N910DC
Registered owner: CLAIR DANIEL, IL (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.
7 reports on file, 2000-12-20 – 2003-09-14.
Part: PROBE — WORN (PITOT STATIC)
CREW REPORTED ON CLIMB THROUGH 29,000 FT, 'ALT' COMPARISON MONITOR ILLUMINATED. CREW FOUND THE NR 1 MADC IN ERROR. NR 3 SELECTED, AND CLIMB CONTINUED TO FL400. 'ALT' COMPARISON LIGHT ILLUMINATED AGAIN, & NONE OF MADC'S AGREED. ON DESCENT, ALL MADC'S AGAIN AGREED TO FL80. APPARENT CAUSE WAS ERRODED PITOT/STATIC PROBES. A/C WAS THOROUGHLY INSPECTED PHYSICALLY & ELECTRONICALLY PER GULFSTREAM V MM & ONLY DEFECT DISCOVERED WAS UPPER LT & RT PITOT/STATIC PROBES WERE ERRODED & CAUSING REPORTED ERRORS. PROBES (P/N 0856TK3 AND 0856TK4) WERE REPLACED PER THE GV MM & AAC GV CAMP DOCUMENT & ALL MADC SYSTEMS PERFORMED TO SPECIFICATIONS. A/C WAS RETURNED TOS ERVICE & RETURNED TO HOME BASE WITHOUT INCIDENT. (M)
Part: BRAKE ASSY — BROKEN (MLG)
DURING INSPECTION OF THE MAIN LANDING GEAR BRAKES, DRIVE ROTOR CLIPS FOUND THE NR 3 AND NR 4 BRAKE ASSEMBLIES TO HAVE FOUR CLIPS EACH BROKEN OFF. REPLACED BOTH BRAKE ASSEMBLIES WITH OVERHAULED UNITS. THIS IS A KNOWN CONDITION AND TROUBLESHOOTING IS ON GOING.
Part: CONTROLLER — MALFUNCTIONED (AUTOTHROTTLE SYS)
ABNORMAL AUTOTHROTTLE DISENGAGMENT OCCURRED AFTER TAKEOFF. PERFORMED AUTOTHROTTLE OPERATIONAL CHECK IAW MM. NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.
Part: SQUAT SWITCH — FAILED (MLG)
LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF OUT OF KTEB. ALL WOW INDICATED AIR MODE EXCEPT COMBINED WOW WHICH WAS AMBER GROUND. AT 1+03 HOURS AFTER TAKEOFF. COMBINED WOW WENT TO AIR. THE GEAR WAS RETRACTED AND ALL SYSTEMS RETURNED TO NORMAL. A FAULTY WEIGHT ON WHEELS SWITCH. REPLACED ALL SUSPECTED WEIGHT ON WHEELS SWITCHES AS A PRECAUTION. SINCE DEFECT COULD NOT BE DUPLICATED. PERFORMED ALL REQUIRED OPERATIONAL CHECKS IAW MM AND RETURNED AIRCRAFT TO SERVICE.
Part: PUMP — DAMAGED (RT ENGINE)
ENGINE DRIVEN HYDRAULIC PUMP, DAMAGED.
Part: PUMP — DAMAGED (LT ENGINE)
ENGINE DRIVEN HYDRAULIC PUMP, DAMAGED.
Part: TERMINAL BLOCK — DAMAGED (RIGHT IDG)
KPTK - DURING ACCOMPLISHMENT OF GAC CB41 FOR IDG SWEDGED TERMINAL INTEGRITY, ONE OF THE TERMINAL LUGS PULLED OFF THE FEEDER WIRE BY HAND. IMPROPERLY SWEDGED TERMINAL END. GULFSTREAM DISPATCHED TECH TO REPLACE ALL TERMINAL LUGS ON INTEGRATED DRIVE GENERATOR''S FEEDER WIRES PER THE INSTRUCTIONS IN CB41. (X)