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Datasheet. 383766-2-5 specification
A recording of the physical,functional,and performance characteristics for an item of supply.
90.0 horsepower max. output, 82.5 lb weight, shaft speed 3100 to 3300 rpm, axial flow turbine wheel
Answers.
1EA
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 2995-01-004-5744 STARTER,ENGINE,GAS TURBINE
- NIIN
- 010045744
- NIIN Date
- 06/10/75
- Schedule B
- 8411997050
- Name Code
- 21907
- FIIG
- A23900
- Item Weight
- 9,999.900lbs
- Item Dimensions
- QUP
- 1
- Historical Price
- $830,190.00 EA
- 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
Major End Users Countries and entities
- - Department of The Navy DSOR Fleet readiness center south east (frc-se), jacksonville fl
- - Greece
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383766-2-5 / 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.
