NSN 2995-00-884-3285
Part Details | AIRCRAFT FLUID MANIFOLD
2995-00-884-3285 An enclosure with three (3) or more openings designed for use in aircraft de-icing, fuel, hydraulic, oil, pneumatic, and vacuum systems to collect and/or distribute fluids. It may contain valves or metering devices and the like. Excludes MANIFOLD, AIRCRAFT INSTRUMENTS.
Alternate Parts: 3509311, 3-50931-1, 3509311, 3-50931-1, 3509311, 3-50931-1, R11525, R11223, 2995-00-884-3285, 00-884-3285, 2995008843285, 008843285
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
29 | JAN 01, 1962 | 00-884-3285 | 27020 ( MANIFOLD, FLUID, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2995-00-884-3285
Part Number | Cage Code | Manufacturer |
---|---|---|
3-50931-1 | 8X044 | DERCO AEROSPACE, INC. |
3-50931-1 | 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE |
3-50931-1 | 0JRC1 | NORTHROP GRUMMAN TECHNICAL SERVICES,INC. |
R11525 | 50599 | PARKER-HANNIFIN CORPORATIONDBA STRATOFLEX PRODUCT DIVISION |
R11223 | 50599 | PARKER-HANNIFIN CORPORATIONDBA STRATOFLEX PRODUCT DIVISION |
Technical Data | NSN 2995-00-884-3285
Characteristic | Specifications |
---|---|
SPECIAL FEATURES | NO FLAMMABLE MATERIALS SHALL BE USED. DISSIMILAR METALS SHALL NOT BE USED. METALLIC SURFACES SHALL BE TREATED I/A/W MIL-F-7179 |
SUPPLEMENTARY FEATURES | FUEL PRESSURE WILL BE 50 PSIG,FLUID TEMPERATURE WILL RANGE FROM -65F TO 110F,AMBIENT TEMPERATURE WILL RANGE FROM -65F TO 200F |
FUNCTIONAL DESCRIPTION | USED TO DIRECT FUEL TO THE MAIN AND AFTERBURNER FUEL PUMPS OF A TURBO JET ENGINE |
END ITEM IDENTIFICATION | T-38A AIRCRAFT ENGINE |
PART NAME ASSIGNED BY CONTROLLING AGENCY | MANIFOLD,ENGINE FUEL,RH ENG |