response shield
NSN
2840-01-200-0123
Part Number
9340M95G07
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 9340M95G07 NSN 2840-01-200-0123

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:
PR
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
--
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

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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