Price Quote Get an up to date pricing and availability quote for this product. Order online or over the phone.
Quality Commitment
Serving our customers with quality and safety first.
- AS9120 Certified
- Audited supply chain
- ITAR Registered
- DDTC Registered
- HAZMAT Certified
- Customer service objectives
- Every product 100% inspected
Datasheet. 2770086-103 specification
The national stock number or the identification information of the end equipment for which the item is a part.
canadair challenger, model 601 aircraft fuel system
Answers.
Schedule B number: 8803300060
Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts the
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 2915-01-459-6735 VALVE,FUEL PRESSURIZING AND DRAI
Used on canadair challenger, model 601 aircraft fuel system.
- NIIN
- 014596735
- NIIN Date
- 10/09/98
- Schedule B
- 8803300060
- Name Code
- 61768
- 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
- - Canada
- - Denmark
Availability for 2770086-103 A member of our team will provide you with a price and availability quote
Request a Quote »Similar by Design Other valves with similar characteristics
Nothing similar to this part number was found in our inventory
2770086-103 / Valve,fuel pressurizing and draiWhat is the formal definition of this item?
An item that provides an automatic proportioning of fuel distribution to the engine fuel manifolds, under pressure, to achieve better fuel atomization at the fuel nozzles over a wide range of fuel flows. it must also provide a means of shutting off fuel supply to the engine and draining the fuel manifold after engine shutdown. it must be spring loaded and is either pressure balanced or linkage operated.
