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tage checked left converter with digital meter: Volts, Freq and 400Hz ou=put, heat soaked while runner for hour on ramp, checked good. -changed two BUSS Couplers for #2 FGC Flight Guidance Computer.,nuisance ite=, checks good now. -BUSS control relay fail 2 & 3 during initial power up is normal nuisance co=e,
ance co=e, and can be cleared by pushing Nutcracker test switch (squat switch or WO=, Weight On Wheels) Circuit, according to HoneyWell Tech ops and SAV Tech s=pport this is normal nuisance item,. But can be remedied by upgrade of FGC c=mputers from our current -905 to -906 computers., system operates norm
tage checked left converter with digital meter: Volts, Freq and 400Hz ou=put, heat soaked while runner for hour on ramp, checked good. -changed two BUSS Couplers for #2 FGC Flight Guidance Computer.,nuisance ite=, checks good now. -BUSS control relay fail 2 & 3 during initial power up is normal nuisance co=e,
ance co=e, and can be cleared by pushing Nutcracker test switch (squat switch or WO=, Weight On Wheels) Circuit, according to HoneyWell Tech ops and SAV Tech s=pport this is normal nuisance item,. But can be remedied by upgrade of FGC c=mputers from our current -905 to -906 computers., system operates norm
tage checked left converter with digital meter: Volts, Freq and 400Hz ou=put, heat soaked while runner for hour on ramp, checked good. -changed two BUSS Couplers for #2 FGC Flight Guidance Computer.,nuisance ite=, checks good now. -BUSS control relay fail 2 & 3 during initial power up is normal nuisance co=e,
ance co=e, and can be cleared by pushing Nutcracker test switch (squat switch or WO=, Weight On Wheels) Circuit, according to HoneyWell Tech ops and SAV Tech s=pport this is normal nuisance item,. But can be remedied by upgrade of FGC c=mputers from our current -905 to -906 computers., system operates norm
Entities connected to both BUSS Couplers and SAV Tech s