Model: 111R304P01

Aircraft Gas Turbine Rotor Blade

Properties:

Overall Length
Between 5.850 inches and 5.868 inches
Overall Width
Between 1.530 inches and 1.570 inches
Material Thickness
Between 0.668 inches and 0.683 inches
End Application
J79 engine
Criticality Code Justification
Agav
Engine Section Location
Turbine
Material
Steel blade
NSN
2840-01-007-5442
Part Number
111R304P01
Description
Blade,turbine Rotor,aircraft Gas
CAGE
07482

An item mounted on a disk, turbine, aircraft gas turbine engine. it is designed to create the flow of air in the turbine section of an engine, gas turbine, aircraft.

Part 111R304P01 NSN 2840-01-007-5442

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50535
FIIG:
A10700
Concept No.:
App. Key:
A
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:
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.4000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
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:
--
WCC:
671
TCC:
Z
SHC:
9
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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