Model: IN8

Aviation Turbine Fuel
Description:

This nsn is for af use only to account for purchases of arctic jp8at mcmurdo, antarctica , in8 code nondefinitive spec/std data.

Special Features:

This nsn is for af use only to account for purchases of arctic jp8at mcmurdo, antarctica

Properties:

Maximum Sulphur Content Percentage By Weight
0.3
Freezing Point Maximum Temp
-72.0 degrees fahrenheit
Fuel Grade Classification
Jp-8
Viscosity At Rated Temp
8.00 -20 degrees celsius
Maximum Aromatics Percentage By Volume
25.0
Distillation Point Percentage At Maximum Temp
205.0 degrees c at 10.0 pct and 300.0 degrees c at the end point.
Copper Corrosion Classification Number
1
Density Value
Between 0.775 kilograms per liter and 0.840 kilograms per liter
Minimum Heat Of Combustion Value
18400.0 british thermal units per pound
Maximum Distillation Loss Volume Percentage
1.5
Minimum Flash Point And Test Method
38.0 degrees celsius pensky-martens closed cup
Density Temp
15.0 degrees celsius
Supply Classification
Bulk
Maximum Amount Of Existent Gum
7.0
Nondefinitive Specification/std Data
In8 code
NSN
9130-01-429-4563
Part Number
IN8
Description
Turbine Fuel,aviation
CAGE
81349

A liquid petroleum distillate refined especially for use in aviation turbine engines.

Part IN8 NSN 9130-01-429-4563

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
26646
FIIG:
A090A0
Concept No.:
App. Key:
F
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:
Y
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
155250
UFC:
77320
LTL:
RATING VARIABLE
LCL:
--
WCC:
600
TCC:
R
SHC:
9
ACC:
Fuels and Lubricants

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Schedule B and Export
  • Schedule B: 2710121550
  • SITC: 33460
  • End Use: Petroleum products, other
  • NAICS: 324110
  • USDA: 1

Freight Class: Motor fuels not elsewhere specified or included

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