P201P05

Aircraft Gas Tur Compressor Vane

NSN 2840-01-204-3707

DEMIL
Shelf Life
UOM
NIIN
Demil:
DEMIL/MLI
Shelf Life:
N/A
UOM:
1 EA
NIIN:
012043707

Detail Specifications

Overall Length:
4.736 inches
Overall Width:
1.051 inches
End Application:
F110 aircraft engine
Criticality Code Justification:
Czcj and abhp and abmk and czbj
Engine Section Location:
Compressor
Stage Number:
1
Material:
Titanium alloy
Material Specification:
C50tf20 cl-a mfr ref single material response
NSN:
2840-01-204-3707
Item Name:
Compressor Stator Half Assembly
Cage Code:
S0635

Manufacturer Part Numbers

Part Number
Cage
RNCC
RNVC
RNAAC
Status
MSDS
SADC
Part Number:
P201P05
Cage Code:
07482
RNCC:
3
RNVC:
2
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
P201P05
Cage Code:
9X952
RNCC:
5
RNVC:
2
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
P201P01
Cage Code:
07482
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
P201P03
Cage Code:
58828
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:
Part Number:
P201P07
Cage Code:
58828
RNCC:
5
RNVC:
9
RNAAC:
MF
Status:
A
MSDS:
SADC:

Part Identification

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50611
FIIG:
A10700
Concept No.:
App. Key:
A
Cond. Code:
1
Status:
A

Part Materials

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
A
ESD:
ESD:
MMAC:
JF
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
7.0 X 3.0 X 3.0
Paclk Weight:
0.3000lbs
Item Weight:
0.1000lbs
Item Dim:
005000130008
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
LVL_B:

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:
Z
ACC:
Equipment for Aircraft

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Pricing & Availability

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Privacy | Terms

Definition Definition of approved item name (AIN): "Compressor Stator Half Assembly"

A component of a vane assembly, compressor, aircraft gas turbine engine. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.

MOE Major Organizational Entities

Entity
DSOR
User:
DEPARTMENT OF THE AIR FORCE Dept. of the Air Force
DSOR:
User:
GREECE Greece
DSOR:
Import / Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft


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