N807QS
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
ON DEPARTURE GEAR RETRACTION HANDLE WOULD NOT MOVE TO GEAR UP POSITION. ON THIRD TRY HANDLE MOVED TO GEAR UP POSITION BUT AMBER CAS MESSAGES BEGAN TO POPULATE ON PFD AND GEAR INDICATIONS DISPLAYED YELLOW BOX WITH DASHES AND A NOSE GEAR DOWN INDICATION. WE RAN THE GEAR CONTROL FAULT QRH PROCEDURE AND DIVERTED. REPLACED MLG OLEO ASSY. OPS CHECK GOOD. IAW AMM 32-10-10.
MAIN CABIN DOOR BECOMING VERY DIFFICULT TO LATCH CLOSED. ARRIVED TO THE A/C IN ATTEMPT TO DUPLICATE THE FAULT, CONNECTED THE A/C BATTERIES, CLOSED THE MED FROM THE OUTSIDE WITH EASE. OPENED THE MED, CLOSED FROM INSIDE THE A/C WITH EASE AS WELL. CLEANED AND LUBRICATED THE PINS, CYCLED THE MED DOOR FROM CLOSE TO OPEN BOTH INSIDE AND OUT MULTIPLE TIMES AND COULD NOT DUPLICATE THE FAULT. PER MCC DUE TO NO HISTORY WE CAN CLEAR THIS MEL, ALL WORK DONE IAW THE AMM 12-20-15.
AFTER LANDING AND SHUTTING ENGINES OFF, MAIN CABIN DOOR WOULD NOT OPEN. NOTHING HAPPENED WHEN PUSHING THE RED BUTTON. WE ENDED UP TURNING THE BATTERIES TO OFF AND THEN THE DOOR WAS ABLE TO BE OPENED. PERFORMED CABIN DOOR RESET PROCEDURE. REMOVED, INSPECTED, AND RERACKED MAIN CABIN DOOR PCB BOARD, NO FAULTS FOUND, OPS CHECKED MED DOOR SUCCESSFULY, NO FAULTS FOUND WITH MED DOOR. RESTORED COCKPIT SIDE CONSOLE BACK TO ITS ORIGINAL CONFIGRATION. ALL WORK ACCOMPLISHED IN REF WITH AMM 24-60-25.
WHEN TESTING EMERGENCY LIGHTS IN ARM POSITION, LIGHTS DO NOT ILLUMINATE. ACCOMPLISHED QRH 25X PROCEDURE TO CHARGE THE BATTERY PACK AND LIGHTS OPERATED NORMALLY AFTER 30 MINUTES OF CHARGING. SUSPECT NUMBER 2 EMERGENCY LIGHTS BATTERY PACK IS FAILING TO HOLD A CHARGE. CORRECTIVE ACTION: REMOVED LH FORWARD EMERGENCY BATTERY. OPS CHECKED GOOD. IAW CE-700 AMM 33-50-05 AND 33-50-07.
CABIN EMERG LIGHT: EMER LTS NOT HOLDING CHARGED. CHARGE AMD STILL NOT HOLDING CHARGE. //SIGNOFF// WE PERFORMED THE EMERGENCY BATTERY EXERCISE PROCEDURE AND FOUND THAT NO LIGHTS ILLUMINATE AFTER THE INITIAL 60·MINUTE CHARGE, WE INSPECTED ALL FOUR EMERGENCY BATTERIES FOR VOLTAGE AND FOUND THE LH AND RH FWD EMERGENCY BATTERIES ARE HOLDING 27 VOLTS, THE LH FWD INERTIA SWITCH PUSHBUTTON IS NOT SECURED AND REQUIRES REPLACEMENT, THE LH AND RH AFT EMERGENCY BATTERIES ARE NOT READING ANY VOLTAGE . ALL FOUR BATTERIES ARE RECEIVING 27 VOLTS FOR CHARGING FROM THE AIRCRAFT WHEN POWER IS APPLIED. WITH ONLY THE FWD EMERGENCY BATTERIES CONNECTED WE ARE ABLE TO ILLUMINATE ALL EMERGENCY LIGHTING, BUT WHEN THE AFT EMERGENCY BATTERIES ARE CONNECTED NO LIGHTS WILL ILLUMINATE BK-JR⢠02/09/2024 FOUND THE LH FWD INTERTIA SWITCH BOOT TO BE DISPLACED, RESECURED RUBBER BOOT AND SWITCH IS OK FOR SERVICE. REMOVED AND REPLACED BOTH AFT EMERGENCY BATTERIES WITH REPAIRED BATTERIES IAW TEXTRON CE-700 AMM 33·50·05 AND PERFORMED OPERATIONAL CHECK IAW TEXTRON CE-700 AMM 33·50-00 WITH NO DEFECTS NOTED. ORIGINAL SUBMISSION DATE: 02/12/2024
UNABLE TO CLOSE MAIN CABIN DOOR FROM INSIDE OR OUTSIDE. MAIN HANDLE WILL NOT CLOSE, IT FEELS JAMMED. GAINED ACCESS TO DOOR INTERNALS. FOUND UPPER AFT LATCH PIN RECESSED OUT OF GUIDES HOLD AND JAMMED. RESEATED UPPER AFT LATCH PIN INTO GUIDE HOLD. ADJUSTED PUSH ROD #3 THE PREVENT THE UPPER AFT LATCH PIN FROM RECESSING TO FAR INTO THE DOOR AGAIN IAW CE700 AMM CH 52-10-43. COMPLETED CABIN DOOR LATCH/LOCK SYSTEM RIGGING IAW CE 700 AMM 52-10-43 AS REQUESTED BY MCC. NO FURTHER DISCREPANCIES FOUND. COMPLETED CABIN DOOR LATCH/LOCK SYSTEM FUNCTIONAL TEST 5 TIMES IAW CE 700 52-10-43 WITH NO DISCREPANCIES FOUND.
UNABLE TO CLOSE MAIN CABIN DOOR FROM INSIDE OR OUTSIDE. 4 PINS ARE COMPLETELY RECESSED AND ARE STOPPING MAIN DOOR HANDLE TO MOVE. REINSTALLED DOOR PIN, CLEANED PIN. TORQUED BOLT ACCORDINGLY. ONCE COMPLETED, TECHS PERFORMED THE GO/NO-GO TOLERANCE CHECKS WITH NO ISSUES NOTED, DOOR BOLTS WITHIN LIMITS PER AMM. ALL WORK DONE IAW AMM CH 52-10-43. PERFORMED MULTIPLE GOOD OPS CHECKS.
MAIN DOOR HANDLE: MAIN DOOR HANDLE IS JAMMED WILL NOT MOVE TO LOCK POSITION. EVEN WITH DOOR OPEN HANDLE WILL NOT MOVE FREELY. ///SIGN-OFF/// REMOVED STEPS AND INSPECTED ALL LINKAGES AND MECHANISMS IAW CE-700 AMM 52-10-00. FOUND LOWER AFT DOOR LOCKING PIN RETRACTED TOO FAR. CLEANED AND LUBED LOCKING PIN AND OPERATED DOOR MULTIPLE TIMES WITH NO DEFECTS NOTED, DOOR WORKS AS REQUIRED. REINSTALLED STEPS IAW CE-700 AMM 52-10-05. PERFORMED OPERATION CHECKS AGAIN FROM INSIDE AND OUTSIDE OPERATION WITH NO DEFECTS NOTED. DOOR IS WORKING AS REQUIRED AT THIS TIME.
EMERGENCY LIGHTING: WHEN EMER LTS SWITCH IS PLACED TO THE ARM POSITION, NO LIGHTS ILLUMINATE, WHEN PLACED ON, ALL LIGHTS ILLUMINATE.//CORRECTIVE ACTION//REMOVED AND REPLACED LH FWD EMERGENCY BATTERY PACK. OPS CHECK GOOD. ALL WORK ACCOMPLISHED IN REF TO 33-50-07 AND 33-50-00.
EMERG LIGHT SWITCH: EMER LIGHTS DO NOT ILLUMINATE IN THE ARMED POSITION. THEY DO COME ON IN THE ON POSITION. SWITCH IS LOOSE IN PANEL. PERFORMED VARIOUS SUCCESSFUL OPS CHECKS. REMOVED PANEL AND TIGHTENED TOGGLE SWITCH NUT. REMOVED ALL ACCESS GAINED. WORK DONE IN REF WITH CE-700 AMM 33-50-00.
CABIN EMERG LIGHT: EMERGENCY LIGHTING SYSTEM FAILS TO TEST PROPERLY ON PREFLIGHT. ALTHOUGH THEY INITIALLY ALL ILLUMINATE PROPERLY WHEN SELECTING THEM TO "ARM" WITH MAIN SHIP BATTERIES "OFF", THEY REMAIN ILLUMINATED ONCE MAIN SHIP BATTERIES ARE "ON" AND ALSO WITH APU RUNNING. ADDITIONALLY, WITH EMER LIGHTS SWITCH SELECTED "OFF", THEY ALL REMAIN ILLUMINATED. SUSPECT EITHER BAD SWITCH AND/OR RELAY. I DO NOT BELIEVE IT IS THE EMER BATTERIES THAT ARE FAULTY. // SIGNOFF// (GAINED ACCESS TO ANO RESET ALL 4 G-SWITCHES IN THE EMER LIGHT SYSTEM, 2 FWD AND 2 AFT TOP CHARGED EMER LIGHT BATTERIES. PERFORMED MULTIPLE OPS CHECKS OF THE EMER LIGHT SYSTEM AND ALL OPS CHECKS ARE GOOD AT THIS TIME. REF. CE-700 AMM 33-50-00.
CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS FLICKER AND EXTINGUISH WHEN TESTING. ONCE SHIPS POWER IS APPLIED EMERGENCY LIGHTS WORK FINE. ONCE SHIPS BATTERIES ARE TURNED THE OFF , LIGHTS FLICKER AND THEN EXTINGUISH WITH EMERGENCY LIGHTS SWITCH IN THE ON POSITION. // SIGNOFF// REMOVED AND REPLACED BOTH AFT EMERGENCY BATTERY PACK REF. C-700 AMM 33-50-05. PERFORMED OPERATIONAL TEST OF CABIN EMERGENCY LIGHTS REF. C-700 AMM 33-50-00. OPS CHECK GOOD AT THIS TIME WITH NO FURTHER DEFECTS NOTED
THE STINGER ASSY HAS CORROSION ON THE OUTER SKIN AT THE 6 OâCLOCK POSITION.
CRACK NOTED AT LT & RT WING RIB STATION 133.07 FLAP BAY. REPAIRED LT & RT WING TE RIB AT WS 133.07 IAW AQRD ERO-586871.
ONE HOUR INTO CRUISE AT FL410, DETECTED AN UNDEFINED ODOR. TEMP SELECTOR WAS IN 11:00 POSITION. THE LT SIDE OF THE CABIN WAS NOTICEABLY WARMER THAN THE RT SIDE. LATER, WITH TEMP SELECT AT 4:00 POSITION THERE WAS NO DECREASE IN ODOR AND NO CHANGE IN TEMPERATURE. THE RT SIDE OF THE CABIN DID HEAT ON DESCENT. VERY LITTLE AIR FLOW CAME OUT OF DEFOG VENTS IN COCKPIT. FOUND RAM AIR DUCT DISCONNECTED IN AFT BAY. SECURED DUCT. CLEANED COALESCER SOCK IAW AMM 221-70-00. PERFORMED ENVIRONMENTAL SYSTEM FUNCTIONAL TEST IAW AMM 21-00-00. OPS CHECKED GOOD AT THIS TIME. NO ODOR NOTED.
DURING CLIMBE, PLACED GEAR HANDLE IN THE UP POSITION, AND GEAR WOULD NOT RETRACT, SHOWED RED "GEAR UNLOCKED" LIGHT. THREE GREEN PLUS THE RED. AFTER ABOUT 30 SECONDS THE ANNUNCIATORS LOW BREAK PRESSURE & ANTISKD INOPERATIVE, STARTED TO FLASH AND WOULD NOT CANCEL. DECLARED AN EMERGENCY, RAN THE EMERGENCY CHECKLIST, AND CONDUCTED A NORMAL LANDING WITHOUT USE OF BRAKES. OPS CHECKED SYSTEM. DUPLICATED DISCREPANCY. TROUBLESHOT TO A MALFUNCTIONING HYD PUMP VALVE IAW AMM 32-30-00 . R & R DUMP VALVE. FOUND RT SWITCH OUT OF RIG. ADJUSTED RIG OF THE RT SQUAT SWITCH AND VERIFIED PROPER RIG IAW MM. CYCLED LANDING GEAR. OPS & LEAK CHECKED GOOD.
TO START THE SEQUENCE OF GEAR RETRACTION, HAVE TO JIGGLE THE GEAR HANDLE IN ITS UP POSITION. FOUND GEAR HANDLE UP SWITCHES TO BE STICKING. REMOVED DME INDICATOR AND CAGE, CONTROLLER,RMU AND CADE DISPLAY CONTROLLER, MFD,THEN REMOVED GEAR HANDLE. REMOVED AND REINSTALLED GEAR CONTROL SWITCHES S112A AND S112B. REINSTALLED GEAR HANDLE ASSEMBLY. PERFORMED GEAR SWING OPS CHECK OF GEAR CONTROL, GEAR CONTROL CHECK GOOD NO DEFECTS WITH RETRACT OR EXTEND. REINSTALLED INDICATOR RACKS. OPS CHECKS GOOD. IAW MM 32-31-01/32-01-00 & WDM 32-30-01.
ON GEAR RETRACTION AFTER TAKEOFF, GEAR UNLOCKED LIGHT REMAINED ILLUMINATED. INSPECTED GEAR, NO DEFECTS NOTED. CHECKED RIGGING ON UPLOCK SWITCHES & FOUND DEBRIS IN NOSE UPLOCK SWITCH ELECTRICAL CONNECTOR, CLEANED ELECTRICAL CONNECTOR. OPS CHECKED GOOD. WORK PERFORMED IAW AMM 32-61-00 & 32-01-00 & WDM 32-30-01.
THE LT MAIN "DOWN AND LOCKED" LIGHT WOULD NOT ILLUMINATE. R & R BULB ON LT GEAR DOWN LOCK ANNUNCIATOR. PERFORMED LANDING GEAR FUNCTIONAL CHECK AND FULL HYD SYS BLEED. SYS CHECKS GOOD. SERVICED GEAR BOTTLE AS REQUIRED. ALL WORK DONE IAW MM 32-01-00.
AFTER UNLOADING PASSENGER BAGGAGE IN THE AFT BAGGAGE COMPARTMENT, I NOTICED A BURNING ODOR. OPENED THE HELL HOLE. IT WAS EITHER AN ELECTRICAL OR RUBBER ODOR. WE USED THE AIR CONDITIONING CONTINUOUSLY IN THE DESCENT FROM 18,000 FT AND NEVER SMELLED ANYTHING. R & R MOTOR IAW CMM 8.8. OPS AND LEAK CHECKS GOOD.
ATTEMPTED A STATIC T/O AND THE RT ENG DIDN'T MAKE THE COMPUTED T/O PWR WITH FULL THROTTLE TRAVEL. IT WAS 2 PERCENT SHORT OF THE REQUIRED 92.2 PERCENT AT 0 DEG C. PERFORMED TAXI/ POWER OF THE DAY CHECKS WITH CREW AT 5 DEGREES C. POWER NEEDED WAS 91.5 PERCENT N1 AND POWER ACHIEVED WAS 93 PERCENT N1. POWER CHECKS GOOD AT THIS TIME IAW AFM.
RT ENG WOULD NOT ATTAIN POWER WITHOUT EXCEEDING ITT AND N2 LIMITS. TAKE OFF ABORTED. REPLACED RT ENGINE WITH REPAIRED UNIT AND REPLACED RT BDV CONTROLLER WITH REPAIRED UNIT. PERFORMED IAW MM CHAP 75-30-01 AND MM CHAP 71-01-05. PERFORMED ALL ENGINE ADJUSTMENTS AND CHECKS IAW MM CHAP 71-00-00 AND MM CHAP 71-01-05. ALL OPS CHECKS AND LEAK CHECKS GOOD AT THIS TIME.
DURING TAKEOFF ROLL, RT ENGINE ITT CLIMBED TO 700 DEG WHERE AS LT ENGINE STABILILZED AT 650 DEG ABORTED TO ROLL. CONFIRMED RT ENGINE TO GO UP TO 700 DEGREES AND T/O POWER. PERFORMED ALL ELECTRICAL CHECKS TO DETERMINE NR2 ITT INDICATION SYSTEM IS READING TRUE ITT. INSTALLED ALL NEW BLEED AIR LINE GASKETS, SEALS, AND BELLOWS. PERFORMED ENGINE RUNS AT T/O POWER, NO BLEED AIR LEAKS NOTICED. PERFORMED 5 POINT PWR RUNS, UNCAPPED N1 91.5 PERCENT, 700 ITT, 99.2 PERCENT N2. ALL PARAMETERS WITHIN LIMITS AT THIS TIME IAW MM CHAP 5-10-00, 77-20-00, 77-20-00, 75-30-01, 75-00-00 AND MM CHAP 36-12-01.
AFTER T/O THE GEAR WOULD NOT RETRACT. INDICATIONS WERE THREE GREEN, UNSAFE DOOR LIGHT AND GEAR HANDLE UP-GEAR HANDLE WAS PLACED BACK DOWN AND WE HAD THREE GREEN, NO RED.JACKED AIRCRAFT AND FOUND RH OLEO STRUT HANGING UP AND NOT ALLOWING RH SQUAT SWITCH TO CONTACT. REPLACED FAULTY OLEO STRUT WITH CUSTOMER SUPPLIED INSPECTED OLEO STRUT. SERVICED STRUT WITH NITROGEN. CYCLED LANDING GEAR SEVERAL TIMES, OPS TEST GOOD. ALL WORK IAW 560 MM 32-11-02 AND 12-14-01. NOTE: INSTALLED STRUT HAS 781 CYCLES
RT MAIN LANDING GEAR LIGHT WOULD NOT ILLUMINATE. FOLLOWED EMERGENCY CHECKLIST PRIOR TO LANDING. BLEW DOWN W/ EMERGENCY PNEUMATIC AIR. ROTARY TEST VERIFED LIGHT INOPERATIVE. REMOVED AND REPLACED BULB, OPS CHECK GOOD. CYCLED GEAR 10 TIMES AFTER RESETTING BOTTLE. SERVICED BOTTLE AND SAFTIED. GEAR OPS CHECKS GOOD. RESERVOIR AT FULL IAW MM 32-01-00 AND 33-11-01.
AFTER LANDING DURING TAXI, THE FUSIBLE PLUGS BLEW ON THE RT MAIN TIRE. REMOVED AND REPLACED RT MAIN WHEEL AND BRAKE ASSEMBLIES IAW CESSNA 560 MM CHAPTER 32-41-01 AND 32-42-01. INSPECTED AIRCRAFT AND DID NOT FIND ANY DAMAGE, BLED BRAKES AND OPS CHECKED GOOD.
DURING DESCENT FROM 35,000, THE EMERGENCY PRESSURIZATION CAME ON AT ABOUT 18,000 AT 10 DEG AND STAYED ON FOR 3-4 SECONDS.