N11985
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
3 reports on file, 1995-01-23 – 1995-06-17.
Part: HYD PUMP — LEAKING (NR 2 ENGINE)
LAX - FLT 0187- THE YELLOW HYDRAULIC SYSTEM FLUID DROPPED TO THE ORANGE DOT DURING CRUISE. THE HYDRAULIC PUMP WAS DUMPED AND THE FLUID LEVEL REMAINED AT THE ORANGE DOT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE YELLOW SYSTEM NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE PUMP WAS REMOVED AND REPLACED AND LEAK CHECK WAS GOOD. (X)
Part: DUCT — RUPTURED (NR 1 ENG)
FLT NR 288 - EWR - TAKEOFF WAS ABORTED AT 60 KNOTS AFTER THE NR 1 ENGINE N1 DROPPED AND THE EGT ROSE TO 950 DEGREES. MAINTENANCE FOUND THE NR 1 ENGINE 14TH STAGE DUCT BLOWN. THE 14TH STAGE DUCT WAS REMOVED AND REPLACED. THE NR 1 ENGINE WAS RUN AT HIGH POWER WITH ALL PARAMETERS AND INDICATIONS CHECKING NORMAL. S/D - THE FAILURE WAS DUE TO HIGH VIBRATORY STRESSES IN THE 14TH STAGE CDP AIR TUBE RESULTING FROM THE 14TH STAGE AIR BLEED TUBE. THE CF6-50 FLEET HAS BEEN MODIFIED BY REMOVING THE 14TH STAGE AIR BLEED TUBE PER GE SERVICE BULLETIN 75-071. (M)
Part: INPUT ROD — OUT OF ADJUST (LT SPEEDBRAKE)
SDQ - FLT 702 - TAKEOFF WAS ABORTED AT LESS THAN 50 KNOTS DUE TO THE TAKEOFF WARNING HORN COMING ON, ACCOMPANIED BY AN INTERMITTENT CONFIGURATION LIGHT AND SPEEDBRAKE LIGHT. MAINTENANCE FOUND THAT THE LT WING O/B SPEEDBRAKE WOULD NOT FULLY STOW. THE INPUT ROD WAS ADJUSTED PER A300 MM 27-62-15 AND OPERATION OF THE SPEEDBRAKES CHECKED GOOD. (W)