N601QS
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
WEAR AND CORROSION ON RT MLG TRAILING LINK PIN FOUND DURING MAIN LANDING GEAR TRUNNION, TRAILING LINK, AND LINK PIN DETAIL INSPECTION.
WEAR AND CORROSION ON LT MLG TRAILING LINK PIN FOUND DURING MAIN LANDING GEAR TRUNNION, TRAILING LINK, AND LINK PIN DETAIL INSPECTION
EMERGENCY LIGHT OVER SEAT 7 DOES NOT ILLUMINATE WITH THE EMERGENCY LIGHT SWITCH IN ARM OR ON. THE LIGHT WILL ILLUMINATE WITH THE READING LIGHT SWITCH. ALL OTHER EMERGENCY LIGHTS OPERATE NORMALLY. WITH EMER LIGHTS ON, WHEN MOVING THE CONNECTOR THE LIGHT WOULD FLICKER ON AND OFF. SEEMED LIKE ONE OF THE RECEPTORS ON THE READING LIGHT SIDE OF THE CONNECTOR WAS POTENTIALLY BENT OPEN SLIGHTLY. REMOVED LEFT CABIN SIDEWALL PANEL. REMOVED AND REPLACED SEAT #7 READING LIGHT. RESECURED LEFT SIDEWALL PANEL REF CE-680A IMM 25-20-23 PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM IAW CE-680A AMM 33-50-00. PERFORMED OPERATIONAL SYSTEM OF THE PAX READING LIGHTS IAW CE-680A AMM 33-20-00. ALL OPS CHECKS ARE GOOD AT THIS TIME PN/SN ON 9919171-1/202300000038212, PN/SN OFF 99191714-1/273007258.
SEVERAL AREAS OF CORROSION ON UPPER VERTICAL STAB R/H SIDE BELOW TIP CAP. PERFORMED MAJOR PERMANENT REPAIR OF AREA IAW AQRD RFTS-116135 REV 0 & AQRD ERO-988077 REV IR.
ENERGENCY LIGHTS ARE INOPERATIVE: OVERHEAD LIGHTS OVER SEATS 3 & 7, LIGHT UNDER SEAT 3. ATTEMPTED CHARGING IAW QRH, NO IMPROVEMENT. MAIN POWER ON, LIGHT UNDER SEAT 3 WOULD ILLUMINATE WHILE 2 OVERHEAD LIGHTS REMAINED OFF. WITHOUT MAIN POWER. NONE OF THE 3 LIGHTS WOULD WORK. R & R NR 1, 2, 3, & 4 POWER SUPPLIES WITH NEW IAW AMM 33-50-06. OPS CHKD IAW AMM 33-50-00, LIGHTS ABOVE SEATS 3 & 7 INOP. REPLACED NR 7 SEAT LIGHT WIRING IAW 5PM 20-30-15 & IWM 25-92-08. REPLACED NR 3 LIGHT CONNECTOR IAW SRM 20-30-15 & IWM 25-92-08. REPAIRED NR 3 SEAT LIGHT WIRING IAW IWM 25-92-08. CONDUCTED AN OPS CHK OF EMERGENCY LIGHTS, NO DEFECTS NOTED REF AMM 33-50-00.
FUEL PRESS LOW L AMBER CAS MESSAGE DISPLAYED IN FLIGHT. MESSAGE CYCLED REPEATEDLY UNTIL THE L BOOST PUMP WAS TURNED ON PER THE QRH. CORRECTIVE ACTION: REMOVED AIRFRAME FUEL PRESSURE SWITCH P/N 9914488-3 S/N 1927564 INSTALLED NEW SWITCH S/N 2315974 OPS CHECK GOOD IAW CE680A AMM CHAPTER 28-40-20. REMOVED ENGINE FUEL PRESSURE SWITCH P/N 9914488-2 S/N 1931819 INSTALLED NEW SWITCH S/N 2430772 OPS CHECK GOOD IAW CE680 AMM CHAPTER 73-10-05. COMPLIED WITH SATISFACTORY OPERATIONAL AND LEAK CHECKS. CLOSED AND SECURED COWLS.
DURING THE EMERGENCY LIGHTS TEST, WHEN PLACING THE SWITCH TO EMER LIGHTS ARM, NO EMERGENCY LIGHTS ILLUMINATE. PRIOR DAY HAD TO CHARGE THE LIGHTS PER THE CHECKLISTS. CORRECTIVE ACTION; REPLACED FAULTY #1 EMER LIGHT BATTERY PACK !AW CE-680A AMM CH. 33-50-06. CHARGED BATTERY FOR 2 HOURS, PERFORMED OPERATIONAL CHECK IAW CE-680A AMM CH. 33-50-00, OPS CHECK GOOD. CHARGED BATTERIES ONCE AGAIN FOR 2 HOURS POST OPS CHECK. NO FURTHER ACTION REQUIRED.
ENGINEERING MEMO DQ31487M1 RIGHT WING CUFF PANEL DAMAGE (IMPACT) DATED 9/14/2021.
MAIN DOOR HANDLE: MAIN CABIN DOOR HANDLE WILL NOT OPERATE WHEN RED BUTTON IS PUSHED. INSPECTED MED FOUND BINDING IN THE HANDLE + OXIDATION ON THE PINS. ACCESSED MED STAIRS + COVER PANEL INSPECTED ALL MECHANICAL CONNECTIONS. NO FAULTS NOTED. CLEANED THE OXIDATION ON THE PINS. LUBED PINS.
FUSELAGE ATTACH FITTINGS: AFTER GEAR/FLAP RETRACTION FROM ORL, WE FELT A VIBRATION THROUGH THE FUSELAGE BETWEEN 500-700 FEET MSL. DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. (UPDATE/CORRECTION TO SDR-ATC DECLARED AN EMERGENCY ON THE CREWS BEHALF). JACKED UP AIRCRAFT. HOOKED UP HYDRAULICS AND RETRACTED GEAR. FOUND R/H MLG DOOR LOOSE, ADJUSTED AS NECESSARY. ALL LANDING GEAR DOORS FIT CHECK GOOD WITH GEAR RETRACTED. WORK PERFORMED IAW CE680A MM 52-80-25. PERFORMED ANTI-SPIN FUNCTIONAL CHECK, NO DEFECTS NOTED. WORK PERFORMED IAW CE680A MM 32-42-00.
MED HANDLE IS DIFFICULT TO OPERATE. SIGN OFF. LUBED AND OPERATED HANDLE SEVERAL TIMES WITH NO DEFECTS NOTED, ALL WORK IAW CE-680A 5PM 20-40-00.
MAIN CABIN DOOR IS "HANGING UP" OR BINDING INTERMITTENTLY WHEN THE HANDLE IS IN THE FULL UP POSITION WHEN ATTEMPTING TO PUSH DOWN TO CLOSE. THE DOOR FUNCTIONS NORMALLY FROM THE OUTSIDE. PERFORMED SERVERAL OPS CHECKS OF MAIN CABIN DOOR IAW CE-680A AMM 52-10-00 OPS CHECK GOOD, DOOR HANDLE NEVER BINDED AND DOOR OPERATED SMOOTH WITH NO BINDING. COULD NOT DUPLICATE
MAIN DOOR DID NOT OPEN/CLOSE - MAIN CABIN DOOR WILL NOT CLOSE AND LATCH FROM INSIDE AIRCRAFT. //SIGNOFF// OPERATIONAL CHECK OF THE CABIN ENTRY DOOR COMPLETED NUMEROUS TIMES WITH NO DISCREPANCIES NOTED. ACOUSTIC DOOR SEAL CLEANED AND INSPECTED FOR CLEANLINESS. MAIN CABIN DOOR EDGES WERE CONTACT IS MADE WITH ACOUSTIC SEAL DURING DOOR CLOSING INSPECTED FOR ANY DISCREPANCIES WITH NONE FOUND. WORK COMPLETED IAW CESSNA 680A AMM 52-20-00. DOOR OPERATIONAL CHECK NORMAL
AFTER TAKEOFF & GEAR RETRACTION, GEAR UNLOCK & HYD PRESS ANNUNCIATOR LIGHTS REMAINED ON. ALL NORMAL INDICATIONS AFTER SELECTING GEAR DOWN. JACKED ACFT & PERFORMED EXTENSION & RETRACTION TEST IAW AMM 32-30-00. PERFORMED UP LOCK INSPECTION & TEST IAW AMM 32-30-05, ALL CHECKS WERE NORMAL. ADJUSTED LT UP LOCK SWITCH IAW AMM 32-61-00. SERVICED NLG STRUT IAW AMM 12-14-00. LUBED & CLEANED ALL UP LOCKS IAW AMM 12-21-02. PERFORMED ADDITIONAL EXTENSION & RETRACTION OF LG & ALL CHECKS WERE GOOD AT THIS TIME.
DURING A SCHEDULED INSPECTION THE ELEVATOR TRIM CABLE WAS FOUND TO BE FRAYED BEYOND LIMITS. THIS CABLE ASSY IS LOCATED WHERE THE CABLE TRANSITIONS FROM A VERTICAL RUN TO THE HORIZ AT A PULLEY LOCATED IN THE HORIZ STABILIZER. HAVE SEEN NUMEROUS WITH THIS SAME CONDITION. A SERVICE CONDITION REPORT HAS BEEN SENT TO MFG UNDER NR 613657.
CLIMBING THRU 3000 FT, RT RED OIL PRESSURE ANNUCIATOR ILLUMINATED WITH A MASTER WARNING. RT OIL PRESSURE GAUGE WENT TO ZERO. INITIALLY OIL TEMP GAUGE WAS IN NORMAL RANGE, THEN UNABLE TO CAPTURE OIL TEMP READING. BURNING ODOR IN CABIN WITH NO VISIBLE SMOKE. PERFORMED PRECAUTIONARY SHUTDOWN ACCORDING TO EMERGENCY CHECKLIST. ON POST FLIGHT STILL HAD BURNING ODOR OUTSIDE THE ACFT AND OIL WAS IN ACCEPTABLE RANGE ON SIGHT GAUGE. NO OIL DRIPS NOTICED.
AFTER COMPLETING EMERGENCY GEAR EXTENSION CHECKLIST NOTICED "BRAKE PRESS LO" & "ANTI SKID INOP" ANNUNC ILLUM. ACFT LANDED USING EMEGENCY BRAKE SYS. CHECKED FOR DAMAGE OR BRAKE FLUID LOSS & FOUND INTACT & RESERVOIR FULL. APPLIED POWER & BRAKE PRESS LO & ANTI SKID INOP LIGHTS ILLUM. CYCLED BRAKE CIRCUIT BREAKERS & NO CHANGE. ACCESSED RELAY KN003 & FOUND POWER 28 VOLTS PRESENT AT A1. POWER AT X1, NO GROUND SIGNAL. JUMPED A1 & A2 & VERIFIED BRAKE MOTOR OPS. REMOVED MLG CONTROL HANDLE & OHM'D PINS D & E & FOUND OPEN. VERIFIED ACFT GROUND GOOD PIN E. REPLACED MLG HANDLE & TESTED BRAKE SYS, FOUND TO OPS NORMAL. BLED BRAKES IAW MM 32-44-00. RAN ACFT & CHECKED BRAKES WITH & WITHOUT ANTI-SKID ENABLED. OPS NORMAL.
LT MLG BECAME STUCK IN THE UPLOCK POSITION WHEN SELECTED GEAR DOWN AT 12500 FT MSG FOLLOWING EMERGENCY/ABNORMAL CHECKLIST, Z3 DID NOT CORRECT UNSAFE LIGHT OR LT MAIN GEAR INDICATION OFF. ABOUT 7 MINS LATER UPLOCK LET LOOSE AND GEAR EXTENDED, OK. ACCOMPLISHED MLG SYS ADJ/TEST IAW MM CH 32-01-00 REV 22. TASK 32-01-00-720. NO DEFECTS NOTED IN THE OPERATION OF LT DOWNLOCK SWITCH OPS CHECKED OK. PANEL REMOVED LT MLG ACTUATOR IAW MM 32-30-04 REV 26. ROUTED TO HYD SHOP TO CHANGE SWITCH. REMOVED SWITCH CORE TO BE GIVEN WITH REO TAG. INSTALLED MLG ACTUATOR IAW MM 32-30-04. LEAK/OPS CHECK GOOD. ADDITIONALLY ACCOMPLISHED LANDING GEAR FT IAW MM CH 32-01-00. OPS CHECK GOOD.
MAIN LEFT LANDING GEAR BECAME STUCK IN THE UP LOCK POSITION WHEN SELECTED GEAR DOWN.
WHEN THE LANDING GEAR WAS LOWERED THE RT DOWN AND LOCKED LIGHT DID NOT ILLUMINATE, RES (UNLOCK) LIGHT REMAINED ON, BLED HYDRAULICS SYSTEMS ON AIRCRAFT IAW MM 32-30-00, 27-50-00, 27-40-00, AND 27-60-00. OPS CHECKS GOOD.
AFTER TAKEOFF RECEIVED ACM OVERHEAT INDICATION WITH RT BLEED AIR AND RT ITT (RED FLAG) INDICATION, ALSO HAD A ODOR OF SOMETHING BURNED COMING OUT OF THE VENTS ITT WAS APPROXIMATELY BETWEEN 750-760 DEG F FOR 4-5 SECONDS. [07-09-07] REMOVED AND REPLACED THE RT FLOW CONTROL VALVE W/A OVERHAULED UNIT AS PER THE CE560XL AMM CHAPTER 21-11-00. OPS CHECKS GOOD. LEAK CHECK SATISFACTORY
DURING ENGINE START, LT ENGINE OIL PRESSURE WOULD NOT COME OUT OF THE RED . AFTER APPROX 15 SEC ITT CLIMBED TO 680 DEG C AND THEN SHOT UP TO 800 DEG C FOR 2-3 SECS . AS SOON AS ITT WENT PAST 720 DEG START WAS ABORTED . ITT WAS NOT AT 800 DEG C FOR MORE THAN 3 SECS. MOTORED ENGINE FOR 30 SEC AFTER ABORT. ITT DROPPED BELOW 720 DEG C AS SOON AS START WAS ABORTED AND CONTINUED TO DROP WILE LT ENGINE WAS MOTORED . INSPECTED LT ENGINE AND OIL LEVEL WAS NORMAL. COMPLIED WITH DCU DOWNLOAD OF LT ENGINE, SENT DOWNLOAD INFO TO PWC FOR INTERPROLATION, PWC REPORT NO EXCEEDANCES AT THIS TIME. P&WC RECOMMENDS STARTING & GROUND RUNNING ENGINE TO CHECK OPERATION. COMPLIED WITH THESE RECOMMENDATIONS ENGINE OPS CKS GOOD PER
DURING TAKEOFF ROLL, PILOTS (LEFT SIDE) PFD WENT BLANK (NO RED X). TAKEOFF WAS ABORTED. AFTER CLEARING RUNWAY DISPLAY RETURNED TO NORMAL. ITEM IS UNDER INVESTIGATION.
NOSE GEAR FAILED TO EXTEND OR LOCK WHEN GEAR SELECTED DOWN. RED UNSAFE LIGHT ON AND NOTICABLE VIBRATION. RECYCLED AND ALL 3 GEAR POSITION LIGHTS CAME ON. LANDED WITHOUT INCIDENT. REMOVED AND INSTALLED A NEW NOSE GEAR UPLOCK ACTUATOR. OPS AND LEAK CHECKS GOOD AT THIS TIME. ALL WORK DONE IAW CESSNA 560XL MM CHAPTER 32-30-05.
AFTER GEAR RETRACTION NOSE WHEEL INDICATOR LITE REMAINED ON. ALL INDICATIONS WERE THAT NOSE GEAR WAS RETRACTED. NORMAL EXTENTION FOLLOWED BY PRECAUTIONARY BLOW DOWN. - COULD NOT DUPLICATE DISCREPANCY. CYCLED GEAR 20 TIMES PERFORMED TIME CYCLE TEST. NOTE: LANDING GEAR BREAKS LOOSE LAST DURING RETRACTION CYCLE. ALL INDUCTIONS ARE NORMAL PER CE 560 XL M/M CHAPTER 32-01-00.
AFTER GEAR RETRACTION NOSE WHEEL INDICATOR LIGHT REMAINED ON. ALL INDICATIONS WERE THAT NOSE GEAR WAS RETRACTED. NORMAL EXTENSION FOLLOWED BY PRECAUTIONARY BLOW DOWN. ITEM IS UNDER INVESTIGATION.
LANDING GEAR FAILED TO RETRACT ON T/O. HANDLE WAS DIFFICULT TO MOVE OUT OF DOWN POSITION; THEN, WHEN ABLE TO MOVE IT UP, NOSE GEAR GREEN LIGHT REMAINED ON WITH MAIN GEAR GREEN LIGHTS OFF AND INTRANSIT LIGHT ON. SELECTED DOWN POSITION AND GOT NORMAL INDICATION. PERFORMED SEVERAL GEAR SWINGS AND FOUND ALL LANDING GEAR OPERATIONS AND INDICATIONS TO BE NORMAL WORK PERFORMED IAW CE560XL MM 32-30-00.
RIGHT FIRE LIGHT ILLUMINATED MOMENTARAILY FOR A FEW SECONDS DURING CRUISE. WENT OUT WHEN POWER WAS REDUCED. REPLACED RT FIRE DETECTOR LOOP WITH NEW REF 560 XL CH 26-11-01. OPERATIONAL CHECK SATISFACTORY.