Model: 6866634

Aircraft Gas Turbine En Air Seal

Properties:

Overall Length
1.280 inches
Diameter
10.046 inches
End Application
Tf-41 aircraft gas turbine engine
Design Type
Axial compressor
Criticality Code Justification
Apgf and czbj and abhp and abmz
Part Name Assigned By Controlling Agency
Original name seal, static rear
Engine Section Location
Turbine
Material
Aluminum alloy
Material Specification
Ams4217 assn standard single material response
NSN
2840-00-236-5002
Part Number
6866634
Description
Seal,air,aircraft Gas Turbine En
CAGE
63005

A rigid metallic item, generally circular. It may be formed of segmented arcs. It is designed to prevent leakage of air in an engine, gas turbine, aircraft. It may be of various cross-sectional shapes. It may have mounting facilities. It may act as a spacer but its primary function is as an air seal.

Part 6866634 NSN 2840-00-236-5002

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50595
FIIG:
A10700
Concept No.:
App. Key:
H
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:
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
2.0000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
RATING VARIABLE
LCL:
--
WCC:
713
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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