N113QS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| NETJETS AVIATION, INC. (DXTA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
WHEN CLOSING MAIN CABIN DOOR ON OUTSIDE OF AIRPLANE USING EXTREMAL SWITCH IN AUTO MODE, MED WENT UP ABOUT 1/3 OF THE WAY AND THEN STOPPED AND CAME BACK DOWN. WAS UNABLE TO USE OUTSIDE SWITCH IN EITHER AUTO OR MANUAL TO RAISE DOOR. TRIED USING SWITCH ON INSIDE OF AIRPLANE IN CABIN AND THAT DOESN'T WORK EITHER. MED WAS LEFT IN DOWN/OPEN POSITION. REMOVED PAX DOOR ACTUATOR IAW AMM 52-11-25-000-891. INSTALLED REPAIRED PAX DOOR ACTUATOR IAW GVFD 5000 AMM 52-11-25-400-801. PERFORMED OPERATIONAL TEST OF THE PAX DOOR IAW AMM 52-11-00-720-802. NO DEFECTS NOTED.
AUTOBRAKE FAIL AMBER CAS: EICAS ILLUMINATED AFTER TAKE OFF AND AUTOBRAKE SWITCH KICKED OUT OF "LOW" POSITION TO "OFF" AND WOULD NOT STAY IN "LOW." "BRAKE 50% DEGRADED" EICAS ILLUMINATED SHORTLY AFTER CORRECTIVE ACTION; REPLACED BRAKE CONTROL UNIT. ALL POST MAINTENANCE CHECKS GOOD. ALL WORK DONE I/A/W GL5000 GVD AMM 32-43-01
WHILE COMPLETING OPERATOR'S BASE MAINTENANCE CHECKLIST FOUND R/H FORWARD EXTERNAL EMERGENCY LIGHT AND LOWBOY CABINET LOWER EMERGENCY EXIT SIGN INOP. #3 EMERGENCY LIGHT POWER SOURCE (ELPS) BATTERY FOUND TO NOT BE FUNCTIONING PROPERLY.
AILERON CONTROL: AILERONS ARE BINDING. SOMETIMES ENOUGH TO TURN OFF THE AUTOPILOT. HAND FLYING MADE IT VERY CLEAR THAT THE BINDING HAPPENS SHORTLY AFTER MOVING THE YOKE OUT OF THE NEUTRAL POSITION. BOTH LEFT AND RIGHT. THOUGH MORE PRONOUNCED WHEN ROLLING RIGHT. MANUALLY OPERATED AILERONS (NO HYD POWER) NOTING SMOOTH OPERATION WITH NO BINDING, CATCHING OR ABNORMALITIES NOTED. GAINED ACCESS TO THE LH AND RH AILERON PCU BOX AREAS AS REQUIRED. GAINED ACCESS TO THE FORWARD AND AFT AILERON QUADRANTS AS REQUIRED. WHILE OPERATING AILERONS, PERFORMED VISUAL INSPECTIONS OF LH AND RH AILERON CABLE RUNS AT FORWARD QUADRANTS, AFT QUADRANTS, PCU BOXES AND TENSION REGULATORS WITH NO DEFECTS. INSPECTED AILERON AUTO PILOT SERVO, TRIM SERVO AND CONNECTING CABLE RUNS WITH NO DEFECTS. LOWERED FLAPS AND INSPECTED LH AND RH AILERON CABLES, PULLEYS AND PASS THROUGHS WITH NO DEFECTS NOTED. POWERED AIRCRAFT AND STARTED APU IAW GL5000 AFM. POWERED HYDRAULIC SYSTEM 3A AND 3B INDIVIDUALLY AND OPERATED AILERONS NOTING SMOOTH OPERATION BUT DID OBSERVE AN ABNORMAL NOISE EMANATING FROM THE LEFT AND RIGHT AILERON PCU BOX AREAS. SHUTDOWN SYSTEM 3 AND POWERED SYSTEM 1B NOTING WHILE CYCLING AILERONS THE LH AILERON PCU BOX AREA NOISE BECAME MUCH LOUDER. SHUTDOWN SYSTEM 1B AND POWERED SYSTEM 2B NOTING THAT WHILE CYCLING AILERONS, THE RH AILERON PCU BOX AREA HAS FAINT NOISE FROM PCU BOX AREA. POWERED HYDRAULIC SYSTEM 1B AND 2B TOGETHER NOTING WHILE OPERATING THE AILERONS APPLIED PENETRATING OIL TO EACH OF THE FOUR AILERON TOGGLE LINKS NOTING THE ABNORMAL NOISE FROM THE LEFT AND RIGHT AILERON PCU BOX AREAS STOPPED. POWERED DOWN HYDRAULIC SYSTEMS AND AIRCRAFT IAW THE GL5000 AFM. CONTACTED MCC WITH OUR FINDINGS AND WAS ADVISED THAT THEY HAVE HAD ISSUES WITH SEIZING TOGGLE LINKS CAUSING AILERON BINDING IN THE PAST. PER MCC, TECHS COMPLIED WITH NJA TASK CARD TC-FLT-27-1001, INSPECTION & LUBE OF AILERON TOGGLE LINKS NOTING THE FINDINGS. REMOVED LEFT AILERON OUTBOARD TOGGLE LINK IAW GL5000 MM TASK 27-11-28-000-801. CLEANED AND INSPECTED TOGGLE LINK AND BALLS WITH NO DEFECTS NOTED. LUBRICATED TOGGLE LINK IAW GL5000 MM TASK 12-22-00-640-838. OK TO INSTALL. INSTALLED SERVICEABLE TOGGLE LINK USING 1EA NEW FOR AND BOLT P/N 376091-5 AND 1EA NEW AFT BOLT P/N NAS6709DU29 IAW GL5000 MM TASK 27-11-28-400-801. NO RIGGING REQUIRED. REMOVED RIGHT AILERON OUTBOARD TOGGLE LINK P/N 376019-1 IAW GL5000 MM TASK 27-11-28-000-801. CLEANED AND INSPECTED TOGGLE LINK AND BALLS NOTING TOGGLE LINK DAMAGED (SURFACE FLAKING) AND REQUIRES REPLACEMENT. LUBRICATED NEW TOGGLE LINK IAW GL5000 MM TASK 12-22-00-640-838. OK TO INSTALL. INSTALLED NEW TOGGLE LINK ASSEMBLY P/N 376019-1 USING 1EA NEW FORWARD BOLT P/N 376091-5 IAW GL5000 MM TASK 27-11-28-400-801. NO RIGGING REQUIRED. REMOVED RIGHT AILERON INBOARD TOGGLE LINK P/N 376019-1 IAW GL5000 MM TASK 27-11-28-000-801. CLEANED AND INSPECTED TOGGLE LINK AND BALLS NOTING TOGGLE LINK BALL DAMAGED (SCORING) AND REQUIRES REPLACEMENT. LUBRICATED NEW TOGGLE LINK IAW GL5000 MM TASK 12-22-00-640-838. OK TO INSTALL. INSTALLED NEW TOGGLE LINK ASSEMBLY P/N 376019-1 USING 1EA NEW FORWARD BOLT P/N 376091-5 IAW GL5000 MM TASK 27-11-28-400-801. NO RIGGING REQUIRED. POWERED HYDRAULIC SYSTEM 1B AND 2B TOGETHER NOTING WHILE OPERATING THE AILERONS THE ABNORMAL NOISE FROM THE LEFT AND RIGHT AILERON PCU BOX AREAS PREVIOUSLY OBSERVED WAS NO LONGER PRESENT. PERFORMED RIGGING CHECK OF THE AILERON CONTROL SURFACES IAW THE MM TASK 27-11-29-220-802. PERFORMED OPERATIONAL TEST OF THE AILERON CONTROL SYSTEM IAW GL5000 MM TASK 27-11-00-710-801. OPERATIONAL CHECKS GOOD. POWERED DOWN HYDRAULIC SYSTEMS AND AIRCRAFT IAW THE GL5000 AFM. CONTACTED MCC WITH FINDINGS AND MCC ELECTS NO FURTHER ACTION AT THIS TIME. CLOSED ALL ACCESS AS REQUIRED. ORIG SUBMISSION DATE: 10-20-2023
MAIN DOOR PRIMARY SEAL: NOTICEABLE AIR NOISE IN VICINITY OF FORWARD SIDE OF THE MAIN DOOR SEAL. DAYLIGHT VISIBLE AT ALTITUDE IN VICINITY OF DOOR HANDLE. // SIGNOFF// INSPECTED MAIN DOOR PRIMARY SEAL AND DOOR VENT SEAL. NO DEFECTS NOTED. PRESSURIZED A/C AND PERFORMED LEAK CHECK OF MAIN DOOR AND DOOR VENT. NO DEFECTS NOTED. REF. BOMBARDIER GLOBAL 5000 AMM 21-00-00.
MAIN DOOR PRIMARY SEAL: AT APPROX FL400 CREW HEARD PULSING AIR NOISE FROM THE MAIN DOOR. NOTICED AMBIENT LIGHT COMING THRU THE RIGHT SIDE OF DOOR SEAL. AT LOWER ALTITUDES LIGHT WAS NOT PRESENT AROUND SEAL. PICTURE INCLUDED.
MAIN DOOR: MAIN CABIN DOOR ONLY COMES UP HALF WAY. BOTH MANUAL AND AUTO MODES ATTEMPTED. MOTOR KEEPS RUNNING AND BOTTOM STEP CONTINUES TO FOLD UP AS NORMAL. // SIGNOFF // REMOVED PASSENGER DOOR ACTUATOR INSTALLED PASSENGER DOOR ACTUATOR IAW GLOBAL 5000 AMM REF 52-11-25 FUNCTIONAL TEST SATISFACTORY
MAIN DOOR: PASSENGER DOOR WILL NOT RISE BEYOND 2 TO 3 FEET DURING THE CLOSE PROCESS. THE DOOR MOTOR STRAINS THEN FAILS TO LIFT IN THE PROCESS. ADDITIONALLY, ONCE CLOSING FAILS, THE DOOR REMAINS IN FAILED POSITION UNTIL THE AIRSTAIR DOOR SWITCH IS PRESSED AGAIN, THEN THE DOOR LOWERS IN A CONTROLLED MANNER. // SIGNOFF// PERFORMED OPERATIONAL CHECK OF PASSENGER DOOR FOUND TO BE SATISFACTORY. DISCREPANCY COULD NOT BE DUPLICATED. WORK REFERENCE GLOBAL 5000 AMM 52-11-00- AS APPLICABLE
L OUTBD BRAKE FAIL AMBER CAS: THE MESSAGE CAME ON WHEN WE SELECTED GEAR DOWN POSITION AT KRVS. WE DID A GO AROUND AND RAN CHECKLIST. RAN ALL CHECKLISTS AND DIVERTED BACK TO KICT DUE TO MUCH LONGER RUNWAY. THE "AUTOBRAKE FAIL " CAS MESSAGE CAME ON AS WELL, BUT WAS DUE TO TUE BRAKE FAILURE. THE AIRPORT IN KICT DECLARED AN EMERGENCY FOR US AND WE WERE MET BY THE FIRE EQUIPMENT. THE FAULT CODE LISTED IS 3246015HA. //SIGNOFF// PERFORMED BRAKE CONTROL VALVE TEST IN A/C OMS AND FOUND L/H OUTBD BCV RESISTANCE TEST FAIL BCV CHANNEL A AND B SHOWS L/H OUTBOARD PRESSURE PULSE TEST FAILURE L/H OUTBOARD BRAKE PRESSURE SHOWS L/H OUTBOARD BRAKE STUCK AND NO HYD FLUID WOULD FLOW AND NO MOVEMENT OF PUCKS ON BRAKE STUCK IAW GLOBLE 5000 AMM PART 2 REV 38 32-43-00 SENT NUM DOWNLOAD TO MCC IAW GL5000 AMM PART 2 REV 7 TASK 45-45-00 R&R L/H BRAKE CONTROL VALVE RESISTANCE TEST IN A/C OMS TEST PASSED PERFORMED OPS TEST OF THE BRAKE SYSTEM IAW GL-5000 AMM 32-43-00 REV 38 TEST FAILED PERFORMED OPS CHECK OF BRAKE HYD FUSE IAW GL-5000 AMM 32-13-33 REV 38 OPS CHECK FAILED R&R BRAKE HYD FUSE IAW GL500 AMM 32-43-33 REV 38 PERFORMED OPS CHECK OF BRAKE HYD FUSE IAW GL500 GVFD AMM 32-93-04 REV 38, OPS CHECK PASSED PERFORMED OPS CHECK OF THE BRAKES SYSTEM IAW GL5000 AMM 32-93-04 REV 38 OPS CHECK PASSED NO DEFECTS NOTED TAXIED AND OPS CHECKED BRAKES IAW GL5000 GROUND OPS CHECK LIST REV 16 NO DEFECTS NOTED