Model: MILS5866TYPESTU1

Air Turbine Engine Starter

Properties:

Major Diameter
1.2645 inches
Outside Diameter
3.190 inches
Minor Diameter
1.090 inches
Document Source
73030
Document Identification
An20002
Teeth Quantity
24
Standard Mounting Feature
Included
Air Supply Inlet Pressure
54.0 pounds per square inch
Drive Rotation Direction
Counterclockwise
Spline Pitch
20
Pitch Circle Diameter
1.200 inches
Air Inlet Connection Type
Band coupler
Quick Detachable Mounting Feature
Not included
Quantity
1
Fsc Application Data
Engine, aircraft turbo fan
NSN
2995-00-908-0564
Part Number
MILS5866TYPESTU1
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 MILS5866TYPESTU1 NSN 2995-00-908-0564

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:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
25.0 X 19.0 X 17.0
Paclk Weight:
50.0000lbs
Item Weight:
30.0000lbs
Item Dim:
012501100110
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000004XE7
SPI Rev.:
A
SPC Mkg:
19
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
133300
UFC:
63220
LTL:
92.5
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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