N582QS
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
DURING DECENT APPLIED SPEED BRAKE HANDLE TO CONTROLL SPEED. THEN THE AMBER CAS HYD VOLUME LOW MESSAGE APPEARED. DECLARED EMERGENCY AND FOLLOWED THE QRH TO AN UNEVENTFUL LANDING. PERFORMED & SUBMITTED AN ARES DOWNLOAD, ON INLTIAL WALK AROUND FOUND HYD FLULD DRIPPING FROM LT ENGINE DRIVEN HYD PUMP DRAIN, MOST FWD DRAIN LINE. CURRENTLY NO HYD LOW MSG & QTY SHOWS MAX OUT AT 700 ON BOTH EICAS & ANALOG GAUGE AT SERVICE PORT . PERFORMED VISUAL INSP OF HYD SYSTS FOR LEAKS IAW MM 29- 00-00, NO LEAKS NOTED. VERIFIED THE HYDRAULIC RESERVOIR VOLUME INDICATOR & POTENTIOMETER FOR CORRECT OPS, NO DEFECTS NOTED IAW MM 29-30-00. REMOVED HYD RESERVOIR ACCUMULATOR. INSTALLED OVERHAULED UNIT IAW MM 29-10-45. SERVICED ACCUMULATOR & RESERVOIR . PERFORMED BLEEDING CHECKS. DURING BLEEDING CHECKS, LT EDP DRIPPING HYD FLULD, 1 DRIP EVERY 10 SECS, 1 DRIP EVERY 3 SECS WITH HYD PRESSURE. REGARDLESS OF AIR OR PRESSURE IN SYS, ALLOWABLE LEAK RATE FOR LT EDP IS 1 DRIP EVERY 2 HRS. EDP REPLACED. PERFORMED AIRCRAFT JACKING AND GEAR SWINGS TO BLEED THE MLG. PERFORMED ENG RUNS OPS AND LEAK CHECKS, NO DEFECTS HYD SYS BLEEDING & SERVICE IS COMPLETED. ALL IAW AMM 29-00-00.
RED AUTO THROTTLE HOLD FAIL CAS CAME ON AT 30KTS ON TAKEOFF AND THE AUTO THROTTLES WERE REDUCING POWER AS THIS OCCURRED. PERFORMED TWO SETS OF OPS CHECKS SUCCESSFULY AND SENT AN ARES DOWNLOAD TO MCC AND TEXTRON. MCC ELECTED TO KEEP ORIGINAL A/T INSTALLED DUE TO PILOT INDUCED FAULT. REF. AMM 22-30-05
FUSELAGE STRUCTURE: REPEAT RIGHT UP. THERE IS A VERY PRONOUNCED AIRFRAME VIBRATION. THE VIBRATION BEGINS AT VARIOUS ALTITUDES MORE OFTEN AT FL260 AND 295KTS. THE VIBRATION REMAINS AT ANY ALTITUDE UNTIL SLOWING TO 250 KN. AT 250 KN THE VIBRATION SLOWLY DISSIPATES AS THE AIRSPEED DECREASES. THERE IS ALSO A VERY LOW HUMMING SOUND LIKE A PROPELLER BEATING.. THE VIBRATION CAN BE FELT IN THE CONTROLS, ON THE GLARE SHIELD AND ON THE AIRFRAME WALLS AND THE RUDDER PEDALS. IT HAS BECOME MORE PRONOUNCED OVER THE LAST THREE FLIGHTS. REPEAT WRITEUP. CORRECTIVE ACTION; FOUND NOSE DOOR FWD LH EDGE NOT FLUSH, ADJUSTED DOOR WITH IN LIMITS IN REF TO CE-680A AMM 52-8-05, ALSO FOUND RH WINDSHIELD HUMP SEAL DETERIORATED AND REQUIRED NEW SEALANT, COMPLETED HUMP SEAL APPLICATION IN MULTIPLE AREAS IN REF TO CE-680A AMM 56-10-00
FLOOR EMERG EXIT LIGHT: RIGHT HAND MAIN DOOR FLOOR EXIT LIGHT INOP. //SIGNOFF// RECONNECTED LOOSE WIRE OF RH MAIN DOOR EXIT EMERG LIGHT. WORK IN REF TO CE680A AMM 33-50-00. OPS CHECK GOOD.
WITH ALL AIRCRAFT POWER REMOVED AND EMER LIGHT SWITCH IN THE OFF POSITION THE EMER LIGHTS AT MAIN CABIN DOOR AREA AND BELOW SEAT 10 REMAIN ILLUMINATED. CYCLED THE EMER LIGHT SWITCH AND AIRCRAFT POWER AND PROBLEM REMAINS. UPON ARRIVAL, ALL. EMER LIGHTS DISGUISHED. OPS OF EMER LIGHTING SYSTEM ON POWER UP NORMAL C/W TCâ¢FLT-33-1001 OPERATING APU WITH THE EMER LIGHT SWITCH IN OFF FOR 60 MINUTES TO CHARGE BATTERIES. NO DEFECTS NOTED. ON POWER DOWN EXIT LIGHT ABOVE MAIN CABIN DOOR STAYED ILLUMINATED, ALONG WITH AISLE LIGHTING AND KICK-PANEL. RESET NR 1 INERTIA SWITCH AND DISTINGUISHED EMER LIGHTS. PERFORMED EMER LIGHTING INSPECTION CHECK. CHECKED NORMAL IAW AMM 33-50-00. . ORIG SUB DATE: 12/27/2022
EMERG EXIT SIGN/LIGHT: ON POST FLIGHT THE EMER EXIT SIGN OVER THE MAIN CABIN DOOR AND THE FLOOR LIGHTING INDER SEAT 10 IS ILLUMINATED. // SIGNOFF// RESOLUTION: ARRIVED AT AIRCRAFT IN TIME VERIFYING FWD ERNER BATT LIGHTS STILL ILLUMINATED. ACCESSED AS NECESSARY AND RESET FWD EMER BATT G SWITCH TRIPPED. RESET SWITCH IAW CE680A MM CH.33-50-11 NOTING LIGHTS EXTINGUISHED. PERFORMED EMGER LIGHTS OPS CHECK
L/H UPPER COWL GOUGED BY O/B BLEED AIR CLAMP AT AFT BLEED AIR COUPLING. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34079M1, DATED. MARCH 22,2022. 680A-0138 (N582QS) ENGINE UPPER COWL (LEFT AND RIGHT) DAMAGE (GOUGE).
R/H UPPER COWL GOUGED BY O/B BLEED AIR CLAMP AT AFT BLEED AIR COUPLING. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34079M1. DATED. MARCH 22, 2022. 680A-0138 (N582QS) ENGINE UPPER COWL (LEFT AND RIGHT) DAMAGE (GOUGE).
RH MLG ACTUATOR UPPER ATTACH FITTING GOUGED FROM CONTACT WITH ACTUATOR LUG. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ34051M1, DATED: MARCH 21, 2022. 680A-0138 (N528QS) RIGHT MAIN LANDING SIDE BRACE ACTUATOR INBOARD FITTING CHAFE DAMAGE.
FLOOR EMERG EXIT LIGHT: FLOOR LIGHT UNDER SEAT 10 WILL NOT EXTINGUISH. THE 3 EXIT SIGNS ON MAIN CABIN DOOR ALSO WON'T EXTINGUISH "CORRECTIVE ACTION" FOUND FWD "G" SWITCH ON THE R/H AFT CENTER PEDESTAL TO BE TRIPPED. RESET SWITCH AND STATED EMERGENCY LIGHTS EXTINGUISHED. TESTED IAW CE-680AS AMM CH 33-50-00
REPAIR TO NOSE LANDING GEAR WHEEL WELL CRACKS. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 06/01/2020, STANDARD REPAIR-CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75 WITH FAA FORM 8100-9 DATED 06/01/2020.
COCKPIT ODOR - CLIMBING THROUGH 300FT TURNED ENGINE ANTI ICE ON AND NOTICED A FUME SMELL ABOUT 500FT. TURNED ENGINE ANTI ICE OFF AFTER ABOUT 2 MINUTES WHEN WE CLIMBED ABOVE THE THIN CLOUD LAYER. SMELL DID SEEM TO DISSIPATE A LITTLE BUT WAS STILL VERY NOTICEABLE. WE DONNED OUR O2 MASKS AND COULDN'T TELL IF THE SMELL FURTHER SUBSIDED. WE DID NOT HAVE TIME TO ISOLATE THE ISSUE. // SIGNOFF //COCKPIT ODOR-CLIMBING THEOUGH 300FT TURN RESEARCHED PREVIOUS SCHEDULED WORK ORDER 124821 AND FOUND GRAFOIL SEALS INSTALLED IN BOTH LH AND RH ENGINE BLEED AIR LINES FOR PREVIOUS LEAK.RAN AIRCRAFT, NOTICED A LIGHT ODOR AFTER TURNING AIR SOURCE ON. ODOR CLEARED FAIRLY QUICKLY, NO FUMES NOTED. RAN BOTH ENGINES THRU VARIOUS POWER SETTINGS TO PURGE SYSTEM. NO ODOR OR FUMES PRESENT. CYCLED LH AND RH ANTI-ICE SYSTEMS AND NO DEFECTS NOTED. VERIFIED OPERATIONAL CHECKS OF LH AND RH BLEED AIR SOURCES GOOD. VERIFIED ANTI-ICE SYSTEMS OPERATIONAL CHECKS GOOD. WORK DONE IAW 680A M/M 36-10-00 AND 30-20-00.STOWED PILOT AND CO-PILOT O2 MASKS. SERVICED 02 SYSTEM IAW 680A M/M CH12-10-60 RAN COCKPIT AND CABIN ENVIRONMENTAL SYSTEM FROM FULL COLD THRU FULL HOT SETTINGS WITH NO ABNORMALITY NOTED. SYSTEM OPS CHECK GOOD IAW 680A M/M 21-20-00.
LEFT MAIN LANDING GEAR FAILED TO RETRACT. DOWN DISPLAYED IN YELLOW ON LEFT MAIN. UP DISPLAYED IN WHITE ON RIGHT MAIN AND NOSE GEAR. UPON COMPLETION OF CHECK LIST THREE DOWN GREEN INDICATION RESULTED IN A SAFE UNEVENTFUL LANDING. R&R MLG UPLOCK SWITCH P/N 6948101-3