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Datasheet. TF12900-16 specification
A recording of the physical,functional,and performance characteristics for an item of supply.
designed for partially submerged operation, non positive displacement, 2 impellers, 1 main 1 auxiliary, 24v dc 6 amps 6500 rpm 2850 phr at 18 psi rated capacity, 8.093 in. lg 7.015 in. w 4.875 in. h approx o/a dim., 12 holes 0.281 in. dia evenly spaced around a 7.015 in. by 4.875 in. oval mtg flange, 2 unprocessed wire lead electric connection, designed for internal or external discharge connections
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 2915-00-289-9731 PUMP,SUBMERGED,AIRCRAFT
- NIIN
- 002899731
- 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
- - Republic of Korea
- - Portugal
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TF12900-16 / 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.
