2760131-103

2760131103 Float Aircraft Fuel Tank Valve

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Datasheet. 2760131-103 specification

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

turbo fan engine, alf 502L-2C

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.

operating pressure 0-60 psig, fluid temp -65 to 135 deg f

Answers.

What is the NSN for 2760131-103?

2915-01-381-5547

How is this classified for shipping?

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

What's the federal classification of 2760131-103?

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 2915-01-381-5547 VALVE,FLOAT,AIRCRAFT FUEL TANK

Used on turbo fan engine, alf 502l-2c. operating pressure 0-60 psig, fluid temp -65 to 135 deg f

NIIN
013815547
NIIN Date
10/19/93
Schedule B
8803300060 
Name Code
20620
FIIG
A23900
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

Major End Users Countries and entities

  • - Canada 
  • - Greece 

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Similar by Design Other valves with similar characteristics

Nothing similar to this part number was found in our inventory

2760131-103 / Valve,float,aircraft fuel tankWhat is the formal definition of this item?

A valve specifically designed to control the fuel level in an aircraft fuel tank, such as during aircraft refueling and/or defueling operations. it may include solenoids to permit remote control of the valve.