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Datasheet. 3505716-6 specification
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.
390.2 mm
A measurement of the longest straight line across a circular cross-sectional plane.
247.1 mm
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.
turbine type: single stage, axial flow; reduction gearing: compound planetary (rotating ring gear) ; internal engagement: sprag clutch type; starter cutoff speed: 6750 rpm max.; output shaft turns: clockwise viewed from output shaft end
Characteristics or qualities of an item,not covered in any other requirement,which are considered essential information for one or more functions excluding nsn assignment.
inlet air connection: 76.2 mm diameter, ; lubrication capacity: 22.6 fluid ounces (640 cc) ; lubrication system type: splash with lube pump
Answers.
Schedule B number: 8411997050
Parts of gas turbine aircraft engines, other than for use in civil aircraft
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 2995-01-581-8321 STARTER,ENGINE,GAS TURBINE
turbine type: single stage, axial flow; reduction gearing: compound planetary (rotating ring gear) ; internal engagement: sprag clutch type; starter cutoff speed: 6750 rpm max.; output shaft turns: clockwise viewed from output shaft end 390.2mm overall length
- NIIN
- 015818321
- NIIN Date
- 01/29/10
- Schedule B
- 8411997050
- Name Code
- 21907
- FIIG
- A23900
- DEMIL / ITAR
- Uncontrolled item (Code A)
- 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
- - Republic of Korea
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3505716-6 / Starter,engine,gas turbineWhat is the formal definition of this item?
An item designed to accelerate a gas turbine engine from rest to starter cutoff speed by means of a combustion gas driven turbine and reduction gear assembly constructed to be mounted on the engine starter drive. the combustion gas is generated from ignited liquid fuel and air in the combustion chamber or from a solid propellant cartridge attached to the combustion chamber of the starter. may have provision for energizing the turbine by low pressure air from engine bleed or ground equipment air supply.
