Model: 1881M11P01

Aircraft Gas Turbine Rotor Blade

Properties:

Overall Length
Between 4.784 inches and 4.794 inches
End Application
Aircraft eng f110ge129
Design Type
Axial compressor
Blade Attachment Method
Fir tree
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Blade, low pressure turbine rotor-stage 1, mach
Engine Section Location
Low pressure turbine
Stage Number
1
Material
Nickel alloy blade
Reference Data And Literature
2j-f110-14 fig 90 ind 1
NSN
2840-01-447-2506
Part Number
1881M11P01
Description
Blade,turbine Rotor,aircraft Gas
CAGE

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 1881M11P01 NSN 2840-01-447-2506

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:
PR
CRITL:
F

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:
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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