Model: MIL-T-38219

Aviation Turbine Fuel
Description:

1.000 gallons quantity within each unit package, jp-7 grade nondefinitive spec/std data.

Properties:

Quantity Within Each Unit Package
1.000 gallons
Maximum Sulphur Content Percentage By Weight
0.1
Freezing Point Maximum Temp
-43.5 degrees celsius
Fuel Grade Classification
Jp-7
Viscosity At Rated Temp
8.00 -20 degrees celsius
Mandatory Additive
Fuel system icing inhibitor, antioxidant, lubricity additive and metal deactivator
Specific Gravity Value At 15.56 Deg Celsius
Between 0.779 and 0.806
Minimum Heat Of Combustion Value
18700.0 british thermal units per pound
Minimum Flash Point And Test Method
60.0 degrees celsius pensky-martens closed cup
Supply Classification
Bulk
Maximum Amount Of Existent Gum
5.0
Nondefinitive Specification/std Data
Jp-7 grade
NSN
9130-00-180-6385
Part Number
MIL-T-38219
Description
Turbine Fuel,aviation
CAGE
81349

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

Part MIL-T-38219 NSN 9130-00-180-6385

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:
65.0
LCL:
65.0
WCC:
600
TCC:
R
SHC:
D
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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