Model: 9686M18P07

Aircraft Gas Turbine En Air Seal

Special Features:

T.O. 2j-tf39-4; turbine nozzle

Properties:

Overall Length
Between 1.240 inches and 1.260 inches
Overall Width
Between 0.245 inches and 0.255 inches
Material Thickness
Between 0.004 inches and 0.007 inches
End Application
Aircraft eng tf-39
Engine Section Location
High pressure turbine
Stage Number
2
Material
Nickel alloy
Material Specification
Ams5536 assn standard single material response
NSN
2840-00-111-1018
Part Number
9686M18P07
Description
Seal,air,aircraft Gas Turbine En
CAGE
07482

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 9686M18P07 NSN 2840-00-111-1018

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:
U
ESD:
ESD:
MMAC:
CRITL:
X

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
194120
UFC:
95100
LTL:
85.0
LCL:
100.0
WCC:
671
TCC:
Z
SHC:
Z
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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