Model: KDS 2840-4003

Aircraft Turbine Blade Retainer

Special Features:

Retainer for the low pressure turbine rotor, stage 1

Properties:

Overall Length
Between 1.115 inches and 1.145 inches
Outside Diameter
Between 21.950 inches and 21.970 inches
End Application
F110-ge-100 aircraft gas turbine engine
Criticality Code Justification
Abhp and abkv and feat
Material
Nickel alloy
NSN
2840-01-434-1990
Part Number
KDS 2840-4003
Description
Retainer,turbine Blade,aircraft
CAGE
3999F

An item specifically designed to position and/or restrain the movement of one or more blade, or blade set, turbine, aircraft gas turbine engine. It may be the full 360 degrees required for one turbine stage or a segment thereof.

Part KDS 2840-4003 NSN 2840-01-434-1990

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52404
FIIG:
A522S0
Concept No.:
App. Key:
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:
O
SPI No.:
SPI Rev.:
SPC Mkg:
33
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
114990
UFC:
58952
LTL:
70.0
LCL:
70.0
WCC:
593
TCC:
Z
SHC:
9
ACC:
Trailers/Vehicles

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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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