Model: STU21A34

Air Turbine Engine Starter

Properties:

Document Source
99237
Document Identification
And20002
Standard Mounting Feature
Included
Air Supply Inlet Pressure
45.0 pounds per square inch
Air Supply Inlet Tempurature Rating
450.0 degrees fahrenheit
Output Torque Rating
225.000 foot-pounds
Air Inlet Connection Type
Flange
Quick Detachable Mounting Feature
Included
Mounting Type Designator
Xii&s
NSN
2995-00-065-9478
Part Number
STU21A34
Description
Starter,engine,air Turbine
CAGE
80049

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

Part STU21A34 NSN 2995-00-065-9478

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:
24.5 X 18.5 X 16.5
Paclk Weight:
37.5000lbs
Item Weight:
23.0000lbs
Item Dim:
010001000123
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
F000003XE7
SPI Rev.:
SPC Mkg:
17
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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