N653QS
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
LH HORIZONTAL STAB UPPER SKIN 3 SPOTS OF CORROSION FWD OF PANEL 351AC. FIX... COMPLIED WITH RFTS 117040 DATED 24APR26 AND REF CE 680A CSPM CH 20-50-00 TO NETJETS STANDARDS.
CROSSFEED INOP BOTH DIRECTIONS. RECONNECTED WIRE. OPS CHECK GOOD. IAW AMM 28-20-00 AND 28-20-55.
NOSE GEAR FAILED TO RETRACT ON DEPARTURE. RAN CHECKLIST. BLOWDOWN BOTTLE USED. CORRECTIVE ACTION: REMOVED FAILED NLG POWER STEERING SYSTEM PN:9914650-2 SN:0452, INSTALLED CUSTOMER SUPPLIED OVERHAULED NLG POWER STEERING SYSTEM PN:9914650-2 SN:0191. OPERATIONAL AND LEAKS CHECKS ARE GOOD REF CE680 AMM 32-50-00.
ENROUTE AT 43,000FT WE GOT FUEL FILTER BYPASS R CAS MESSAGE. REMOVED GEA 7100 #3 P/N 011-02635-00 S/N 28Y005869. INSTALLED CUSTOMER SUPPLIED REPAIRED GEA 7100 011-02635-00, PERFORMED SOFTWARE CONFIGURATIONS AS REQUIRED. PERFORMED HIGH POWER ENGINE RUN WITH NO DEFECTS NOTED. OPERATIONAL CHECKS SATISFACTORY AT THIS TIME. WORK PERFORMED IN REF TO AMM 31-40-15.
FUEL FLTR BYPASS R CAS MESSAGE APPEARED IN FLIGHT. QRH CHECKLIST WAS EXECUTED. NO OTHER SYMPTOMS OR FAULTS APPEARED. REMOVED RH FUEL FILTER AND INSTALLED NEW FUEL FILTER, MX IAW PWC 306D 73-10-03. NO FUEL FILTER BYPASS CAS AT THIS TIME. PN:30B6653-01 FILTER KIT RAN RH ENGINE - OPS & LEAK CHECKS - GOOD AS WELL AS CHANGING THE FUEL FILTER WE FOUND THE PE017 PLUG AT THE FUEL BYPASS SWITCH TO HAVE RESIDUAL OIL IN THE PLUG CONNECTION. REMOVED PLUG AND CLEANED BACKSHELL AND RESECURED AS REQUIRED. MX IAW PWC 306D MM 73-10-03.
FUEL FLTR BYPASS R AMBER CAS: FL360 FUEL FILTER BYPASS R AMBER CAS ILLUMINATED. REPEAT WRITE UP .
GEAR DISAGREE R AMBER CAS: ON GEAR RETRACTION THE AMBER CAS GEAR DISAGREE R DISPLAYED. THERE WAS AN ASSOCIATED AMBER X OVER THE GEAR POSITION INDICATOR. RAN THE QRH AND RETURNED TO LAND. PERFORMED THREE POINT JACKS. SWAPPED RT AND LT MLG DOWNLOCK SWITCH TO VERIFY IF THE GEAR DISAGREE R CAS MESSAGE TRANSFERED TO THE LH SIDE. REMOVED FAULTY RT MLG DOWNLOCK SWITCH. INSTALLED A NEW RT MLG DOWNLOCK SWITCH IAW AMM 32-30-15.
NLG LANDING GEAR RETRACTION: UPON DEPARTING HCR LANDING GEAR WOULD NOT RETRACT. RAN APPROPRIATE QRH. MATCHED HANDLE TO INDICATION 3 GREEN. HAD ASSOCIATED WOW MISCOMPARE AMBER MESSAGE.//CORRECTIVE ACTIONS//REMOVED SUSPECTED FAULTY NOSE SQUAT SWITCH PN: 6948001-2 SN: NSN AND INSTALLED NEW NOSE SQUAT SWITCH PN: 6948001-2 SN: NSN REF CE680A MM 32-60-10. JACKED AIRCRAFT IAW CE680A MM 07-10-10. PERFORMED NOSE SQUAT SWITCH RIGGING REF CE680A MM 32-60- 00 .. OPERATIONAL CHECK GOOD. AFTER WE RECEIVED THE UPPER NOSE LANDING GEAR HARNESS PN: 8469800-2. CONTACTED MCC TO DISCUSS IF THEY WOULD LIKE US TCI REPLACE THE UPPER HARNESS AS WELL. PER MCC, IT WAS DECIDED TO REPLACE THE UPPER NOSE LANDING GEAR HARNESS DUE TO MAN POWER AND TOOLING AVAILABILITY. GAINED ACCESS TO AND REMOVED SUSPECTED FAULTY UPPER NOSE LANDING GEAR HARNESS PN: 8469800-2 SN: NSN AND INSTALLED NEW UPPER NOSE LANDING GEAR HARNESS PN: .8469800-2 SN: NSN USING 2 EA. GROMMETS PN: MS35489-141REF CE680A MM 32-20-00. PERFORMED LANDING GEAR OPERATIONAL CHECK IAW CE680A MM 32-00-00 WITH NO DEFECTS OR FAULTS NOTED. NLG HARNESS CLEARANCE CHECKS GOOD. PERFORMED OPERATIONAL CHECK OF TAXI LIGHTS IAW CE680A MM 33-40-00 WITH AND NOTED NLG RH TAXI LIGHT BULB ELEMENT BURNT OUT, SEE DISCREPANCY 6.1 FOR DETAILS. PERFORMED POWER STEERING CONTROL UNIT OPERATIONAL CHECK REF CE680A MM CH.32-50-00. OPERATIONAL CHECKS GOOD. DOWN-JACKED AIRCRAFT IAW CE680A MM CH.07-10-10. SQUAT SWITCH PN OFF/ON: 6948001-2 NSN NLG HARNESS PN OFF/ON : 8469800- NSN
FIRE DETECT FAIL L AMBER CAS: DURING DESCENT IN TURBULENCE FIRE DETECT FAIL L AMBER CAS MESSAGE ILLUMINATED MULTIPLE TIMES BETWEEN FL240 AND 11000 FEET. REMOVED, INSPECTED AND CLEANED BOTH INNER AND OUTTER FIRE LOOP CONNECTORS. FOUND NO ISSUES WITH EITHER CONNECTIONS. REINSTALLED CONNECTORS AND OPS CHECKED FIRE SYSTEM AND OPS CHECKED GOOD. CONTACTED MCC ROBERT AND ADVISED HIM OF NO FAULT FOUND, HE APPROVED SIGN OFF. ALL WORK WAS DONE IAW CE-680A AMM 31-3~00 AND P&W MM 26-10-01
CABIN DOOR OPEN AMBER CAS: CABIN DOOR LIFTING FUNCTION WOULD NOT WORK AND WE HAD THE AMBER CAS "CHECK DOORS" AND AMBER CAS "CABIN DOOR OPEN". WENT THROUGH THE QRH RESET PROCEDURE WITH MCC. WE COULD GET THE DOOR PHYSICALLY CLOSED BUT WE STILL HAS A WHITE "CHECK DOORS" CAS AND AN AMBER "CABIN DOOR OPEN" CAS. (PRE-FLIGHT)// SIGNOFF// CW CED MOTOR RESET PROCEDURE, CLOSED CED AND VERIFIED SQUAWK, REMOVED CED MONITOR PCB PT# 7468101-17 SN 0368 AND INSTALLED NEW CED MONITOR PCB PT# 7468101-17 SN 0417, CW 3 CYCLES OF THE CED FROM THE INSIDE OF AC AND 3 CYCLES FROM THE OUTSIDE OF THE AC, JET AC SIT FOR 1 HOUR AND CW 3 MORE CYCLES FROM THE INSIDE OF AC AND 3 MORE CYCLED FROM THE OUTSIDE OF AC IA W CE-680A MM CH 24-60-40 OP'S CK GOOD.
MAIN DOOR WILL NOT CLOSE WITH ELECTRIC POWER. POWER DOWN AND RESTART ATTEMPTED, PER AFM. DOOR STILL WILL NOT CLOSE. SIGNOFF. GAINED ACCESS TO AIRCRAFT AND PERFORMED VARIOUS OPERATIONAL CHECKS SUCCESSFULLY. DOWNLOADED ARES FILES AND SENT THEM TO TEXTRON FOR REVIEW, PER TEXTRON DOOR LIFT SWITCH IS WORKING INTERMITTENTLY OR THERE IS A WIRING ISSUE. TECH'S PERFORMED GVI INSPECTION OF THE INTERIOR DOOR LIFT SWITCH AND RESEATED ELECTRICAL CONNECTOR. PERFORMED VARIOUS DOOR CYCLES USING BOTH HE EXTERIOR AND INTERIOR DOOR SWITCHES WITH NO DEFECTS NOTED. NO MAINTENANCE IS REQUIRED DUE TO TECHS NOT BEING ABLE TO DUPLICATE SQUAWK. WORK DONE, IAW CE-680A AMM 52-15-00, NO DEFECTS NOTED.
AFTER TAKEOFF WHEN GEAR UP WAS SELECTED THE GEAR RETRACTED NORMALLY FOLLOWED BY AN AMBER LEFT GEAR DN INDICATION, AN AMBER GEAR DISAGREE L, AND AMBER ADC SSEC MISCOMPARE. CLIMB WAS CONTINUED TO 10,000' WITH IAS REMAINING BELOW 200KTS. WHEREUPON THE QRH AMBER MESSAGE PROCEDURE E4 AND X2 WERE ACCOMPLISHED. THE EMERGENCY/ABNORMAL PROCEDURE N2 WAS CONSULTED THEN COMPLETED UPON ARRIVAL AT THE DESTINATION RESULTING IN NORMAL GEAR EXTENSION AND INDICATIONS FOLLOWED BY AN UNEVENTFUL LANDING. RANG OUT THE LEFT HAND LANDING GEAR SQUAT, DOWN LOCK, AND UNLOCK SWITCHES. SWITCHES RANG CORRECT IN AIR AND ON GROUND MODE WITH NO DEFECTS NOTED. ALL SWITCHES ARE WORKING AS NORMAL. WE ALSO RANG OUT ALL AIRFRAME GROUNDS FROM THE THREE SWITCHES AND ALL CHECKED GOOD. WE CLEANED EACH CONNECTOR WITH CONTACT CLEANER. PERFORMED FUNCTIONAL TEST WITH THE IN-AIR SIMULATOR TEST BOXES, SYSTEM OPERATED AS NORMAL. REMOVED TEST BOXES AND PERFORMED MULTIPLE GEAR SWINGS AND NO CAS MESSAGES. TEAM SAID THAT THE FAULT CODE 1019 CAME FROM THE LEFT MLG SQUAT SWITCH SAYING THAT WITH THE GEAR HANDLE SELECTED UP THE SQUAT SWITCH STILL SHOWED IT ON THE GROUND. ADVISED SENSE THE SQUAT SWITCH IS WHAT THREW THE FAULT TO BEGIN WITH THEY WOULD RECOMMEND REPLACING THE LEFT MLG SQUAT SWITCH. RECEIVED NEW SQUAT SWITCH. REPLACED SQUAT SWITCH ON LT MAIN LANDING GEAR IAW AMM 32-60-05-4. PERFORMED SQUAT SWITCH RIG IAW AMM32-60-00-5. NO FAULTS NOTED.
NLG - DURING LANDING GEAR EXTENSION ON FINAL APPROACH, NOSE GEAR DID NOT EXTEND. CYCLED LANDING GEAR ONE TIME AND ALL THREE LANDING GEAR EXTENDED NORMALLY. WHEN THE LANDING GEAR WAS SELECTED DOWN YOU COULD HEAR THE NOSE GEAR RELEASE FROM THE UPLOCK THEN A FEW SECONDS LATER IT FINALLY EXTENDED. PERFORMED SATISFACTORY WIRING CHECKS OF THE UPLOCK, DOWNLOCK, AND SQUAT SWITCHES WITH NO DEFECTS NOTED. WE WILL NEED TO JACK THE AIRCRAFT TO PERFORM GEAR SWINGS. HAD TO WAIT FOR A TENNANT TO DEPART SO WE COULD PUT THE AIRCRAFT ON JACKS. JACKED THE AIRCRAFT AND PERFORMED SATISFACTORY EXTENSION AND RETRACTIONS OF THE LANDING GEAR WITH NO DEFECTS NOTED. REMOVED AND REPLACED THE DOWNLOCK SWITCH WITH A NEW UNIT IAW MM 32-30-10. ADJUSTMENT AND OPERATIONAL CHECKS GOOD. ALSO PERFORMED A SATISFACTORY VISUAL INSPECTION OF THE NLG ASSY. AND DOORS AS REQUIRED TO SEE IF THERE WAS ANY BINDING OR RESTRICTIONS OF THE EXTENSION OR RETRACTION. NO DEFECTS NOTED. PERFORMED ANOTHER GEAR SWING TO ENSURE FIT ENSURE PROPER FIT. NO DEFECTS NOTED.