N46AR
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| GULFSTREAM INTERNATIONAL AIRLINES INC | Operator | on 2007-04-18 | Operator named in NTSB report |
Accident & incident history
Operated by GULFSTREAM INTERNATIONAL AIRLINES INC (per NTSB report)
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.
28 reports on file, 2005-03-01 – 2011-06-02.
Part: ANTI-SKID SYS — MALFUNCTIONED (MLG) · airframe 16,359 hrs · 21,989 cycles
PILOT REPORTED WITH ANTISKID ON, ACFT DIFFICULT TO STOP. SERVICED ANTISKID SYS AND PERFORMED ANTISKID SYS CHECK, OPS CHECKED AND TAXI OK, NO DEFECTS NOTED.
Part: CHECK VALVE — FAILED (ANTI SKID SYSTEM) · airframe 16,359 hrs · 21,989 cycles
PILOT REPORTED WITH ANTISKID ON, ACFT DIFFICULT TO STOP. REPLACED ANTISKID HYD SYS CHECK VALVE, OPS CHECK GOOD.
Part: BRAKE ASSY — MALFUNCTIONED (MLG) · airframe 16,264 hrs · 21,864 cycles
AFTER LANDING THE BRAKES WERE INEFFECTIVE, TURNED OFF ANTISKID AND BRAKES WORKED, ANTI SKID FAIL NEVER ILLUMINATED. DRAINED AND SERVICED BRAKE SYS, OPS CHECK GOOD.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,246 hrs · 21,840 cycles
AS ACFT CROSS THE COASTLINE ON THE APPROACH FOR 10L THE CAPTAIN SIDE WINDSHIELD CRACKED. THE INNER WINDOW PANE MADE NUMEROUS CRACK LINES BUT STAYED INTACT. DECLARED AN EMERGENCY, RECEIVED PRIORITY AND LANDED WITHOUT FURTHER INCIDENT. R & R CAPTAINS WINDSHIELD.
Part: PANEL — DEBONDED (LT WING) · airframe 16,139 hrs · 21,707 cycles
DURING SCHEDULED ROUTINE INSP DISCOVERED LT WING INBD EDGE PANEL CORROSION AND DEBOND. REMOVED DAMAGE AND INSTALLED A FILLER AND AN EXTERNAL DOUBLER REPAIR.
Earlier reports · 2005–2010 · 23 reports
2010
Part: BRACKET — BROKEN (AIRSTAIR DOOR) · airframe 15,599 hrs · 21,026 cycles
FLIGHT: 6005 ASD/PBI PILOT REPORTED AIRSTAIR DOOR SNUBBER BRACKET BROKEN. REPLACED AIRSTAIR DOOR COUNTER BALANCE LEVER ASSY.
Part: DOOR — BINDING (EMERGENCY EXIT) · airframe 15,434 hrs · 20,813 cycles
DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT EMERGENCY EXIT DOOR HARD TO OPEN. LUBED LEFT EMERGENCY EXIT DOOR OPERATIONAL CHECKS GOOD.
Part: DOOR — BINDING (EMERGENCY EXIT) · airframe 15,434 hrs · 20,813 cycles
DURING SCHEDULED ROUTINE INSPECTION DISCOVERED LEFT EMERGENCY EXIT DOOR HARD TO OPEN. LUBED LEFT EMERGENCY EXIT DOOR OPERATIONAL CHECKS GOOD.
Part: DOOR — STUCK (EMERGENCY EXIT) · airframe 15,434 hrs · 20,813 cycles
DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT AFT EMERGENCY EXIT HARD TO OPEN. LUBED RIGHT AFT EMERGENCY EXIT OPERATIONAL CHECKS GOOD.
2009
Part: STRUCTURE — LOOSE (AIRSTAIR DOOR) · airframe 15,163 hrs · 20,454 cycles
PILOT REPORTED PLASTIC CASING ON INSIDE AIRSTAIR DOOR GETS CAUGHT ON DOOR JAM WHEN TRYING TO OPEN DOOR. SECURED AIRSTAIR DOOR FWD TRIM PANEL AND HARDWARE. OPS CHECKS GOOD.
Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 14,988 hrs · 20,232 cycles
DURING MX DISCOVERED RT ELEVATOR INBD HINGE BRACKET HAS CORROSION. REPLACED RT ELEVATOR INBD HINGE BRACKET.
Part: SKIN — DELAMINATED (WING) · airframe 14,938 hrs · 20,174 cycles
DURING SCHEDULED INSP, DISCOVERED LT AND RT WING SKIN DELAMINATED AROUND FUEL ACCESS PANELS 531CB, 532CB, 531DB, 532DB, 532FB, 541AB, 632AT,632CB AND 632DB. REPAIRED WING SKIN AROUND FUEL ACCESS PANELS.
Part: ACCESS PANEL — CORRODED (LT WING) · airframe 14,932 hrs · 20,164 cycles
DURING INSP OF LT WING FUEL LEAK, FOUND FUEL ACCESS PANEL 532AB HAS CORROSION AND DEBOND ON INTERNAL RING. INSTALLED REPAIR RINGS AT LT FUEL ACCESS PANEL 532AB.
Part: STRINGER — CORRODED (LT WING) · airframe 14,932 hrs · 20,164 cycles
DURING INSP FOR FUEL LEAK ON LT WING DISCOVERED CORROSION AT LT STRINGER INSIDE COLLECTOR TANK. CLEANED CORROSION AND INSTALLED REPAIR STRAP.
Part: HINGE BRACKET — CORRODED (RUDDER) · airframe 14,884 hrs · 20,102 cycles
DURING SCHEDULED ROUTINE MAINT DISCOVERED RUDDER CENTER HINGE BRACKET HAS EXFOLIATION. REPLACED RUDDER CENTER HINGE BRACKET.
Part: UPLOCK SWITCH — MALFUNCTIONED (LT MLG) · airframe 14,857 hrs · 20,066 cycles
FLIGHT: 5400 AFTER TAKEOFF, LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION, LIGHT EXTINGUISHED AFTER RUNNING QRH. REPLACED LT MAIN GEAR UPLOCK SWITCH. OPS CHECK OK.
Part: SKIN — CORRODED (FUSELAGE) · airframe 14,693 hrs · 19,857 cycles
DURING SCHEDULED ROUTINE INSP DISCOVERED CORROSION ON THE FUSELAGE BELLY UNDER BEACON LIGHT MOUNTING PLATE AT FS 370.750. REMOVED CORROSION AT BEACON LIGHT CUTOUT AND INSTALLED EXTERNAL DOUBLER REPAIR.
Part: SKIN — CORRODED (BS 277 S2-3R) · airframe 14,693 hrs · 19,857 cycles
DURING SCHEDULED ROUTINE INSPECTION DISCOVERED AIRCRAFT FUSELAGE BELLY EXFOLIATION AT F.S 227.630 BETWEEN STRINGERS 2R AND 3R. DURING FUTHER INSPECTION EXFOLIATION LOCATED FS 327.630 AIRCRAFT BELLY BETWEEN STRINGER 14R AND 15R NOT STRINGERS 2R AND 3R REMOVED DAMAGED AREA AND INSTALLED EXTERNAL DOUBLER REPAIR.
2008
Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 14,555 hrs · 19,684 cycles
DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT EMERGENCY EXIT HARD TO OPEN. LUBRICATED LT EMERGENCY EXIT INNER AND OUTER HANDLES. OPS CHECK GOOD.
Part: UPLOCK SWITCH — OUT OF ADJUST (MLG)
FLIGHT 6005, DURING FLIGHT, LANDING GEAR HANDLE LIGHT ILLUMINATED SEVERAL TIMES HYD FLUID LOW ANNUNCIATOR WAS NOT ILLUMINATED AND AIRSPEED KEPT UNDER 180KIAS. C/A ADJUSTED RT MLG UPLOCK SWITCH. OPS CHECK NORMAL. (A)
2007
Part: WIRE HARNESS — DAMAGED (MLG) · airframe 13,186 hrs · 18,008 cycles
AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT, J HOOK, MANUALLY OVERRIDE GEAR STILL WOULD NOT RETRACT. RETURNED TO PBI. LANDED WITHOUT INCIDENT. REPLACED RT MLG DOWNLOCK SWITCH AND SQUAT SWITCH HARNESS. RIGGED LANDING GEAR. EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL.
Part: ENGINE — SEIZED (RIGHT) · airframe 12,645 hrs · 17,344 cycles
FLIGHT: 9265 MHH/PBI - ON STATIC TAKEOFF, AS ADVANCING POWER TO 1,000 LBS OF TORQUE, HEARD LOUD BANG AND RIGHT ENGINE SEIZED OPERATION. ABORTED TAKEOFF. REPLACED RIGHT ENGINE. OPERATIONAL CHECK NORMAL. SUSPECT 2ND STAGE PT BLADE FAILURE.
Part: DPU — SHORTED (COCKPIT) · airframe 12,632 hrs · 17,329 cycles
FLIGHT: 6007, DURING APPROACH COPILOTS EADI WENT BLANK THEN STARTED TO SMOKE. REPLACED COPILOTS DPU OPERATIONAL CHECK NORMAL.
Part: WIRE — LOOSE (RT FIRE BOTTLE) · airframe 12,598 hrs · 17,288 cycles
FLIGHT: 6004, DURING FLIGHT RT FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED. SECURED LOOSE WIRE ON RT FIRE EXTINGUISHER BOTTLE.
Part: CONNECTOR — LOOSE (FIRE BOTTLE) · airframe 12,400 hrs · 17,040 cycles
(9262) FPO/PBI DURING FLIGHT RT FIRE DISCHARGE ANNUNCIATOR ILLUMINATED. SECURED RT FIRE BOTTLE WIRE CONNECTION OPERATIONAL CHECK NORMAL.
2006
Part: FIRE BOTTLE — DEFECTIVE (RT ENGINE) · airframe 12,145 hrs · 16,711 cycles
FLIGHT: 6002 PBI/ASD DURING CLIMB RIGHT ENGINE FIRE EXTINGUISHER DISCHARGE INDICATOR FLICKERED. RETURNED TO PBI LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE AND REPLACED RIGHT ENGINE FIRE BOTTLE OPERATIONAL CHECK NORMAL.
Part: INDICATOR — INOPERATIVE (TCAS)
FLIGHT:9220 PBI/TPA DURING APPROACH TCAS FAILED FOLLOWED BY FUMES IN THE COCKPIT. REPLACE THE LEFT IVSI/TCAS INDICATOR, OPERATIONAL CHECK GOOD.
2005
Part: SPAR — CORRODED (HORIZONTAL STAB)
DURING AN (I) CHECK INSPECTION THE UPPER AND LOWER HORIZONTAL SPAR CAPS WERE FOUND WITH CORROSION IN THE AREA OF THE ELEVATOR HINGES. THIS AREA WAS NOT TREATED OR PRIMED BY THE FACTORY DURING AC MANUFACTURE AND THUS WAS CONDUCIVE TO CORROSION. THIS IS CONSIDEREED TO BE AFACTORY DEFECT REQUIRING INSPECTION, CORROSION CONTROL AND REPAIRS IAW MFG FIELD REPAIR DETAILS.