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MRC | Name | Details |
---|---|---|
AGAV | END ITEM IDENTIFICATION | F110-GE-100 AIRCRAFT ENGINE |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | "PUMP,FUEL BOOST" |
FEAT | SPECIAL FEATURES | FSCAP |
FTLD | III FUNCTIONAL DESCRIPTION | BOOST FUEL PUMP |
FTLD | FUNCTIONAL DESCRIPTION | BOOST FUEL PUMP |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | "O/A LG DRIVE SHAFT TO INLET SIDE 8.295 IN. NOM,INLET DIA 4.86 - 4.92 IN.; MOUNT 6.055 - 6.115 IN. DIA,3 HOLLS 0.64 IN. THRU ONE END 0.403 - 0.412 IN. DIA,2 HOLES 0.64 IN. THRU OTHER END 0.403 - 0.412 IN. DIA; ROTATION COUNTERCLOCK; MAIN DISCHARGE 0.98 IN. NOM ID,SEAL AREA 1.839 IN. MIN OD; AUG DISCHARGE 1.78 IN. NOM ID,SEAL AREA 2.745 IN. MIN OD; SPLINE DATA: 16 TEETH,PRESSURE ANGLE 30 DEG,MAJ DIA 0.845 - 0.850 IN.,MINOR DIA 0.682 - 0.692 IN." |
ZZZY | III REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | SOURCE CONTROL DWG NO. 1296M72 |
ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | SOURCE CONTROL DWG NO. 1296M72 |