N595QS
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
CABIN ODOR: ON ROTATION NOTICED A STRONG SMELL OF BURNING OIL. SMELL DISSIPATED AFTER 1-2 MINUTES. CORRECTIVE ACTION; REMOVED OIL STREAKING FROM AIRCRAFT TAIL, AND LEAK CHECKED APU. NO LEAKS NOTED, SUSPECT APU OIL WAS OVERSERVICED. COMPLETED BORESCOPE OF THE APU COMPRESSOR INLET AREA AND FORWARDED IMAGES TO MCC AND HONEYWELL. COMPLETED ENVIRONMENTAL CONTROL SYSTEM BLEED AND TRIM BLEED DUCT BURN PROCEDURE AND DETECTED NO EVIDENCE OF BURNING OIL SMELL REF TC-68A-21-181006MR3 .
AFTER SELECTING GEAR UP ON T.O. RECEIVED A GEAR DISAGREE CAS MESSAGE AND NOSE GEAR STARTED TO BANG. CREW SELECTED LANDING GEAR DOWN AND RECEIVED 3 GREEN INDICATION WITH WOW MISCOMPARE CAS MESSAGE. RAN THE QRH FOR BOTH CAS MESSAGES. CREW LEFT LANDING GEAR DOWN AND DIVERTED TO TJSJ AT 170 KNOTS. TOWER FLYBY INDICATED 3 GEAR DOWN AND THEN MADE A EMERGENCY LANDING AT APPROXIMATELY 25,350 LBS. CORRECTIVE ACTION: PERFORMED 5 GEAR SWINGS TO OPS CHECK. OPS CHECK OF NLG SQUAT SWITCH. OPS CHECKS GOOD. NO DEFECTS NOTED. IAW CE 680A AMM 32-30-00 & 32-20-00.
UPON TAKE OFF AND GEAR RETRACTION. NOSE GEAR STARTED TO BANG. WE HAD A GEAR DISAGREE CAS AND A WOW MIS COMPARE CAS. QRH FOR BOTH PROBLEMS WERE ACCOMPLISHED GEAR APPEARED TO LOCK DOWN. (3 GREEN. ). LANDED WITH NOSE HIGH TO KEEP WEIGHT OFF AS LONG AS POSSIBLE. UPON LANDING NOSE WHEEL SHUTTERED FOR A FEW SECONDS WE WERE ABLE TO TAXI NORMALLY BACK TO FBO FOUND NLG STRUT WAS IMPROPERLY SERVICED, SERVICED NLG STRUT WITH MIL-5606 AND N2 IAW CE-680A AMM 12-10-52. PERFORMED LEAK CHECK OF NLG STRUT, NO LEAKS NOTED. PERFORMED LG RETRACTION CHECK IAW CE-680A AMM 32-30-00-720. NO DEFECTS NOTED.
EMERGENCY LIGHTS DO NOT EXTINGUISH WITH THE EMER LIGHT SWITCH IN THE ARM POSITION AND DC POWER ESTABLISHED ON THE AIRCRAFT. COMPLIED WITH TC-FLT-33-1001 AND PERFORMED EMERGENCY LIGHTS OPERATIONAL CHECK TASK CARD PERFORMED SUCCESSFULLY WITH NO FAULTS FOUND AND OPERATIONAL CHECK GOOD WITH NO FAULTS FOUND NO OTHER DISCREPANCIES NOTED AT THIS TIME WORK PERFORMED IAW AMM 33-50-00.
MAIN DOOR HANDLE RELEASE BUTTON IS LOOSE IN ITS HOUSING. THE BUTTON FALLS OUT WHEN HANDLE IS OPENED//CORRECTICE ACTION// UPON FURTHER EVALUATION FOUND DOOR HANDLE RELEASE BUTTON BACKING NUT LOOSE,RETIGHTENED I/A/W CE 680A M/M 52-10-16
AIR DISTRIBUTION: CRUISING AT FL400 WE GOT A TEMP FAULT CABIN WHITE MESSAGE. IT EXTINGUISHED AFTER ABOUT 5 SECONDS. THEN WE GOT AN AMBER ACM O'HEAT FOLLOWED BY AN AMBER EMER PRESS. ALL CHECKLISTS WERE COMPLIED WITH. // SIGN OFF // REMOVED AND REPLACED CABIN DUCT TEMP SENSOR TT041 SN: 241444 WITH NEW SN: 330012. PERFORMED SATISFACTORY OPS CHECK, WORK PERFORMED IAW CE-680A AMM 21-60-10 & 21-60-00
L/H AND R/H MLG SIDE BRACE FITTING GOUGE.
APPROXIMATELY 90 MINUTES INTO THE FLIGHT WE STARTED OUR DECENT FOR LANDING. FIRST WE GOT A ENG CNTRL FAULT R MESSAGE THEN WE WOULD GET A GEA FAIL 3 MESSAGE (THAT WOULD CYCLE ON AND OFF FOR THE DURATION OF THE PROBLEM). WITH THE GEA FAIL 3 MESSAGE WE WOULD ALSO GET LOSS OF INDICATIONS OF RIGHT FUEL FLOW AND OIL PSI, RIGHT GEAR AND ROLL SPOILER INDICATIONS AND RIGHT ELECTRICAL INDICATIONS. THE EVENT MARKER WAS PRESSED TWICE (ONCE FOR JUST THE ENG CNTRL FAULT AND AGAIN FOR BOTH MESSAGES). RUNNING THE CHECK LISTS DID NOT CLEAR THE PROBLEM. APPROX 25 MINS INTO THE PROBLEM AND AT 13000 ALL PROBLEMS CLEARED UP AND NEVER SHOWED UP AGAIN. AS PER THE CHECK LIST THE GEAR WAS BLOWN DOWN. "CORRECTIVE ACTION" INSTALLED DIAGNOSTICS COMPUTER AND RETRIEVED ENGINE DATA. DISCONNECTED AND CLEANED THE RT ENGINE EEC CONNECTORS IAW MM 72-00-02 FIGURE 110 AND 111. RELOADED GEA 7100 #3 SOFTWARE IAW MM 42-10-04-5. PUSHED AIRCRAFT OUTSIDE AND PERFORMED ENGINE RUNS. NO DEFECTS NOTED DURING ENGINE RUNS.
AIRCRAFT LEFT AIRPORT AND RETURNED BACK, AFTER TAKEOFF LANDING GEAR HANDLE WAS RAISED ON SCHEDULED BUT AFTER THE MAIN MOUNTS INDICATED UP AND LOCKED THE NOSE GEAR INDICATED A AMBER HASH PATTERN INDICATING ACCORDING TO THE EMERGENCY/ABNORMAL CHECKLIST N-2 THAT NEITHER DOWNLOCK NOR UPLOCK IS INDICATING LOCKED AND AMBER GEAR DISAGREE CAS MESSAGE IS DISPLAYED. CREW COMPLETED EMERGENCY/ABNORMAL CHECKLIST PROCEDURES AND GOT 3 GREEN DOWN AND LOCKED INDICATIONS THEN RETURNED FOR A NORMAL LANDING. SUSPECT RIGHT NOSE GEAR DOOR WAS OFF ITS OVER CENTER STOP PRIOR TO DEPARTURE CAUSING OPERATING ROLLERS TO CONTACT DOOR. PERFORMED SLOW CYCLE AND SEVERAL NORMAL GEAR CYCLES ALSO CHECKED DOOR GAPS AND ATTACH POINTS, NO DEFECTS NOTED LANDING GEAR OPERATED NORMAL REF. CE680A M/M. 32-00-00. DAMAGE NOTED TO BOTTOM SIDE OF RIGHT NOSE LANDING GEAR DOOR - COMPLETED REPAIR OF RH NLG EDGE GUARD REF RFTS-104018 REV 0. PERFORMED LANDING OPERATIONAL AND CLEARNANCE CHECKS IAW MM 32-00-00. OPS/CLEARANCE CHECKS GOOD.
CAPTAIN MLG BRAKE PEDAL SOFT/SPONGY - WHILE BRAKING ON THE RUNWAY IT FELT AS IF THERE WAS NO MORE BRAKING AVAILABLE WHILE APPLYING BOTH BRAKES. THE RIGHT PEDAL FELT SQUISHY AND HAD MORE PLAY. THE MORE I PRESSED THE BRAKE PEDALS THERE WAS NO MORE PRESSURE. SO SLOWING TOOK LONGER THAN NORMAL FOR THE WEIGHT AND RUNWAY CONDITIONS.**SUPPLEMENTAL INFORMATION: CHECKED PILOT & CO-PILOT BRAKE PEDALS. FOUND TO BE SLIGHTLY SOFT. BLED NR 1, NR 2, NR 3, NR 4 BRAKES. VERIFIED PILOT & CO-PILOT BRAKE PEDALS ARE FIRMED UP. WORK DONE IAW MM 32-42-00. NO FURTHER ACTION TAKEN AT THIS TIME.
AFTER RETRACTING LANDING GEAR THE LT GREEN GEAR DOWN INDICATOR, LIGHT STAYED ON. THE LT GEAR DID RETRACT AND ALL OTHER OPERATIONS WERE NORMAL. REMOVED LT MLG ACTUATOR. INSTALLED INSPECTED ACTUATOR IAW 32-30-04 ALL TEST PASS AT THIS TIME.
AFTER RETRACTING LANDING GEAR THE LT GREEN GEAR DOWN INDICATOR LIGHT STAYED ON. THE LT GEAR DID RETRACT AND ALL OTHER OPERATIONS WERE NORMAL.
ON FINAL APPROACH, GEAR WAS SELECTED DOWN AND RESULTED IN THE FOLLOWING INDICATIONS: NOSE AND RT MAIN - GREEN; LT MAIN - NO LIGHT, UNLOCKED LIGHT - RED, HYD PRESS - NO LIGHT. T/S AND FOUND LT MAIN DOWN AND LOCKED SWITCH INOP. RMVD AND REPLACED LT MAIN ACTUATOR. BLED SYSTEM, OPS AND LEAK CHECKS GOOD. IAW MM 32-30-04.
DURING DESCENT, WE NOTICED THE LT MAIN DOWN AND LOCK GREEN ANNUNC ON, WITH NO OTHER ABNORMAL INDICATIONS. T/S TO BAD ACTUATOR. REPLACED L/H MAIN LANDING GEAR ACTUATOR IAW 560XL MM CH 32-30-04. ADJUSTED CAMBER IAW 560XL MM CH 32-10-00. OP'S & LK CK GOOD