NSN 2915-01-055-6515 · NIIN 010556515 · FSC 2915
NO DASHES 2915010556515
In Stock
PUMP,FUEL,JET ENGINE
Engine Fuel System Components, Aircraft and Missile Prime Movers
Application: FUEL CONTROL, STARTING, TURBINE ENGINE
Technical characteristics
9 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABKW | OVERALL HEIGHT | INCHES MAXIMUM 4.085 |
| ABMK | OVERALL WIDTH | INCHES MAXIMUM 2.205 |
| AGAV | END ITEM IDENTIFICATION | FUEL CONTROL, STARTING, TURBINE ENGINE |
| ARJA | PRESSURE RATING | POUNDS PER SQUARE INCH (PSI) 90.0 |
| FEAT | SPECIAL FEATURES | SPLINE SHAFT DRIVEN |
| SPCL | SPECIAL TEST FEATURES | OPERATING CONDITIONS: SPEED NOMINAL 4200 RPM; BOOST PRESSURE: 5 PSI ABOVE TRUE VAPOR PRESSURE OF THE FUEL TO THE MAXIMUM WORKING PRESSURE OF 90 PSIA; FUEL TEMPERATURE: -65 DEGREES FAHRENHEIT TO +200 DEGREES FAHRENHEIT; AMBIENT TEMPERATURE: -65 DEGREES FAHRENHEIT TO +250 DEGREES FAHRENHEIT; EXTERNAL SPLINE DATA: PITCH: 48/96; PRESSURE ANGLE: 45 DEGREES; NUMBER OF TEETH: 11; PITCH DIAMTER: .2292; BASE DIAMETER: .1621; MAJOR DIAMETER: .2470-.2500; MINOR DIAMETER: .2013-.2083; TOOTH THICKNESS MAXIMUM EFFECTIVE: .0369; TOOTH THICKNESS MINIMUM ACTUAL: .0317; TOOTH THICKNESS, MAS ACTUAL: .0329 |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ANODIZED ALUMINUM CASTING PER MIL-A-8625 TYPE I |
| ZZZV | FSC APPLICATION DATA | ENGINE FUEL SYSTEM COMPONENT,NON AIRCRAFT |
| ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROL DRAWING 102-203-5 |