3001T03G02

3001T03G02 Fuel Pressurizing And Drai Valve

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Datasheet. 3001T03G02 specification

Overall Length
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.

2.790in. ⁓2-51/64"

Overall Height
The distance measured in a straight line from the bottom to the top of an item.

2.750in.

Overall Width
An overall measurement taken at right angles to the length of an item,in distinction from thickness.

1.560in.

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

J85-GE-5/-13 turbo jet engine

Special Features
Those unusual or unique characteristics or qualities of an item not covered in the other requirements and which are determined to be essential for identification.

t.o.2J-J85-54, f.33a and t.o.2J-J85-64, f.29; drain valve

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.6J15-4-53-3; drain valve ay

Answers.

What quantity is this sold in?

1EA

What material is the fuel pressurizing and drai valve made of ?

Aluminum alloy

What is the overall width?

1.560 inches

What is the NSN for 3001T03G02?

2915-00-073-5712

How is this classified for shipping?

Schedule B number: 8803300060
nmfc 127220
Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts the

What's the federal classification of 3001T03G02?

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 2915-00-073-5712 VALVE,FUEL PRESSURIZING AND DRAI

Used on j85-ge-5/-13 turbo jet engine. t.o.2j-J85-54, f.33a 1.560" overall width 2.790" overall length

NIIN
000735712
NIIN Date
01/01/63
Schedule B
8803300060 
Name Code
61768
FIIG
A23900
Item Weight
1.400lbs
Item Dimensions
63 X 53 X 40
QUP
Historical Price
$8,911.70 EA
DEMIL / ITAR
USML/ITAR controlled item (Code: D)
Hazmat
No hazard information available from HMIRS.
MSDS
N/A
Precious Metals
Metal content unknown
Enviromental
N/A
Electrostatic ESD & EMI
No ESD or EMI sensitivity

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

Major End Users Countries and entities

  • - Department of The Navy  DSOR Contract contiguous united states (conus)
  • - Department of The Air Force  DSOR Contract contiguous united states (conus)
  • - Brazil 
  • - Spain 
  • - Malaysia 
  • - Canada 
  • - Republic of Korea 
  • - Norway 
  • - Greece 
  • - Turkey 

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Shipping Information

Special Handling
Other or no special handling required (sh) 
LTL (less than a truck load rating)
77.5 
LCL (less than a car load rating)
77.5
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)
127220 PRESSURE REG/RED/RELIEF VALVES NOI 
UFC (universal freight code)
64490 

Similar by Design Other valves with similar characteristics

Nothing similar to this part number was found in our inventory

3001T03G02 / Valve,fuel pressurizing and draiWhat is the formal definition of this item?

An item that provides an automatic proportioning of fuel distribution to the engine fuel manifolds, under pressure, to achieve better fuel atomization at the fuel nozzles over a wide range of fuel flows. it must also provide a means of shutting off fuel supply to the engine and draining the fuel manifold after engine shutdown. it must be spring loaded and is either pressure balanced or linkage operated.