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Datasheet. 26482-1000 specification
The national stock number or the identification information of the end equipment for which the item is a part.
auxiliary power unit; power unit, gas turb
The name assigned to the item by the government agency or commercial organization controlling the design of the item.
combuster assembly
Answers.
1EA
Schedule B number: 8411917010
Parts of turbojets and turbopropeller aircraft engines 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 2995-01-521-1200 STARTER,ENGINE,DIRECT COMBUSTION
Used on auxiliary power unit;power unit,gas turb. combuster assembly
- NIIN
- 015211200
- NIIN Date
- 06/10/04
- Schedule B
- 8411917010
- Name Code
- 61122
- FIIG
- A23900
- QUP
- 1
- Historical Price
- $3,182.50 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
- - Spain
- - Republic of Korea
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26482-1000 / Starter,engine,direct combustionWhat is the formal definition of this item?
An item designed to accelerate a gas turbine engine from rest to starting speed by means of gas generated by combustion of fuel and air in a combustion chamber, and thrust directly on the engine turbine through an impingement nozzle mounted in the turbine section. consists of a combustion chamber, air and fuel system components and igniter. may include the starter tube and/or impingement nozzle.
