Model: 305-415-804-0

Aircraft Gas Turbine Rotor Blade

Special Features:

Material inconel 100

Properties:

Overall Length
4.000 inches
End Application
F108 aircraft engine
Design Type
Compressor
Blade Attachment Method
Lock
Criticality Code Justification
Agav
Part Name Assigned By Controlling Agency
Blade assembly-lpt rtr stg 1
Engine Section Location
Low pressure turbine
Stage Number
1
Material
Nickel alloy
Reference Data And Literature
T.O. 2j-f108-14, fig fin 72-54-00-9 ind 525
NSN
2840-01-371-5782
Part Number
305-415-804-0
Description
Blade,turbine Rotor,aircraft Gas
CAGE
58828

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 305-415-804-0 NSN 2840-01-371-5782

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:
PN
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
4.0 X 4.0 X 6.0
Paclk Weight:
0.3000lbs
Item Weight:
0.1000lbs
Item Dim:
004000100010
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F013715336
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:
77.5
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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