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Datasheet. PDC1-1B-6-4 specification
A recording of the physical,functional,and performance characteristics for an item of supply.
current rating 5 amps inductive at 18 to 29.5 vdc; contact resistance 0.25 ohm max.; alt limits range from 1000 ft to 50000 ft; temp limits operative range from 32 deg f to 122 deg f; ZZKJA92114-PDC1-1B-6-4
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 2915-01-343-5509 REGULATOR,FUEL FLOW,TURBO-JET EN
- NIIN
- 013435509
- NIIN Date
- 08/14/91
- Schedule B
- 8803300060
- Name Code
- 60914
- FIIG
- A23900
- DEMIL / ITAR
- USML/ITAR controlled item (Code: B)
- Hazmat
- No hazard information available from HMIRS.
- MSDS
- N/A
- Precious Metals
- --
- Enviromental
- N/A
- Electrostatic ESD & EMI
- No ESD or EMI sensitivity
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PDC1-1B-6-4 / Regulator,fuel flow,turbo-jet enWhat is the formal definition of this item?
A regulator designed to automatically turn on the fuel and ignition at a specific percent of speed for starting a turbo-jet engine. at another speed, it cuts the ignition and places the fuel pumps in series operation. at still another fixed speed, it shuts off the compressor, bleeds and restores electronic devices to their normal circuits.
