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Datasheet. 254A1290-5 specification
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.
6.000in. ⁓6-1/64"
The distance measured in a straight line from the bottom to the top of an item.
2.000in.
An overall measurement taken at right angles to the length of an item,in distinction from thickness.
6.000in.
The name assigned to the item by the government agency or commercial organization controlling the design of the item.
engine start brake assembly
A recording of the physical,functional,and performance characteristics for an item of supply.
spring loaded friction disks apply resistance to and give feedback to the engine start lever assembly during normal operation. in CUT-Off position the switchs inside the engine start brake assy operates the fuel supply CUT-Off to the engine
Answers.
6.000 inches
Schedule B number: 8411997050
Parts of gas turbine aircraft engines, other than for use in civil aircraft
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 2915-01-582-1218 FUEL CONTROL,STARTING,TURBINE EN
engine start brake assembly 6.000" overall width 6.000" overall length
- NIIN
- 015821218
- NIIN Date
- 02/09/10
- Schedule B
- 8411997050
- Name Code
- 61548
- FIIG
- A23900
- DEMIL / ITAR
- USML/ITAR controlled item (Code: D)
- 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
- - Australia
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254A1290-5 / Fuel control,starting,turbine enWhat is the formal definition of this item?
A self-contained metering unit consisting primarily of pumping, controlling, valving, and/or governing components. it is designed for regulating the delivery of starting fuel into a turbine engine.
