Model: 9502M19P02

Aircraft Gas Turbi Metallic Seal

Special Features:

Ring, mating, seal, t.O. 2j-f110-14; 8.300 in. Id; 0.100 in. Dia. 16 holes eq sp; o.266 in. Dia. 15 holes, 20 slot eq sp; case is located on the endof the turbine rotor assembly

Properties:

Overall Length
2.505 inches
Diameter
10.960 inches
End Application
F110 aircraft engine
Criticality Code Justification
Agav
Engine Section Location
Low pressure turbine
Material
Steel outer case
Material Specification
Ams6322 assn standard single material response outer case
Surface Treatment
Chromate outer case and nickel outer case
Surface Treatment Specification
Ams2406 assn standard 1st treatment response outer case and ams2404 assn standard 2nd treatment response outer case
NSN
2840-01-192-5374
Part Number
9502M19P02
Description
Seal,metallic,aircraft Gas Turbi
CAGE
07482

A single or multi-piece item of metallic construction, specifically designed to form either a tight fuel or oil seal in an engine, gas turbine, aircraft.

Part 9502M19P02 NSN 2840-01-192-5374

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50597
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:
PR
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
12.5 X 12.5 X 4.5
Paclk Weight:
4.8000lbs
Item Weight:
3.5000lbs
Item Dim:
010000020002
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
F000001D36
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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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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