3060710-23

306071023 Fuel Jet Engine Pump

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Datasheet. 3060710-23 specification

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.

fuel PUMP-Main turbine engine (post SB73-3122) (post SPBTFE0931)

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

honeywell TFE731-5Br

Specification/standard Data
The document designator of the specification or standard which established the item of supply.

99193-3060710-23 manufacturers standard

Answers.

What is the NSN for 3060710-23?

2915-01-594-6484

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 3060710-23?

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 2915-01-594-6484 PUMP,FUEL,JET ENGINE

fuel pump-main turbine engine (post SB73-3122) (post SPBTFE0931)

NIIN
015946484
NIIN Date
04/25/11
Schedule B
8803300060 
Name Code
32360
FIIG
A23900
DEMIL / ITAR
USML/ITAR controlled item (Code: Q)
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

Major End Users Countries and entities

  • - Spain 

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Similar by Design Other pumps with similar characteristics

Nothing similar to this part number was found in our inventory

3060710-23 / Pump,fuel,jet engineWhat is the formal definition of this item?

A device specifically designed to deliver fuel to a jet engine. the device may be of single/multistage and positive/nonpositive displacement design. it mounts on a jet engine accessory drive case or on the fuel control and is driven by the engine. excludes all pumps not specifically designed to be used on a jet engine.