N818QS
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
VERY DIFFICULT TO SECURE FORWARD CABIN DOOR. MUST USE A LOT OF FORCE TO SECURE MAIN CABIN DOOR. VERIFIED DISCREPANCY ON MAIN CABIN DOOR; DOOR PINS FOUND DRY AND CONTAMINATED. CLEANED DOOR LATCH PINS AND PERFORMED INITIAL OPS CHECK WITH SATISFACTORY RESULTS, THOUGH LUBRICATION WAS NOTED AS REQUIRED. COORDINATED WITH MCC, TEXTRON, AND AQRD REGARDING APPROVED GREASE; MOLYKOTE 6173 IDENTIFIED AS SPECIFIED LUBRICANT, WITH NO APPROVED ALTERNATES FROM OEM. RECEIVED AQRD APPROVAL (RFTS-117683 REV. 0) FOR ALTERNATE USE OF MOLYKOTE 33 MEDIUM EXTREME LOW TEMPERATURE GREASE. GAINED ACCESS TO DOOR PINS AND LUBRICATED LATCH PINS USING MOLYKOTE 33 IAW RFTS-117683 REV. 0. PERFORMED OPERATIONAL CHECK OF CABIN DOOR WITH SATISFACTORY RESULTS; DOOR HANDLE OPERATES SMOOTHLY. CLOSED UP ACCESS AS REQUIRED. WORK PERFORMED IAW CE-700 AMM 12-20-15 AND RFTS-117683 REV. 0. MOLYKOTE 6173 REMAINS ON ORDER.
NO EMER LIGHTS ARE ILLUMINATED WHEN SWITCH IN ON POSITION. C/W MULTIPLE OPS OF THE EMERGENCY LIGHTS. OPS CHECKS ARE GOOD AT THIS TIME IAW CE-700 AMM 33-50-00
SEAT NR 4 EMERGENCY PATH LIGHT INOPERATIVE. REMOVED FAULTY SEAT NR 4 PATH LIGHT FUSE AND REPLACED WITH A CUSTOMER SUPPLIED NEW UNIT, OPS CHECKS.ARE GOOD AT THIS TIME. ALL WORK DONE IAW AMM 33-50-15.
EXCESSIVE VIBRATION/SHUDDER WHILE BRAKING DURING LANDING. IT BECAME WORSE WHILE DECELERATING, THEN LET UP WHEN RELEASING THE BRAKES. RETORQUED #1 AND BOTH NOSE WHEELS. OPS CHECK GOOD. IAW MM 32-40-05. ORIGINAL SUBMISSION DATE: 1/16/2025
MAIN DOOR HANDLE: REPEAT WRITE UP. WHEN CLOSING THE MAIN CABIN DOOR FROM INSIDE THE CABIN THE HANDLE BINDS MIDWAY WHEN LOWERING THE HANDLE TO THE CLOSED POSITION. ADJUSTED ECCENTRIC STRIKERS AS REQUIRED. VERIFIED DOOR GAPS WAS WITHIN LIMITS. VERIFIED DOOR FLUSH MEASUREMENTS WAS WITHIN LIMITS. REF. MM 52-10-00.
MAIN DOOR HANDLE: MAIN CABIN DOOR HANDLE DOES NOT WORK CORRECTLY. WHEN CLOSING DOOR AND PULLING HANDLE DOWN INTO THE LOCKED POSITION THE HANDLE BINDS UP HALF WAY THROUGH ITS NORMAL FULL TRAVEL. EVIDENCE OF METAL ON METAL RUBBING LOCATED NEAR MIDDLE RIGHT LOCKING PIN. PERFORMED DOOR LATCH/LOCK ADJUSTMENT & TEST & DOOR HEALTH CHECK, DATA COLLECTION CHECKLIST, GAINED ACCESS, INSPECTED ALL COMPONENTS, VERIFING DOOR RIGGING IAW AMM 52-10-43. FOUND AFT DOOR HINGE O-RING TORN & HANGING FROM HINGE HOUSING. RESEARCHED AFT DOOR HINGE O-RING. CONTINUED WITH ADJUSTMENT TEST OF DOOR, VERIFIED DOOR HINGE RIGGING, PERFORMED LATCH STRIKER RIGGING, FOUND ALL LATCH STRIKER BOLTS TO BE UNDERTORQUED, FOUND FWD BOTTOM LATCH STRIKER BOLT TO BE UNSERVICEABLE, VERFIED RUB BLOCK RIGGING, VERIFIED DOOR STOP RIGGING, VERIFIED DOOR COUNTERBALANCE RIGGING, VERIFIED STEP ANGLE RIGGING IAW AMM 52-10-00. R & R FWD BOTTOM LATCH STRIKER BOLT. INSTALLED & TORQUED, CONTINUED WITH LATCH STRIKER RIGGING, TORQUED & VERIFIED RIGGING OF ALL REMAINING LATCH STRIKERS. GAINED ACCESS TO DOOR HINGE BOLTS, INSPECTED HINGE BOLTS, LUBRICATED HINGE BOLTS & DOOR PINS. ACCOMPLISHED PRESSURIZATION, LEAK CHECKS AS WELL AS FOLLOW ON CHECKS FOR CABIN DOOR IAW AMM 52-10-00 AND 21-30-00. OPS CHECKED GOOD, NO DEFECTS NOTED.
MAIN CABIN DOOR HANDLE WILL NOT CLOSE ALL THE WAY TO SECURE THE DOOR. HANDLE TRAVELS HALF WAY THEN BINDS UP. ADJUSTED AND SERVICED LATCH DOOR IS OPERATIONAL WITH NO DEFECTS TO NOTE CURRENTLY REF CESSNA 700 AMM 12-20-15MAIN DOOR HANDLE
AFTER TAKEOFF AND CLIMBING THROUGH 3,000' AMBER CAS MSGS CHECK DOORS AND CABIN DOOR OPEN LIGHTS CAME ON. NO PRESSURE LOSS WAS NOTICED AND RETURNED TO DEPARTURE AIRPORT. WHILE TAXIING BACK TO THE RAMP THE AMBER CAS MSG AUTO TEST FAIL ILLUMINATED. PERFORMED A ARES DOWNLOAD AND SENT TO TEXTRON ALSO TROUBLESHOOT CABIN DOOR DID'NT FIND ANY DISCREPANICES AT THIS TIME WAITING FOR ARES DOWNLOAD RESULTS . DJ 04/03/24 CHECKED ALL THE RIGGING ON ALL CABIN DOOR PROXIMITY SWITCHES IAW CE 700AMM 52-70-25. ALL PROXIMITY SWITCHES ARE WLTHIN LIMTS. FUTHER TROUBLESHOOTING I FOUND CABIN DOOR VENT WAS OUT OF RIGGS UMITS. PERFORMED CABIN DOOR LATCH/LOCK SYSTEM RIGGING IAW CE 700 AMM 52-10-43. OPS CHECK NORMAL
AT 3 OR 4 THOUSAND FEET CHECK DOORS AND CABIN DOOR OPEN CAS MESSAGES WERE DISPLAYED. WE RAN THE QRH CHECK AND RETUNED TO SCOTTSDALE. NO CABIN PRESSURE LOSS. REMOVED THE MAIN CABIN STAIRS TO GAIN ACCESS TO THE SC007 PROXIMITY SWITCH TO CHECK THE RIGGING AND ALSO CHECKED THE CONNECTOR AND WIRING FOR DAMAGE. NO DEFECTS FOUND. REMOVED INOP PROXIMITY SWITCH & INSTALLED NEW PROXIMITY SWITCH IAW AMM 52-70-25. OPS CHECK NORMAL. REMOVED INOP HARNESS ASSY CABIN DOOR THRESSHOLD. INSTALLED NEW HARNESS IAW WM 52-70-25 OPS CHECK NORMAL NO. DEFAULTS FOUND.
MAIN DOOR: AFTER T/O THE CABIN DOOR OPEN AMBER CAS AND CHECK DOORS AMBER CAS MESSAGE CAME ON. CHECK LIST WAS RUN AND DOOR VERIFIED CLOSED. ELECTED TO RETURN TO DEPARTURE AIRPORT. ADJUSTED DOOR HANDLE PROX SWITCH. OPS CHECK GOOD. IAW CE-700 AMM 52-10-05
MAIN DOOR: MAIN DOOR WHEN CLOSING FROM INSIDE DOOR HANDLE IS NOT SMOTH CLOSING HANDLE DOWN. IT BINDS AT THE MIDDLE WHEN CLOSING IT. PLEASE EVALUATE THE DOOR. ALSO, (THERE'S A VIDEO ATTACHED TO IT.). TROUBLE SHOT DOOR FOR PROPER OPERATION AND CLEANED BULIT UP DEBRIS FROM MALE AND FEMALE BAYONETS. LUBRICATED AND ACTUATED DOOR SEVERAL TIMES FOR CORRECTION OPERATION NO FURTHER ISSUES WITH DOOR. REFERENCE CE-700 AMM-52-10-12 NO FURTHER DEFECTS NOTED.
CAPTAIN COCKPIT SLIDING WINDOW: CAPTAIN COCKPIT SIDE WINDOW CRACKED WHILE DESCENDING THROUGH 16,000'. REMOVED CRACKED L,H COCKPIT SIDE WINDOW AND INSTALLED NEW WINDOW IAW AMM CH56-10-10
AT ALTITUDE THE FLAPS FAIL AMBER CAS MESSAGE ILLUMINATED. QRH & QRC WERE REVIEWED &COMPLETED. FLAPS 0 LANDING PREFORMED. ACCESSED ARES DATA, FOUND FLAP CONTROL WENT OFFLINE CAUSING ARINC DATA TO STOP BEING TRANSMITTED TO GSD 1 WHICH SET THE FLAP FAIL CAS MESSAGE, FLAP CONTROL PCB REMAINED OFFLINE. ACCESSED ARES DATA, FLAP CONTROL PCB SHOWED NO FAULTS AND REMAINED ONLINE FOR ENTIRE FLIGHT, REMOVED PCB, INSPECTED ALL PINS, SOCKETS, AND PCB NO DISCREPANCIES NOTE. RANG OUT CIB HZ151 FLAP CNTL PCB POWER, & CHECKED FOR VIBRATION & MOVEMENT SENSITIVITY, NO FAULT FOUND. REMOVED INTERMITTENT PCB. & INSTALLED A NEW PCB. ACCOMPLISHED FLAP CONTROL FUNCTIONAL CHECK IAW AMM 27-50-00 FUNCTIONAL CHECKS WAS GOOD.
MAIN DOOR: SHORTLY AFTER TAKEOFF FROM KFLL, CABIN DOOR OPEN AND CHECK DOORS EICAS WAS DISPLAYED, CABIN ALSO STOPPED PRESSURIZING. //SIGNOFF //POWERED AIRCRAFT AND WAS ABLE TO DUPLICATE SQUAWK, GAINED ACCES TO CMC AND VERIFIED SWITCHES OPERATION AND VENT DOOR SWITCH WAS WORKING BUT IT FAIL ONE TIME AND DID NOT FALL AGAIN. GAINED ACCESS TO VENT DOOR AND SWITCH AND FOUND S5 SWITCH TO HAVE EXCESSIVE GAP. RESEARCHED A.M.M. AND MEASURED A GAP OF .180 AND MANUAL STATE THAT SHOULD BE .10. READJUSTED S5 VENT DOOR SWITCH AS REQUIRED AND ALSO FOUND VENT DOOR NOT CLOSING COMPLETLY. RIGGED VENT DOOR AS REQUIRED. PERFORMED GOOD OPERATIONAL CHECK WITH THE ACCESS OPEN. CLOSED ACCESS BY REINSTALLING CABIN DOOR STEPS AND TRIM PANELS. PERFORMED OPERATIONAL CHECK OF STEP ENTRY LIGHTS, OPS CHECK GOOD. PERFORMED OPERATIONAL CHECK OF CABIN DOOR, NO DEFECTS NOTED AT THIS TIME. WORK ACCOMPLISHED IN REFERENCE WITH CE 700 AMM CH 52-10·00 , 52-70--25, 52-10-43..
ENGINE CONTROL FAULT L CAS, LEFT ENGINE CONTROL FAULT CAME ON DURING FINAL APPROACH. RAN THE CHECKLIST AND WILL NOT RESET. ENGINE STUCK AT 67 PERCENT N1 AND WILL NOT IDLE ON FLARE, HAD TO SHUT DOWN ENGINE. PERFORMED LEFT ENGINE DOWNLOAD AND SENT FOR REVIEW. DOWNLOAD REVEALED LEFT EEC OVERTEMP FAULT CODE. INSPECTED LEFT ENGINE FOR BLEED AIR LEAK AND FOUND ONE FITTING DISCONNECTED. REPLACED THE SEALS AND RECONNECTED THE FITTING. REPLACED THE LEFT EEC AND PERFORMED ENGINE RUNS AND LEAK CHECKED SATISFACTORY, NO FAULT CODES PRESENT IAW EMM 73-20-03 AND AMM 36-00-00.
LT TRAILING LINK INNER BORE HAS LARGE AREA OF CORROSION AND AXLE IS HEAVILY CORRODED. FOUND WHILE PERFORMING TASK 32-11-02-210 MAIN LANDING GEAR INSP AND TASK 32-30-00-210 MLG TRAILING LINK INTERNAL BORE INSP. AS PART OF THE PHASE 5 INSPECTION. REMOVED AND REPLACED.
BRAKES CATCH & GRIND DURING ROLLOUT & COMING TO A STOP. BRAKES CATCH & GRIND DURING ROLLOUT & COMING TO A STOP. TAXI CHECKED AND VERIFIED DISCREPANCY. PERFORMED COMPLETE ANTI-SKID BRAKE SYSTEM BLEED, PERFORMED TAXI CHECK AND OPS AND LEAK CHECKED GOOD. BRAKE MODULATION & ACTIVATION IS GOOD. DONE IAW MM 32-42-00.
AT 41,000FT, A SLIGHT ELECTRICAL ODOR WAS NOTICED. WALKING TOWARDS THE BACK OF THE PLANE, THE ODOR WAS NOTICEABLY MUCH STRONGER STARTING AT THE CABIN DOOR AND MOVING AFT. RAN ENGINES AT IDLE AND POWER SETTINGS WITH BLEED AIR ON AND OFF, ADJUSTED CABIN AND COCKPIT TEMP. TO FULL HOT AND FULL COLD NO UNUSUAL ODOR NOTED. HAD ALL POWER ON. AVIONICS ON. GALLEY POWER ON. CABIN AND COCKPIT LIGHTING ON, EMER LIGHTING ON AND CABIN ENTERTAINMENT ON FOR SEVERAL HOURS DURING RUNS AND THEN FOR SEVERAL HOURS IN THE HANGER NO ELECTRICAL ODOR NOTED. COULD NOT DUPLICATE. GROUND RAN AIRCRAFT FOR INSPECTION RUN. NO DEFECTS NOTED. NO FURTHER TROUBLESHOOTING NEEDED PER AMCC.
FREON AIR CONDITIONER WAS WORKING ON PREVIOUS FLIGHT. WHILE INVESTIGATING A ELETRICAL BURNING ODOR ON GROUND, DISCOVERED THE FREON AIR CONDITIONER TO BE INOPERATIVE AND LIKELY THE CAUSE OF THE ODOR. OPERATED SYS MOTOR FAILED TO RUN. FOUND OPEN FUSE LIMITER IN J-BOX AND EVIDENCE THAT MOTOR FAILED. R & R A/C MOTOR. SERVICED REFRIDGERANT. LEAK AND OP CHECKED GOOD. WORK DONE IAW MM 21-52-00.
GEAR EXTENDED ON APPROACH. GOT 2 GREEN AND NO RT MAIN GEAR INDICATOR BUT NO RED LIGHT. PERFORMED "LANDING GEAR WILL NOT EXTEND" CHECKLIST WHICH REQUIRES GEAR BLOWDOWN. PERFORMED ROTARY TEST (UNSUCCESFUL). DID NOT GET ANY AURAL TONE. AFTER LANDING ALL 3 LIGHTS WERE ILLUMINATED UPON TAXI IN.
ON APPROACH EXTENDED GEAR. RECEIVED TWO GREEN AND NO RT GEAR INDICATIONS & NO RED LIGHTS. PERFORMED "LANDING GEAR WILL NOT EXTEND" CHECKLIST WHICH REQUIRES GEAR BLOWDOWN. PERFORMED UNSUCCESFUL ROTARY TEST . DID NOT GET AURAL TONE. AFTER LANDING ALL 3 LIGHTS ILLUMINATED ON TAXI IN. R & R RT MAIN & NOSE GEAR INDICATOR BULBS IAW MM 33-11-01. PERFORMED FULL LANDING GEAR FUNCTIONAL TEST & SERVICE IAW MM 32-01-00. GEAR WARNING HORN FUNCTION CORRECT IAW CONFIGURATION. OPS & LEAK CHECKED GOOD.
AUTOPILOT TRANSFERRED COPILOT, PILOTS SIDE ATTITUDE INDICATOR SHOWS DISCREPANCY WITH COPILOTS SIDE. INDICATES 2.5 DEGREES LOW IN CLIMB, 1 DEGREE LOW LEVEL FLIGHT. CHECKED FOR CURRENT CODES ON AIP SYS, NO CURRENT CODES AT THIS TIME. PERFORMED AHRS HEADING, PITCH AND ROLL FUNCTIONAL TEST. NO DEFECTS NOTED. PERFORMED AHRS LEVELING PROCEDURE. OPS CHECKED NORMAL. WORK DONE IAW MM 34-21-16.
STBY GYRO DISPLAYED "EXT MANUV" ANNUNCIATOR AND SHOWED A 10 DEGREE RT BANK AND HEADING PRECESS OF MORE THAN 180 DEGREES. HEADING PRECESS ABOUT 10 DEGREES EVERY 2 MINUTES. REPLACED STANDBY GYRO (SECONDARY FLIGHT DISPLAY) WITH REPAIRED UNIT, OPS CHECKED NORMAL. WORK PERFORMED IAW THE MM 34-21-17.
AT FL410 STBY, GYRO SHOWED 6 DEGREE LT BANK, AND HEADING MISCOMPARE OF APPROX 120 DEGREES. (HEADING OF 330 THEN SLOWY MOVED TO 030). PLANE HEADING WAS 084. ALSO EXT MANUVER ANNUNCIATOR WAS ON. OPS CHECKED NORMAL. PERFORMED RESISTANCE CHECK OF FUSE. FUSE NORMAL. REMOVED STINGER & INSPECTED WIRING AND MAGNOMETER. NO DEFECTS. REMOVED DISPLAY. CONNECTOR PLUG BACKSHELL BROKEN. REINSTALLED COMPONENTS. R & R MAGNOMETER WITH REPAINTED UNIT. OPS CHECKED NORMAL. REMOVED DISPLAY. INSTALLED NEW BACKSHELL. REINSTALLED DISPLAY. OPS CHECKED NORMAL. WORK DONE IAW WDM 34-10-03.
UPON TAXING OUT GOT LOW BRAKE PRESS/ANTISKID INOP ANNUCIATOR WITH THE POWER BRAKES CIRCUIT BREAKER POPPED. RESET, 20 SECONDS LATER THE POWER BRAKES CIRCUIT BREAKER POPPED AGAIN. R & R HIGH AND LOW PRESSURE SWITCHES AT CUSTOMER REQUEST. R & R BRAKE MOTOR RELAY. OPS AND LEAK CHECKS GOOD. BLED BRAKE SYS IAW M & M 32-42-05 AND 32-42-00.
ON CLIMBOUT AND AT A FLAPS SETTING OF 7 DEGREES, A NEAR MISS CAUSED A FLAP OVERSPEED OF APPROX 40 KNOTS. COMPLIED WITH CESSNA 'OVERSPEED CHECK'. NO DEFECTS NOTED. INSPECTED IAW MM CH 5-50-00. PERFORMED TRAVEL CHECKS ALSO. TRAVELS GOOD. WORK IAW MM TASK 27-57-00-714
AFTER TAKE OFF THE LANDING GEAR WOULD NOT RETRACT. THE GEAR DID NOT EVEN COME OUT OF THE LOCKS, WE HAD 3 GREEN THE ENTIRE TIME. WE CHECKED THE CB'S AND NONE WERE TRIPPED. JACKED AIRCRAFT AND SWING GEAR SEVERAL TIMES. WE HAD HYD. PRESSURE LIGHT. THE THREE GREENS EXTINGUISHED AND CAME ON AT APROPRIATE TIMES. GEAR SWINDS WERE NORMAL, COULD NOT DUPLICATE DISCREPANCY. WORK DONE IAW MM 32-30-00.
ON ARRIVAL, THE "LT" GEAR DOWN INDICATION LIGHT DID NOT ILLUMINATE. JACKED ACFT, RESET EMERGENCY BLOW-DOWN BOTTLE. REMOVED AIR FROM SYSTEM. FOUND ROTARY KNOB WOULD NOT TEST. REPLACED ALL (4) LAMPS. SWITCH TEST NORMAL. PERFORMED GEAR SWINGS SEVERAL TIMES. ALL INDICATIONS ARE NORMAL.