Model: 1807M26G01

Aircraft Gas Turbine Rotor Blade

Special Features:

Material external platinum aluminide coating, this is part of the ht90 mod for the tf39, original drawing name blade, high pressure turbine rotor stage 2, trail

Properties:

Overall Length
4.891 inches
Overall Width
Between 1.347 inches and 1.352 inches
End Application
Aircraft eng tf39
Design Type
Axial compressor
Blade Attachment Method
Fir tree
Criticality Code Justification
Agav
Engine Section Location
High pressure turbine
Stage Number
2
Material
Aluminum blade
NSN
2840-01-444-7012
Part Number
1807M26G01
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 1807M26G01 NSN 2840-01-444-7012

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:
NY
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
6.3 X 6.3 X 10.5
Paclk Weight:
1.8000lbs
Item Weight:
1.0000lbs
Item Dim:
004900140014
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000001XA1
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
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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