What was found
DURING CLIMB. RIGHT OUTER TANK DECREASEED TO 3.32 LBS AND RIGHT INNER INCREASEDTO 14.4. LEFT OUTER WAS 6.13 & LEFT INNER WAS 11.91. WAS ABLE TO STOP R/O DECREASE BY TRINING OFF R/O PUMPS., BUT RIGHT INNER DID NOT DECREASE. AT 37000 LEVEL OFF L/O 6.16 L/I 7.84 CTR 0.07 TRIMI 5.06 R/O 3.15 R/I 11.30. BY USING "FWD" WAS ABLE TO KEEP WING TO WING BALANCE BY USING ONLY CTR & TRIM FUEL. IAW M/M 12-11-28 ATTEMPTED TO TRANSFER FUEL FROM RH INNER TANK, NO LUCK. WHEN SELECTIING ENG PAGE AND FUEL PRESSURE INDICATION, THE RH INNER TANK SHOWED NO FUEL PRESSURE. CYCLED ISO VALVE AND VALVE CONSTANTLY FLASHED. REF M/M 28-22-52- 04 PIGGY BACKED NEW ACTUATOR AND ISO VALVE INDICATION FUNCTIONED NORMALLY. REPLACED ISOLATION VALVE ACTUATOR IAW M/M 28-22-52-04. TRANSFERED AND BALANCED FUEL LOAD PER M/M 12-11-28, CKS NORMAL. PERFORMED FQIS OPERATIONAL BITE, SYSTEM TESTS NORMAL. REF M/M 31-46-00-5 CGCC SYSTEM CKS NORMAL.