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Datasheet. TF53400-2 specification
A recording of the physical,functional,and performance characteristics for an item of supply.
designed for partially submerged operation, non positive displacement, 24v dc, 7500 rpm, vertical design, 9.281 in. h parallel to shaft axis, 5.657 in. lg perpendicular to shaft axis, 4.453 in. w perpendicular to shaft axis, 8 mtg holes 0.219 in. dia equally spaced on a 3.687 in. dia circle, external discharge outlet fitted w/straight hose connection 1.000 in. od
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 2915-00-203-1152 PUMP,SUBMERGED,AIRCRAFT
- NIIN
- 002031152
- 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
Other Part Numbers Parts with same form, fit, and function by other manufacturers
Major End Users Countries and entities
- - Republic of Korea
- - Portugal
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TF53400-2 / 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.
