9398M83P19

9398M83P19 Main Turbine Engine Fuel Control

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Datasheet. 9398M83P19 specification

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

F110-GE-100 turbo fan augmented jet engine

Part Name Assigned By Controlling Agency
The name assigned to the item by the government agency or commercial organization controlling the design of the item.

main engine control

Functional Description
Describes the capabilities,intended use,and/or purpose for which the item is provided.

FUEL-Metering device used on turbine engines that meters the proper quantity of fuel to be fed into the combustion chambers of the engine.it integrates the parameters of inlet air temperature, compressor speed, compressor discharge pressure, and exhaust gas temperature with the proper position of the cockpit power control lever and demands from the electronic engine control system

Material
The chemical compound or mechanical mixture properties of which the item is fabricated.

aluminum alloy

Reference Data And Literature
Literature and references available for information pertaining to the item.

t.o.6J3-4-115-513 (tcto) ; 2J-F110-4, f.20, i.113

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 drawing

Answers.

What quantity is this sold in?

1EA

What material is the main turbine engine fuel control made of ?

Aluminum alloy

What is the NSN for 9398M83P19?

2915-01-448-0588

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 9398M83P19?

FSC 2915 ⁓ Engine fuel system components, aircraft and missile prime movers

Note-fuel components specially designed for propulsion fuel systems, aircraft and missiles are to be placed in this fsc.

Excluding aircraft fuel tanks (fsc 1560); in-flight refueling system fuel components (fsc 1680). fuel system components not specifically designed for use with aircraft engines or missile prime-movers.

NSN 2915-01-448-0588 FUEL CONTROL,MAIN,TURBINE ENGINE

Used on f110-ge-100 turbo fan augmented jet engine. main engine control

NIIN
014480588
NIIN Date
08/20/97
Schedule B
8411997050 
Name Code
61547
FIIG
A23900
Item Weight
65.000lbs
Item Dimensions
200 X 200 X 205
QUP
Historical Price
$279,184.53 EA
DEMIL / ITAR
USML/ITAR controlled item (Code: D)
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. 8062-672 Cage 66503
2. 9398M83 Cage 07482

Major End Users Countries and entities

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

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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 fuel controls with similar characteristics

Nothing similar to this part number was found in our inventory

9398M83P19 / Fuel control,main,turbine engineWhat is the formal definition of this item?

A self contained metering unit consisting primarily of pumping, controlling, valving, and/or governing components. it is designed for regulating the delivery of fuel into the main fuel system of a turbine engine.