Model: 1999M69P06

Aircraft Gas Tu Compressor Blade

Special Features:

Original name blade, compressor rotor, turbine engine

Properties:

Overall Length
Between 30.814 inches and 30.834 inches
Overall Width
3.397 inches
Diameter
31.305 inches
Material Thickness
Between 0.230 inches and 0.561 inches
End Application
Acft.Eng. Tf39
Design Type
Compressor
Criticality Code Justification
Agav
Engine Section Location
Low pressure compressor
Stage Number
2
Material
Steel blade
NSN
2840-01-117-2903
Part Number
1999M69P06
Description
Blade,compressor,aircraft Gas Tu
CAGE
07482

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

Part 1999M69P06 NSN 2840-01-117-2903

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50531
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:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
36.1 X 15.1 X 9.4
Paclk Weight:
22.0000lbs
Item Weight:
12.7000lbs
Item Dim:
031301100051
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F010365687
SPI Rev.:
A
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114215
UFC:
63220
LTL:
RATING VARIABLE
LCL:
85.0
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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