N805QS
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
AFTER DEPARTING KMDW WHEN ATTEMPTING TO RETRACT LANDING GEAR, GEAR HANDLE WAS STUCK IN DOWN POSITION. A FEW SECONDS LATER, WE RECEIVED AN AMBER GROUND DETECT FAULT AMBER CAS MESSAGE. MESSAGE REMAINED ON FOR ENTIRE FLIGHT AND WE DID NOT ATTEMPT ANY MORE GEAR RETRACTIONS. NOSE GEAR WOW TAB APPEARS TO HAVE POSSIBLE DAMAGE RELATED TO PREVIOUS WRITE UP. MEASURED NLG STRUT IAW AMM 12-20-10 AND FOUND TO BE 9.75 WITH NO SERVICING NEEDED AND NO DEFECTS NOTED. ALL OPS CHKD GOOD. INSPECTED ALL NLG WIRING FOR DAMAGE WITH NO DEFECTS. RANG OUT NLG WOW SWITCH & FOUND SWITCH INTERMITTENT. REMOVED FAILED SWITCH & INSTALLED A NEW SWITCH IAW AMM 32-60-10. OPS CHKD GOOD.
AMBER DOOR CLOSED LED ON MAIN CABIN DOOR INOP. THE AMBER DOOR LED TURNS OFF WHEN THE DOOR IS CLOSED WITH THE DOOR HANDLE IN THE OPEN POSITION. THE AMBER LED TURNS OFF WHEN THE DOOR IS ABOUT HALF WAY UP. CORRECTIVE ACTION: REMOVED HARNESS ASSY CAB DOOR THRESHOLD PN 8250171-1 AND INSTALLED A NEW HARNESS ASSY CAB DOOR THRESHOLD PN 8250171-1. REF: MODEL 700 MAINTENANCE MANUAL 52-10-00. NO FURTHER DEFECTS NOTED AND OPS CHECK IS GOOD.
LH & RH ENGINE UPPER AND LOWER THRUST REVERSER DOORS HAVE EVIDENCE OF CORROSION.....LH & RH ENGINE UPPER AND LOWER THRUST REVERSER DOORS HAVE EVIDENCE OF CORROSION. LEFT T/R UPPER AND LOWER PIVOT DOORS INNER SURFACE PAINT REMOVED I.A.W. CITATION STANDARD PRACTICES MANUAL (REV 7) 20-50-00 4.C.(2). BLENDED CORROSION ON L/H 7 RH UPPER & LOWER T/R DOOR REF SAFRAN CMM 35L0012-35L0013 SERIES 78-30-04. READY FOR NDT. NDT PERFORMED BY TOLEDO JET CENTER LLC. CRS# 2TJR420B ON WORK ORDER TOL84109. REMAINING MATERIAL THICKNESS VERIFIED FOR REFERENCE AND REPAIR. NO DEFECTS NOTED. COMPLIED WITH RFTS-111267, REV. 0, DATED: 12JUL2024, TITLE: R/H AND L/H THRUST REVERSER BUCKET SKIN CORROSION. COMPLETED PAINT ON UPPER AND LOWER TR DOORS I.A.W. CE-700 C.S.P.M. 20-50-00.
EMERGENCY LIGHTS DO NOT PASS PREFLIGHT TEST. NO LIGHTS COME ON IN THE ARM SWITCH POSITION, BUT THEY DO LIGHT IN THE ON POSITION. REMOVED AND REPLACED THE LT FWD EMERGENCY BATTERY PACK. BEFORE TECH COULD PERFORMED BATTERY CHARGING PROCEDURE ENCOUNTER BATTERY COLD L/R FAULT WHICH TRIPPED THE REMOTE CBS TURNING OFF MAIN BATTERIES, ENABLED BATTERY HEATERS TO HEAT BATTERIES IN ORDER TO POWER ON A/C. ONCE POWER WAS FINALLY APPLIED TO A/C, CHARGED EMER BATTERY PROCEDURE THEN PERFORMED OPS CHECK. OPS CHECK IS GOOD. CLOSED UP ALL ACCESS PANELS. ALL WORK ACCOMPLISHED IN REF TO 33-50-07 AND 33-50-00.
NO EMERGENCY LIGHTS ILLUMINATE WITH EMERGENCY LIGHT SWITCH IN ON POSITION. POWERED ON AC AND ALLOWED ALL SYSTEMS BOOT UP AS REQUIRED. PERFORMED OPS CHECK, OPS CHECK FAILED, CONFIRMED DISCREPANCY. ACCESSED #3 & #4 BATTERY PACKS. REPOSITIONED #3 BATTERY POWER SUPPLY ASSY IAW CUSTOMER REQUEST. INSTALLED SERVICEABLE BATTERY POWER SUPPLY ASSY IAW AMM 33-50-05. REPOSITIONED #4 BATTERY POWER SUPPLY ASSY IAW CUSTOMER REQUEST. INSTALLED SERVICEABLE BATTERY POWER SUPPLY ASSY IAW AMM 33-50-05. PERFORMED AND FOUND OPERATIONAL TEST SATISFACTORY. ACCOMPLISHED TC-FLT-33-1001 TO SUPPLEMENT MX. ITEM GOOD TO RTS. 15DEC2023
MAIN DOOR: REPEAT WRITEUP: AMBER CABIN DOOR OPEN CAS MESSAGE DISPLAYED DURING CRUISE FLIGHT. DOOR PINS VERIFIED TO BE CLOSED. NO NOISE OR CHANGE IN CABIN PRESSURE. ///SIGNOFF/// TECHS FOUND THAT ELECTRICAL CONNECTOR PCOSS TO BE LOOSE AND CAUSING AN INTERMITTENT DISCONNECTION OF THE S6 SWITCH AS INDICATED BY THE INTERNAL LED SWITCHING ON AND OFF WHEN THE CONNECTOR WAS MANIPULATED. REMOVED PCOSS AND VISUALLY INSPECTED CONNECTOR AND PINS WITH NO DISCREPANCIES NOTED. REINSTALLED CONNECTOR AND VERIFIED RIGGING OF THE S6 SWITCH IAW CE700 52-70-25 WITH NO DISCREPANCIES NOTED. CLOSED ACCESS TO THE S6 SWITCH AS REQUIRED. PERFORMED THE CABIN DOOR LIFT MOTOR AND WARNING SYSTEM TEST (POWER OFF, BATTERIES CONNECTED) IAW CE700 MM 52-70-00 WITH NO DISCREPANCIES NOTED. PERFORMED THE CABIN DOOR LATCHING/LOCKING SYSTEM AND DOOR WARNING SYSTEM TEST (POWER OFF, BATTERIES CONNECTED) IAW CE700 MM 52-70-00 WITH NO DISCREPANCIES NOTED. PERFORMED THE CABIN DOOR WARNING SYSTEM TEST (POWER ON, BATTERIES CONNECTED) IAW CE700 MM 52-70-00 WITH NO DISCREPANCIES NOTED.
PERFORMING THE EMERGENCY LIGHT BATTERY OPS CHECK, FOUND THAT THE EMERGENCY LIGHT SWITCH , WORKS INTERMITTENTLY. REMOVED OVERHEAD CONTROL PANEL AND INSPECTED THE SWITCH AND FOUND EMERGENCY LIGHT SWITCH WIRING CONNECTOR THAT WASNT LOCK DUE TO WORN OUT CLIP.
EMERGENCY LIGHTS BATTERY: ON POWER ON CHECKS EMERGENCY LIGHTS DO NOT ILLUMINATE IN ARM OR ON POSITION // SIGNOFF// REMOVED FAILED #3 EMER LIGHT BATTERY P/N: CBS28-1, S/N: 000152 AND REPLACED WITH A CUSTOMER SUPPLIED REPAIRED BATTERY P/N: CBS28-1 1 S/N: 007340. REMOVED FAILED #4 EMER LIGHT BATTERY P/N: CBS28-1, S/N: 005586 AND REPLACED WITH A CUSTOMER SUPPLIED REPAIRED BATTERY P/N: CBS28·1, S/N: 007306. ALL REF CE700 AMM 33-50-05. TESTED EMER LIGHTS NORMAL REF CE700 AMM 33-50-00.
MAIN DOOR: CABIN MAIN ENTRY DOOR OPENS NORMALLY THEN PAUSES AFTER 12" OF TRAVEL.. DOOR WILL MANUALLY OPEN REMAINDER OF TRAVEL//CORRECTIVE ACTION//REMOVED THE CABIN DOOR LIFT MOTOR DUE TO DOOR NOT OPENING SMOOTHLY. INSTALLED A REPAIRED NJA SUPPLIED GEAR MOTOR PERFORMED VARIOUS SUCCESSFUL OPERATIONAL CHECKS. WORK DONE IN TO CE-700 AMM 52-15-05. NO DEFECTS NOTED.
CABIN EMERG LIGHT: DURING PREFLIGHT CHECKS, THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE WHEN POWERED BY THE EMERGENCY BATTERIES. // SIGNOFF// PERFORMED EMERGENCY LIGHTS OPERATIONAL CHECK, NO DISCREPANCIES NOTED AT THIS TIME. ALL WORK PERFORM PER CESSNA 700 AMM 33-50â¢00,
MAIN DOOR: MAIN CABIN DOOR RESISTS OPENING FROM INSIDE OR OUTSIDE . REQUIRES PHYSICAL FORCE TO OPEN - DOES NOT GRAVITY FALL. // SIGNOFF// OPS CHECK DOOR AND FOUND SATISIACTORY, NO RESISTANCE OPERATING DOOR FROM INSIDE OR OUTSIDE IAW CE 700 MM 52-00-00
FLAPS FAIL AMBEER CAS: AMBER FLAPS FAIL CAS ILLUMINATED INFLIGHT, FLAPS WOULD NOT RESET, LANDED WITH 0 FLAPS. DOWNLOADED ARES DATA AND SENT TO TEXTRON FOR EVALUATION. HAD TO SEND EACH FILE INDUVIAL, WOULD NOT SENT MORE THAN ONE AT A TIME. ASSISTED WITH OPEN UP, OPERATIONAL CHECKS, AND CLOSE UP. VERIFIED COTTER KEY INSTALLATION ON LEFT FLAP POSITION SENSOR. REMOVED LEFT INBD FLAP LVDT P/N GM13339 S/N 1214 AND INSTALLED NEW LEFT INBD FLAP LVDT P/N GM13339 S/N 1305 OPS CHECKED GOOD IAW 27-50-00 AMM REMOVED FLAP MONITOR PCB P/N 7468162-5 S/N 0117 AND INSTALLED NEW FLAP MONITOR PCB P/N 7468162-5 S/N 0151 OPS CHECKED GOOD IAW 24-60-20 AMM.
ALL EMERGENCY LIGHTS (EXIT SIGNS, LIGHTS OVER SEATS, WING INSPECTION LIGHTS) ARE ILLUMINATED WITH ALL POWER OFF. WE TRIED TO RESET THE SWITCH UNDER PILOT'S SEAT TO NO AVAIL. RESET RT FWD EMERGENCY EXIT BATTERY PACK, LIGHTS EXTINGUISHED APPLIED POWER TO A/C. ACCOMPLISHED EMERGENCY LIGHTING ADJUSTMENT TEST, NO DEFECTS WERE NOTED. ACCOMPLISHED REF: CE700MM 33-50-00.
WHEN BRAKING NOTHING HAPPENS UNTIL BRAKE HYD PRESSURE GAUGES READ 200 PSI THEN BRAKES GRAB HARD. SEEMS THE CAPTAINS BRAKE PEDALS ARE BAD, CO-PILOT'S SIDE BRAKES SEEM NORMAL.REMOVED AND REPLACED BRAKE CONTROL VALVE. ALL WORK DONE IAW MM.
WHEN BRAKING, NOTHING HAPPENS UNTIL PRESSURE GAUGE READS 200PSI THEN BRAKES GRAB HARD. THIRD WRITEUP. RECEIVED OH MAXARET P/N AC65216 S/N 58268 & NEW MAXARET P/N AC65218 THROUGH NJA SUPPLY. REMOVED AND REPLACED EXISTING MAXARET NR 1 P/N AC65218 S/N 022CJ, NR 2 AC65216 P/N S/N GX189. INSTALLED MAXARET S/N 58268 ON NR 1 AND S/N 58268 ON NR 2. PERFORMED OP CHECK OF BRAKE SYSTEM. OPS CHECK WAS GOOD. ALL WORK ACCOMPLISHED IAW H-800XP MM CH 32-40-101
BRAKES FEEL MUSHY AFTER LANDING AND DURING TAXI. REPLACED NR 1 AND 2 BRAKE ASSEMBLIES. BLED SYSTEM. OPS CHECKED OK IAW HAWKER 800XP M.M. 32-40-00
TEN MINUTES AFTER STARTING APU, SMOKE, SPARKS, AND FLAME CAME OUT OF APU PANEL. IT STOPPED AFTER APU SHUTDOWN AND POWER WAS SHUT OFF, NO EXTINGUISHER WAS USED. INSPECTED AREA AND FOUND THE APU CONTROL PANEL BURNT. REPLACED WITH NEW PANEL IAW PATS INC HAWKER 800XP GTCP36-150W MM CHAPTER 49-11-00, OPERATIONAL CHECKED SATISFACTORY.