N632QS
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
Maintenance disclosures
EMER LIGHTS DON'T TEST PROPERLY. BATTERY PACKS 1 AND 3 DON'T ILLUMINATE ANY LIGHTS AFTER 2 30 MINUTE CHARGE SESSIONS. REMOVED NR 1 EMER LIGHT BATTERY PACK AND INSTALLED A NEW NR 1 EMER LIGHT BATTERY PACK, REMOVED NR 2 EMER LIGHT BATTERY PACK AND INSTALLED NEW NR 2 EMER LIGHT BATTERY PACK, REMOVED NR 3 EMER LIGHT BATTERY PACK AND INSTALLED A NEW NR 3 EMER LIGHT BATTERY PACK IAW AMM 33-50-10. OPS CHECK NORMAL
AMBER CAS "CHECK DOORS" AND "CABIN DOOR OPEN" WILL NOT EXTINGUISH AFTER DOOR CLOSED AND QRH PROCEDURES COMPLETED. AMBER DOOR OPEN LIGHT ON CABIN DOOR STAYS ILLUMINATED WITH DOOR HANDLE ENGAGED. CORRECTIVE ACTION: REPLACED MAIN CABIN DOOR LATCH PAWL PROXIMITY SWITCH. OPERATIONAL CHECK OF MAIN CABIN DOOR GOOD CURRENTLY WITH NO FURTHER DEFECTS TO NOTE.
CORROSION AROUND AFT AND FWD NUTPLATES ON PANEL 316DBC AND 316CBC MOUNTING FLANGES
LEFT FLAP EXTENSION: DURING APPROACH IN DESCENT AT 6000' FOR 4000' AIRSPEED 230 INDICATED. FLAPS SELECT TO 1 AND FAILED BETWEEN 0 AND 1. FLAP FAIL QRH AND FLAPS INOP LANDING QRH ACCOMPLISHED. CARRIED OUT INSPECTION OF FLAP PDU/ ACTUATORS, FLEX SHAFTS, CONTROLER, POSITION SENSOR AND RELAY BOX I/A/W CESSNA 680A 27-50-50 C/O FLAP CONTROL SYSTEM T/S AND FOUND FLAP CONTROLLER FAULT CODE 2 ILLUMINATED. PERFORMED FLAP SYSTEM RESET PROCEDURE I/A/W CESSNA 680 AMM 27-50-00 AND CLEARED FAULT CODE. PERFORMED FLAP MOVEMENT CHECK I/A/W CESSNA 680A MM 27-50-00 MULTIPLE FULL CYCLES AND NO FAULT CODES PRESENT. NO FLAP FAIL CONDITION ANYMORE IN EICAS DISPLAY. FLAP SYSTEM OPERATIONAL CHECK SERVICEABLE
PASSENGER COMPARTMENT EQUIPMENT: STRONG OILY ODOR IN CABIN, WHEN ENGINES RUNNING. MOST PRONOUNCED ON POWER REDUCTIONS AND LOW POWER SETTINGS NO SMOKE PRESENT. PERFORMED TC-68A-21-181006M, BOROSCOPED LH AND RH ENGINES AND BLEED DUCTS COMING OFF ENGINES FOR OIL OR OIL RESIDUE WITH NONE NOTED. LEAK CHECKS SATISFACTORY. WORK DONE IAW EMM 72-00-00. NO OTHER DEFECTS NOTED.
APU SMOKE: AFTER APU START THE ENTIRE PLANE, COCKPIT AND CABIN, FILL WITH SMOKE. HIGHLY RECOMMEND CLEANING ENTIRE INTERIOR BEFORE PUTTING CREW OR PAX BACK ON PLANE. // SIGNOFF // REMOVED APU P/N 3800785-1 S/N P-879 DUE TO SMOKE IN CABIN, IAW CE-680A MM 49-10-00 INSTALLED REPAIRED APU P/N 3800785-1 S/N P-833 WITH 2676.8 HRS AND 3492 CYCLES DUE TO SMOKE IN CABIN, OPS CHECK GOOD LEAK CHECK GOOD JAW CE-680A MM 49-10-00. PERFORMED LONG APU RUN W/ BLEED AIR ON AND NO SMOKE NOTED. CLOSED ALL PANELS, TOROUE WRENCH: JE0899, OK TO CONTINUE.
MLG: AFTER TAKEOFF, NOSE GEAR DID NOT RETRACT. A HATCHED NOSE GEAR LIGHT APPEARED WITH A "GEAR DISAGREE N" CAS MESSAGE. WE RAN THE APPROPRIATE CHECKLIST AND LANDED WITH NO FURTHER INCIDENCE. // SIGNOFF// IVISUALL Y INSPECTED THE LANDING GEAR, NO DEFECTS NOTED. PERFORMED ARIES DOWLOAD SUBMITTED TO TEXTRON. PLACED THE AIRCRAFT ON JACKS AND PERFORMED MULTIPLE GEAR SWINGS WITH NO DEFECTS NOTED. CONTACTED MANUFACTURER AND DISCUSSED FURTHER ACTION TAKEN. AFTER REVIEW OF THE ARIES DOWNLOAD TEXTRONS RECOMMENDATION IS TO REPLACE INLG UPLOCK SWITCH. REMOVED AND REPLACED THE NLG UPLOCK SWITCH IA W CE-680A AMM 10. PERFORMED SEVERAL GEAR SWINGS WITH NO DEFECTS NOTED. LOWERED THE AIRCRAFT REMOVED THE JACKS.
EMERGENCY EXIT LIGHT ABOVE THE CABIN DOOR REMAINED ON AFTER SHUTDOWN. SIGNOFF. REMOVED CENTER PEDESTAL PANEL 224BR TO GAIN ACCESS TO THE NR 1 EMERGENCV INERTIAL SWITCH. ONCE SWITCH WAS RESET THE CABIN DOOR EMERGENCY EXIT LIGHT TURNED OFF. PERFORMED OP CHECK OF THE EMERGENCV LIGHTING. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED. REINSTALLED PANEL 224BR. ALL WORK DONE, IAW CE680A AMM 33-50-11.
RIGHT MLG LANDING GEAR RETRACTION DID NOT RETRACT - ON GEAR RETRACTION WE HAD AMBER GEAR DISAGREE LIGHT WITH THE RIGHT MAIN NOT RETRACTED CYCLED DOWN IAW CHECKLIST PROCEDURE AND RETURNED TO DEPARTURE AIRFIEL
RIGHT MLG LANDING GEAR RETRACTION DID NOT RETRACT - ON GEAR RETRACTION WE HAD AMBER GEAR DISAGREE LIGHT WITH THE RIGHT MAIN NOT RETRACTED CYCLED DOWN IAW CHECKLIST PROCEDURE AND RETURNED TO DEPARTURE AIRFIELD *** CORRECTIVE ACTION *** INTERROGATED ARES DATA. FOUND FAULT ON 5/13/2020 WAS DUE TO RH GEAR UPLOCK SWITCH NOT BEING MADE. JACKED AIRCRAFT AND CYCLED GEAR. COMPLETED MULTIPLE GEAR SWINGS, UNABLE TO DUPLICATE FAULT. DISCONNECTED CANNON PLUG PG002 MAIN GEAR PLUG AND METERED PINS 24 AND 25 AND READ OPEN WHEN SWITCH WAS ACTUATED (FAIL) THEN METERED PINS 25 AND 26 WHEN THE SWITCH WAS NOT ACTUATED READINGS SHOWED .5 OHMS(GOOD), THEN METERED PINS 27 AND 28 READ .5 OHMS(GOOD) WHEN SWITCH WAS ACTUATED THEN METERED PINS 28 AND 29 AND READINGS SHOWED .5OHMS(GOOD) WHEN SWITCH WAS NOT ACTUATED. THEN TO ENSURE THAT IT WAS NOT WIRING WE DISCONNECTED PG008 RH MAIN LANDING GEAR UPLOCK SWITCH AND TOOK ALL READINGS AGAIN PINS A AND B (PINS 24 AND 25 ON PG002) THE SWITCH STILL READ OPEN WHEN SWITCH WAS ACTUATED. AFTER LEAVING THE METER CONNECTED AND DEPRESSING THE SWITCH IN RAPID SUCCESSION THEN CONTACTS WOULD INTERMITTENTLY READ .7 OHMS THEN AFTER A FEW MORE ACTUATIONS THE READINGS WOULD READ OPEN SWITCH IS CONFIRMED BAD. REMOVED SWITCH P/N 65-430087 S/N N/A. INSTALLED REPLACEMENT SWITCH P/N 65-430087 S/N N/A. ACCOMPLISHED RIGGING AND OPERATIONAL CHECKS. NO FAULTS FOUND DURING OPERATIONAL CHECKS. WORK DONE IAW MODEL 680A MAINTENANCE MANUAL REV. 11 CH.32-32-25-4
AFTER TAKE OFF THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. CYCLED THE GEAR DOWN, LIGHT EXTINGUISHED. [SUP 05-03-07] FOUND NOSE GEAR NOT SEATING IN UPLOCK. JACKED AIRCRAFT AND PERFORMED NOSE GEAR STRUT SERVICING PROCEDURE IAW CE560XL MM 12-14-00. PERFORMED SEVERAL GEAR SWINGS, AND LANDING GEAR AND GEAR INDICATION OPS CHECK NORMAL. NO DEFECTS NOTED.
RECEIVED A NO TAKEOFF MESSAGE AROUND 40KTS, ABORTED TAKEOFF. FOUND ELEVATOR TRIM INDICATOR STRIP AND PROX SWITCH FOR NO TAKEOFF SYSTEM OUT OF ADJUSTMENT. ADJUSTED ELEVATOR TRIM STRIP INDICATOR AND PROX SWITCH IAW CH 27-31-00 OF THE CE 560 XL M.M. OPS CHECKS GOOD.
DURING CRUISE FLIGHT FROM FNL TO PWA, CREW DETECTED THE SMELL OF ENGINE OIL COMING FROM THE GASPERS. THE OIL SMELL WAS INTERMITTENT AND STRONG. IRRITATION TO EYES, THROAT AND NOSE WAS REPORTED BY CREW MEMBER. TROUBLESHOOTING SUSPECTS L ENG, RAN A/C TO CRUISE FOR 45 MIN. NO OIL SMELL DETECTED. HAD SLIGHT OIL SMELL ON ENGINE STARTS ONLY. NEED TO CLEAN WATER SEPARATOR SOCK. C/W IAW MM 12-19-02, CLEANED SOCK FOR ACM AND REINSTALLED.
AFTER T/O, GEAR WOULD NOT RETRACT WITH GEAR HANDLE IN UP POSITION. RECYCLED HANDLE ONCE AND GEAR STILL WOULD NOT RETRACT. ELECTED TO LEAVE GEAR DOWN. NEVER GOT AN UNLOCK LIGHT. SHORTLY BEFORE LANDING, EMERG BLEW "BLOW DOWN" BOTTLE AS A SAFETY PRECAUTION. JACKED A/C. ATTEMPTED GEAR CYCLE AND FOUND GEAR INOP. T/S GEAR CONTROL SYSTEM. REMOVED GEAR CONTROL HANDLE AND FOUND DEBRIS INHIBITING GEAR HANDLE SWITCH OPERATION. CLEANED DEBRIS FROM GEAR HANDLE SWITCHES. INSTALLED GEAR CONTROL HANDLE. PERFORMED GEAR OPS CHECK. L/G OPS CHECK GOOD. DOWNJACKED A/C. RESET AND SAFETIED GEAR NITROGEN BOTTLE. SERVICED EMERG GEAR NITROGEN BOTTLE. WORK PERFORMED REF, CE560XL MM CHAP 12-13-01, 32-01-00 AND 32-30-01.
PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT WING AILERON CABLES IAW CESSNA 560XL MM CHAPTER 27-10-03.
DURING APPROACH TO HXD FOUND NOSE LANDING GEAR WOULD NOT COME DOWN, DIVERTED TO SAV. AIRCRAFT LANDED WITH NLG PARTIALLY EXTENDED. ITEM IS UNDER INVESTIGATION.
REPORT 110840, INSPECTED WHEEL WELL AREAS LT AND RT, FOUND THE LT WHEEL WELL LINES TO BE OK AT THIS TIME. RT WHEEL WELL BRAKE LINE ASSY , PN 6627100-34 AND THE FLAP RETRACT LINE ASSY PN 6627000-68, TO BE CHAFED BEYOND ALLOWABLE LIMITS STATED IN MM. REMOVED AND REPLACED BOTH LINES WITH NEW AND PERFORMED OPS AND LEAK CHECKS
WHILE PERFORMING NJA'S ONE TIME INSPECTION OF THE HYDRAULIC/PNEUMATIC LINES IN THE WHEEL WELLS, FOUND THE RT EMERGENCY BRAKE LINE CHAFED THROUGH, AND FLAP RETRACT LINE CHAFED BEYOND LIMITS. - REMOVED AND REPLACED DEFECTIVE HYDRAULIC AND PNEUMATIC LINES IAW CESSNA 560XL MM CH 27-51-00 AND 32-42-09, SYSTEM OPS AND LEAK CHECKED GOOD.