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Datasheet. TF53500 specification
A recording of the physical,functional,and performance characteristics for an item of supply.
designed for fully submerged operation, non positive displacement, 2 impellers, 2 motors 27v dc 16 amps 5500 phr at 12 psi rated capacity, JP-4 fuel, 26 holes 0.281 in. dia evenly spaced around a 7.656 in. by 14.656 in. oval mtg flange, 14.656 in. lg, 9.406 in. w, 7.656 in. h o/a dim., 2 separate 3 wire unprocessed electrical connections, facility for internal separate or common discharge connection
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 2915-00-308-1642 PUMP,SUBMERGED,AIRCRAFT
- NIIN
- 003081642
- NIIN Date
- 01/01/63
- Schedule B
- 8803300060
- Name Code
- 28519
- FIIG
- A23900
- 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
- - Greece
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TF53500 / Pump,submerged,aircraftWhat is the formal definition of this item?
A completely inclosed machine consisting of a positive or nonpositive displacement pump with a driving motor used to transmit or transfer fluid from an aircraft tank to an engine driven pump or to another tank. it is designed to be partially or completely submerged in the fluid it is intended to pump.
