N510TA
Registered owner: TAUS CORP, DE (owner ≠ operator)
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.
24 reports on file, 2005-03-24 – 2008-12-19.
Part: FIRE LOOP — DEFECTIVE (NR 1 ENGINE)
ENGINE NR 1 SHUT DOWN IN FLIGHT DUE TO A FIRE INDICATION DURING FLIGHT FROM BDL TO BQN. BOTH FIRE BOTTLES WERE DISCHARGED. WARNING LIGHT EXTINGUISHED. ACFT LANDED NORMALLY. NO FUEL DUMPED. MX REPLACED 3 FIRE LOOPS AND AN AMPLIFIER. RUN UP CHECK OK. ACFT RETURNED TO SERVICE.
Part: SILL — FOD (CARGO DOORWAY)
AC AFTER TAKEOFF, LOUD WHISTLING NOISE HEARD AND AC HAD PROBLEMS PRESSURIZING. AC MADE UNSCHEDULED STOP, WITH NORMAL LANDING. FOUND F.O.D. AND DEBRIS IN MAIN CARGO DOOR SILL AREA. REMOVED F.O.D. AND DEBRIS FROM CARGO DOOR SEAL AREA IAW 52-70-00. SEAL FOR MAIN CARGO DOOR INSPECTED IAW A300 52-36-11 SUPPLEMENT MANUAL, SEAL LEAK CK SATISFACTORY. AC RETURNED TO SERVICE. (A)
Part: VALVE — STUCK (GROUND VENT)
AFTER TAKEOFF, PRESSURIZATION MALFUNCTION OCCURRED. ACCOMPLISHED ABNORMAL PROCEDURES. AC RETURNED TO FIELD. LANDING NORMAL. MX FOUND GROUND VENT VALVE STUCK CLOSED. MX CLEANED AND RESET GROUND VENTING VALVE IAW 21-31-17, PG 501. OPS CHECKED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (K)
Part: CSD — MALFUNCTIONED (NR 1) · airframe 40,282 hrs · 24,694 cycles
DURING FLIGHT, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY RISING OIL TEMPERATURE. DISCONNECTED CSD AND RETURNED TO MFM FOR A SAFE LANDING. REPLACED CSD IAW MM 24-11-11 PG 401 AND CSD OIL COOLER IAW 24-11-21 PAGE 401. AIRCRAFT RELEASED FOR SERVICE.
Earlier reports · 2005–2007 · 20 reports
2007
Part: DAMPER — MALFUNCTIONED (LT MLG) · airframe 39,684 hrs · 24,271 cycles
AFTER DEPARTURE WHEN RAISING GEAR, LEVER WOULD NOT GO PAST THE MID POSITION, GEAR POSITION LIGHTS REMAINED 'GREEN'. RETURNED TO FIELD AND MADE A SAFE LANDING. AIRCRAFT MAINTENANCE FERRIED TO CTS IN JAPAN FOR CORRECT ACTION. REPLACED LT GEAR PITCH DAMPER, AIRCRAFT RELEASED FOR SERVICE.
Part: LINE — OBSTRUCTED (PITOT/STATIC) · airframe 39,440 hrs · 24,163 cycles
DURING TAKEOFF ROLL, FIRST OFFICERS AIR SPEED LAGGED BEHIND CAPTAINS BY 40-60 KNOTS, ABORTED TAKEOFF. FLUSHED DEBRIS FROM PITOT PRESSURE LINES, ACCOMPLISHED PITOT/STATIC TEST IAW 34-11-10 PAGE 501. TEST NORMAL. AIRCRAFT RELEASED FOR SERVICE.
Part: PITOT TUBE — LEAKING · airframe 39,440 hrs · 24,163 cycles
DURING TAKEOFF THE FIRST OFFICERS AIRSPEED INDICATOR LAGGED 40-60 KNOTS BEHIND CAPTAINS AIRSPEED INDICATOR. FOUND RT PITOT PROBE LEAKING, REPLACED RT PITOT PROBE IAW A300 MM 34-11-15 PAGE 401. ACCOMPLISHED LEAK CHECK IAW A300 MM 34-11-10 PAGE 501. AIRCRAFT RELEASED FOR SERVICE.
Part: CIRCUIT BREAKER — WEAK · airframe 39,439 hrs · 24,162 cycles
AFTER TAKEOFF, FUEL PUMP NR 1; 1A; 2 CIRCUIT BREAKERS POPPED, AND AFCS AND FLIGHT ENGINEER PANEL LIGHTS WENT OFF. RETURNED TO FIELD AND MADE A SAFE LANDIBG. REPLACED FAULTY BREAKER IN 101VU PANEL.
Part: FITTING — CORRODED (FUSELAGE) · airframe 39,437 hrs · 24,160 cycles
DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 36R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12, INSTALLED FITTING IAW SRM 51-30-30.
Part: FITTING — CORRODED (FUSELAGE) · airframe 39,437 hrs · 24,160 cycles
DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 38R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12, INSTALLED FITTING IAW SRM 51-30-30.
Part: FITTING — CORRODED (FUSELAGE) · airframe 39,437 hrs · 24,160 cycles
DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 37R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12, INSTALLED FITTING IAW SRM 51-30-30.
Part: FITTING — CORRODED (FUSELAGE) · airframe 39,427 hrs · 24,160 cycles
DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD STR TIE END ANGLE FITTING AT 35R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40, APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12, INSTALLED FITTING IAW SRM 51-30-30.
Part: BOLT — CORRODED (NR 2 ENGINE) · airframe 39,437 hrs · 24,160 cycles
DURING ACCOMPLISHMENT OF CPCP C54-400-03-00 AT M96 CHECK LEVEL II CORROSION WAS FOUND ON 4 HORIZONTAL BOLTS OF NR 2 ENGINE AFT MOUNT. REMOVED AND REPLACED 4 HORIZONTAL MOUNT BOLTS IAW MM 20-21-17 AND MM 70-00-00.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,437 hrs · 24,160 cycles
DURING ACCOMPLISHMENT OF CPCP TASK C53-310-02-00 AT M96 CHECK, LEVEL II CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD AT STR TIE END ANGLE FITTING AT 35R. FABRICATED FITTING FROM 7076 T6511 EXTRUSION IAW SRM 51-10-40. APPLIED PROTECTIVE COATINGS IAW SRM 51-40-12. INSTALLED FITTING IAW SRM 51-30-30.
Part: INDICATION SYS — MALFUNCTIONED (COCKPIT) · airframe 39,437 hrs · 24,160 cycles
DURING TAKEOFF FOR TEST FLIGHT AFTER HEAVY MAINTENANCE VISIT, CONFIGURATION LIGHT AND WARNING HORN CAME ON, TAKEOFF ABORTED. REPLACED LEADING EDGE INSTRUMENTATION UNIT IAW MM 27-84-11. AIRCRAFT RELEASED, TEST FLIGHT COMPLETED SATISFACTORY.
Part: SUPPORT — CRACKED (NR 2 NACELLE) · airframe 39,437 hrs · 24,160 cycles
DURING M-96 CHECK, A 3 INCH CRACK WAS FOUND IN THE NR 2 ENGINE OUTBOARD CORE COWL SUPPORT. ACCOMPLISHED WELD REPAIR IAW ENGINEERING ORDER 2-54907-800 FROM EMTEQ.
Part: TRUNNION — CORRODED (MLG) · airframe 39,437 hrs · 24,160 cycles
DURING M-96 CHECK, CORROSION WAS FOUND IN LT MAIN LANDING GEAR AFT TRUNNION FORWARD LUG FITTING BORE AND FACE. REMOVED CORROSION BY OVERSIZING BORE AND SPOT FACING THE LUG FACE AND INSTALLED NEW BUSHING IAW REPAIR DESIGN APPROVAL SHEET RAS/BAE/1005347/2007.
Part: RIB — UNSERVICEABLE (TE FLAP) · airframe 39,437 hrs · 24,160 cycles
DURING M96 COMPLY WITH S/B A300-57-0245, REPLACEMENT OF LT INBOARD FLAP RIB NR 7. REMOVED LEFT WING INBOARD FLAP, RIB NR 7, PERFORMED HFEC INSPECTION IAW A300-57-0245, NO DEFECTS NOTED. INSTALLED NEW NR 7 RIB P/N A5796005000400 IAW S/B A300-57-0245.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 39,437 hrs · 24,160 cycles
DURING M-96 CHECK, FOUND LOWER CROSS BEAM OF FLOORBEAM AT FRAME 57 BL 0 CRACKED. STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-30.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,437 hrs · 24,160 cycles
DURING M-96 CHECK, FLOOR SUPPORT BEAM IN AFT CARGO AT FRAME 63 WAS FOUND CORRODED AND HAD A 5 INCH CRACK BETWEEN STR 41L AND 43L. CUT OUT DAMAGED SECTION OF FLOORBEAM CAP ANGLE AND INSTALLED 12 INCH LENGTH OF FLOORBEAM AND REPAIR DOUBLER IAW SRM 51-41-40.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,437 hrs · 24,160 cycles
DURING M-96 CHECK, FLOOR SUPPORT BEAM IN AFT CARGO A7 FRAME 63 WAS FOUND CORRODED AND HAD A 5 INCH CRACK BETWEEN STR 41L AND 43L. CUT OUT DAMAGED SECTION OF FLOORBEAM CAP ANGLE AND INSTALLED 12 INCH LENGTH OF FLOORBEAM AND REPAIR DOUBLER IAW SRM 51-41-40.
Part: SLIDE — DEPLOYED (LT DOOR) · airframe 39,378 hrs · 24,138 cycles
ON GROUND, CREW OPENED LEFT HAND DOOR WITH DOOR ARMED, SLIDE WAS DEPLOYED. SLIDE WAS PLACED ON MEL 52-61-01 AND AIRCRAFT RELEASED FOR SERVICE. SLIDE WAS REPLACED ON 6-6-07 PER MM 25-61-00 PAGE 401.
2006
Part: SLIDE — WILL NOT ARM (R2 DOOR) · airframe 37,759 hrs · 23,676 cycles
R2 DOOR SLIDE WILL NOT ARM. REPLACED DOOR SLIDE IAW A300 25-61-11. RETURNED TO SERVICE.
2005
Part: ADC — UNSERVICEABLE · airframe 35,058 hrs · 22,896 cycles
AFTER TAKEOFF, CAPTAINS AIRSPEED INDICATOR DECREASED TO ZERO (0). CAPTIANS ALTIMETER REMAINED AT 300 FT. DURING CLIMB OUT. AIRCRAFT RETURNED TO AIRPORT, LANDING NORMAL. REMOVED AND REPLACED AIR DATA COMPUTER IAW 34-12-34. OPS AND FUNCTIONAL CHECK SATISFACTORY, AIRCRAFT RETURNED TO SERVICE.