Model: 458-50040-1

Air Turbine Engine Starter

Properties:

Outside Diameter
Between 7.455 inches and 8.000 inches
End Application
F108-cf-100 engine for kc135r aircraft
Teeth Quantity
24
Drive Type
Spline
Drive Rotation Direction
Counterclockwise
Spline Pitch
20/30
Pitch Circle Diameter
1.200 inches
Air Inlet Connection Type
Flange
Quantity
1
Shape
Round
Reference Number Differentiating Characteristics
As differentiated by source control dwg 458-50040-1
NSN
2995-01-140-2105
Part Number
458-50040-1
Description
Starter,engine,air Turbine
CAGE

An item designed to accelerate turbojet and turboprop engines from rest to starter cutoff speed by means of an air driven turbine.

Part 458-50040-1 NSN 2995-01-140-2105

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
20437
FIIG:
T135-E
Concept No.:
App. Key:
EA
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:
X

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
25.0 X 14.5 X 15.0
Paclk Weight:
50.0000lbs
Item Weight:
40.0000lbs
Item Dim:
014500800080
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000004XE3
SPI Rev.:
SPC Mkg:
19
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:
671
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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