Model: 9687M94G01

Aircra Turbine Component Support

Properties:

Inside Diameter
Between 35.047 inches and 35.063 inches
Overall Length
Between 0.540 inches and 0.560 inches
Outside Diameter
Between 38.725 inches and 38.755 inches
Mounting Hole Diameter
Between 0.312 inches and 0.314 inches
Mounting Hole Quantity
118
End Application
Aircraft eng tf-39
Criticality Code Justification
Agav
Material
Steel
Material Specification
Ams 5536 assn standard single material response
NSN
2840-00-111-5749
Part Number
9687M94G01
Description
Support,turbine Component,aircra
CAGE

A support designed for a turbine assembly,aircraft gas turbine engine or one of its components. Excludes support,seal,aircraft gas turbine engine.

Part 9687M94G01 NSN 2840-00-111-5749

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
52560
FIIG:
A521B0
Concept No.:
1
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:
U
ESD:
ESD:
MMAC:
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
850.0000lbs
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:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
052460
UFC:
30360
LTL:
60.0
LCL:
60.0
WCC:
576
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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