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)
29JAN 01, 196200-884-328527020 ( MANIFOLD, FLUID, AIRCRAFT )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2995-00-884-3285
Part Number Cage Code Manufacturer
3-50931-18X044DERCO AEROSPACE, INC.
3-50931-176823NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE
3-50931-10JRC1NORTHROP GRUMMAN TECHNICAL SERVICES,INC.
R1152550599PARKER-HANNIFIN CORPORATIONDBA STRATOFLEX PRODUCT DIVISION
R1122350599PARKER-HANNIFIN CORPORATIONDBA STRATOFLEX PRODUCT DIVISION
Technical Data | NSN 2995-00-884-3285
Characteristic Specifications
SPECIAL FEATURESNO FLAMMABLE MATERIALS SHALL BE USED. DISSIMILAR METALS SHALL NOT BE USED. METALLIC SURFACES SHALL BE TREATED I/A/W MIL-F-7179
SUPPLEMENTARY FEATURESFUEL PRESSURE WILL BE 50 PSIG,FLUID TEMPERATURE WILL RANGE FROM -65F TO 110F,AMBIENT TEMPERATURE WILL RANGE FROM -65F TO 200F
FUNCTIONAL DESCRIPTIONUSED TO DIRECT FUEL TO THE MAIN AND AFTERBURNER FUEL PUMPS OF A TURBO JET ENGINE
END ITEM IDENTIFICATIONT-38A AIRCRAFT ENGINE
PART NAME ASSIGNED BY CONTROLLING AGENCYMANIFOLD,ENGINE FUEL,RH ENG