458-50040-1

458500401 Engine Air Turbine Starter
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Datasheet. 458-50040-1 specification

Outside Diameter
The length of a straight line which passes through the center of a circular figure or body,and terminates at the outside circumference.

7.455in. and 8.000in.

End Item Identification
The national stock number or the identification information of the end equipment for which the item is a part.

F108-CF-100 engine for KC135R aircraft

Teeth Quantity
The number of teeth included on the item.

24

Drive Type
Indicates the type of drive for turning,rotating,or positioning the mechanism.

spline

Drive Rotation Direction
The direction of rotation of a rotating drive.

counterclockwise

Spline Pitch
A measurement of the spline pitch of the item.

20/30

Pitch Circle Diameter
The length of a straight line which passes through the center of a pitch circle,and terminates at the circumference.

1.200in.

Air Inlet Connection Type
Indicates the type of air inlet connection on the item.

flange

Quantity
A numeric value which represents a positive whole value without regard to any unit of measure.

1

Shape
The physical configuration of the item.

round

Reference Number Differentiating Characteristics
A feature of the item of supply which must be specifically recorded when the reference number covers a range of items.

as differentiated by source control dwg 458-50040-1

Answers.

What quantity is this sold in?

1EA

What is the outside diameter?

7.455 inches minimum and 8.000 inches maximum

What is the NSN for 458-50040-1?

2995-01-140-2105

How is this classified for shipping?

Schedule B number: 8411997050
nmfc 133300
Parts of gas turbine aircraft engines, other than for use in civil aircraft

What's the federal classification of 458-50040-1?

FSC 2995 ⁓ Miscellaneous engine accessories, aircraft

Note-items classified in this class must be specifically designed for use with aircraft or quided missile primemovers only.

Excluding exhaust system; (fsc 1560); jet engine hydraulic reservoirs (fsc 2840); jet engine oil tanks (fsc 2840); electrical starters (fsc 2925); cockpit mounted control quadrants (fsc 1680); aircraft engine covers (fsc 1730).

NSN 2995-01-140-2105 STARTER,ENGINE,AIR TURBINE

Used on f108-cf-100 engine for kc135r aircraft. 7.455" outside diameter

NIIN
011402105
NIIN Date
10/08/82
Schedule B
8411997050 
Name Code
20437
FIIG
T135-E
Item Weight
50.000lbs
Item Dimensions
250 X 145 X 150
QUP
1 
Historical Price
$79,962.88 EA
DEMIL / ITAR
USML/ITAR controlled item (Code: B)
Hazmat
No hazard information available from HMIRS.
MSDS
N/A
Precious Metals
No precious metals
Enviromental
N/A
Electrostatic ESD & EMI
No ESD or EMI sensitivity

Other Part Numbers Parts with same form, fit, and function by other manufacturers

1. 36E153-2A Cage 99551
2. 36E153-4A Cage 99551
3. 458-50040-503 Cage 82918
4. 36E153-6B Cage 99551
5. 36E153-6C Cage 99551
6. 458-50040-502 Cage 82918
7. 36E153-6E Cage 6T459

Major End Users Countries and entities

  • - Department of The Air Force  DSOR Oklahoma city air logistics complex (afsc), oc-alc, tinker afb, ok
  • - Singapore 

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Shipping Information

Special Handling
Other or no special handling required (sh) 
LTL (less than a truck load rating)
Rating variable 
LCL (less than a car load rating)
85.0
Special Cargo
No special type of cargo code applicable 
Air Freight (Minimum cargo door size required)
Shipment is not a consolidation and does not exceed 84 inches in any dimension. 
Customs Requirement Classification
Supplies and equipment for aircraft and aerial targets, including aircraft and maintenance parts, aircraft accessories, aircraft 
Commodity (for shipments via water)
Aircraft parts, to include test/tool sets and equipment (other than armament systems) 
NMFC (national motor freight code)
133300 MACHINERY/MACHINES NOI 
UFC (universal freight code)
63220 

Similar by Design Other starters with similar characteristics

Nothing similar to this part number was found in our inventory

458-50040-1 / Starter,engine,air turbineWhat is the formal definition of this item?

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