N624QS
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
EMERGENCY LIGHT OUT AT SEAT 8. FOUND SEAT 8 EMER LIGHT DISCONNECTED, RE-CONNECTED LIGHT CONNECTOR, AND OPS GOOD. WORK PERFORMED IN REF TO CE 680A AMM 33-20-05, 33-50-00.
CABIN EMERG LIGHT: BATTERIES HOOKED UP. NO POWER TO AIRCRAFT. TURNING THE EMERGENCY LIGHTS SWITCH TO ON. EMERGENCY LIGHTS COME ON EXCEPT FOR THE TWO RED EXIT LIGHTS BY THE MAIN CABIN DOOR. EMERGENCY LIGHTS GO OFF WHEN SWITCHING THE EMERGENCY LIGHT TO ARM POSITION. THE EMERGENCY LIGHTS SHOULD STAY ON. REMOVED #1 EMERGENCY BATTERY AND INSTALLED NEW CONDITON #1 EMERGENCY BATTERY IAW CE680A AMM 33-50-06. PERFOMRED OPS AND FUNCTIONAL CHECKS IAW CE680A AMM 33-50-00. OPS AND FUNCTIONAL CHECKS GOOD WITH NO DEFECTS NOTED.
CABIN EMERG LIGHT: CENTER SECTION OF CABIN EMERGENCY LIGHTS AND OVER WING LIGHTS ARE REQUIRING A CHARGE PROCEDURE TO PASS THE PREFLIGHT TEST AND WILL NOT HOLD THE CHARGE FOR VERY LONG. EMERGENCY EXIT SIGNS WORK, ISLE PATH LIGHT BELOW LAV WORKS, AND SWITCH WORKS CORRECTLY. REMOVED #3 EMERGENCY BATTERY PACK PN: CBS28-1 SN: 2628M AND INSTALLED CUSTOMER SUPPLIED REPAIRED EMERGENCY BATTERY PACK PN: CBS28-1 SN: 009010. REMOVED #2 FAILED BATTERY PN CBS28-1, SN 2236M. INSTALLED CUSTOMER SUPPLIED REPAIRED BATTERY PN CBS28-1, SN 008942 AT THE #2 LOCATION. OPERATIONAL CHECK GOOD. IN REF TO CE-680A MM 33-50-06
MAIN CABIN ENTRY DOOR WOULD NOT OPEN UPON ARRIVAL. PRESSED RED BUTTON AND HANDLE WOULD NOT LIFT. NO WARNINGS OR CASS MESSAGES ASSOCIATED WITH DOOR FAILING TO OPEN. LINE STAFF ASSISTED OPENING THE DOOR FROM OUTSIDE. ONCE LINE STAFF OPENED DOOR, WE TRIED CLOSING AND OPENING AGAIN WITH THE SAME RESULT OF IT NOT OPENING. INSTALLED REPLACEMENT CONTACTOR ON BROKEN WIRE AT CABIN DOOR INNER HANDLE PUSH BUTTON SWITCH. INSTALLED CONTACTOR INTO REPLACEMENT SPLICE. OPERATIONAL CHECK SATISFACTORY.
WING BLD LEAK L AMBER CAS: WING BLEAD LEAK L ILLUMINATED ON FINAL. THE MESSAGE WAS ON UNTIL WE SHUT THE AIRPLANE COMPLETELY DOWN. THE FIRE DEPARTMENT THERMAL SCANNED THE WING AND IT WAS AT AMBIENT. REMOVED AND REPLACED LH WING BLEED AIR LEAK DETECTION SENSING ELEMENT PERFORMED HIGH POWER RUNS OPS CHECK GOOD NO FAULTS AT THIS TIME NO DEFECTS NOTED AT THIS TIME
AFTER WE CLOSED CABIN DOOR DOOR WOULD NOT LOCK AND THE CABIN DOOR OPEN CAS MSG REMAINED ILLUMINATED. RAN CHECKLIST (AFM 3-510-29). FAULT DID NOT CLEAR. REMOVED CED MONITOR PCB PIN: 7468101-17 SIN: 0216 AND INSTALLED "NEW' CED MONITOR PCB PIN: 7468101-17 SIN: 31469861-3 IAW 680A AMM 24-60-40. OPERATIONAL CHECKS ARE GOOD AT THIS TIME.
PASSENGER / CREW DOORS: MAIN CABIN DOOR MADE A CONTINUAL CLUNKING SOUND DURING FLIGHT. SIMILAR TO THE CLUNK SOUND HEARD FROM THE VENT DOOR WHEN CLOSING THE MAIN CABIN DOOR. EITHER WITH POWER ON OR NOT. HAPPENED AT LEAST 25 TIMES DURING A 40 MINUTE FLIGHT AT 17000MSL. DOOR SHOWED SECURED.//CORRECTIVE ACTION// POWERED UP A/C AND CYCLED DOOR NUMEROUS TIMES. ACTUATED SWITCH ON HANDLE MULTIPLE TIMES AND SOLENOID OPERATES EVERY TIME. MONITORED DOOR DURING ENGINE RUNS, NO NOISE OR CAS MESSAGES NOTED. ADVISED MCC AND THEY STATED NO HISTORY. DOORS OPS CHECK GOOD. WORK DONE IN REF CE680A MM 52-10-00
RIGHT MLG LANDING GEAR RETRACTION: AFTER TAKEOFF THE RIGHT MAIN LANDING GEAR DID NOT RETRACT. ACCOMPLISHED ABNORMAL PROCEDURES CHECKLIST AND AFTER ACHIEVING 3 DOWN AND GREEN WE LANDED. // SIGNOFF// OPERATED LANDING GEAR UPON ARRIVAL AND COULD NOT DUPLICATE ISSUE. COLD SOAKED SWITCH AND CHECKED WITH METER AND NO DEFECTS WERE NOTED. RESEARCHED ISSUE IN ARES AND FOUND RH UPLOCK SHOWED UP AND LOCKED WITH AIRCRAFT ON THE GROUND. CONTACTED MCC AND CONFIRMED THEY WOULD LIKE THE SWITCH HARNESS REPLACED. 2023-02-02 23:08:04 MATTHEW FITZPATRICK ( C47524 ) REMOVED AND REPLACED RH UP LOCK HARNESS ASSEMBLY PN 6948101-3 IAW CE 680A MM 32-32-00. OPERATED GEAR 10 CYCLES WITH NO DEFECTS NOTED,
APU STINGER DEBRIS SHIELD CRACK.
EMERG EXIT SIGN/LIGHT: INTERIOR EMERGENCY LIGHTS AROUND MAIN CABIN DOOR AND SEAT 10 FLOOR LIGHT WILL NOT EXTINGUISH AFTER POWERING DOWN (BATTERIES DISCONNECTED AND EMER LIGHT SWITCH OFF) // SIGNOFF // CONFIRMED DISCREPIINCY, RESET INERTIAL SWITCH ASSOCIATED WITH THE EFFECTED EMER LIGHTS AND THE LIGHTS EXTIGUISHED. COMPLIED WITH NETJETS TASK CARD TC-TLT-33-1001 EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE. BATTERIES PASSED PER TASK CARD AND CMM 33-50-03 NO FURTHER DEFECTS NOTED.
NLG LANDING GEAR RETRACTION: AFTER TAKEOFF, DURING GEAR RETRACTION SEVERE VIBRATION FELT. GEAR RETRACTION TERMINATED AND LANDING LEFT EXTENDED WITH NORMAL INDICATIONS (3 GREEN). FLIGHT DIVERTED TO KGSP. DURING 30 MINUTE FLIGHT GEAR INDICATIONS WERE NORMAL (EXTENDED) AND AIRCRAFT HANDLING CHARACTERISTICS WERE NORMAL. NORMAL LANDING AND VISUAL INSPECTION, NO DISCREPENCIES NOTED. REMOVED AND REPLACED BOTH THE #1 AND #2 NLG WHEEL ASSEMBLES. SERVICED TIRES. RETURNED AIRCRAFT TO ORIGNAL CONDITIONAL AT THIS TIME. NO FURTHER DEFECTS NOTED WORK DONE IAW MM 32-40-15
EMERGENCY LIGHTS BATTERY: EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN EMER.SWITCH IS PLACED INTO ON///SIGN-OFF//REMOVED AND REPLACED EMERGENCY BATTERY PACKS. IAW 680AS AMM 33-50-06.
THE AUTO THROTTLES WOULD NOT ENGAGE DURING TAKEOFF ROLL, AT POSITIVE RATE, CALLED GEAR UP. MLG WOULD NOT RETRACT. GEAR HANDLE CAME OUT OF DETENT AND RAISED HANDLE SOUNDED LIKE A JACKHAMMER AND THE GEAR WOULDNT RETRACT. GEAR HANDLE RETUNED TO DETENT AND POWER REDUCED AT THE SAMETIME, VIBRATION CEASED. RAN THE QRH AND RETURNED TO MDW FOR LANDING. REMOVED LANDING GEAR CONTROL MANIFOLO P/N 9914&49·5 S/N: 1082. DUE TO MLG WOULD NOT RETRACT. INSTALLED CUSWMER SUPPLIED OVERHAULED LANOING GEAR CONTROL MANIFOLD P/N: 991464~S S/N: 0989. ALL WORK IN REFERENCE TO AMM 32·30-20. REMOVED CHECK. VALVE P/N 1C5230 CLUE TO VALVE BEING SEIZED. INSTALLED CUSTOMER SUPPLIED NEW CHED< VALVE P/N ICS230. PERFORMED BLEEDING PROCEDURE AND OPS CHECK. BLEEDING AND OPS CHECK GOOD. DOWNJACKED AIRCRAFT: AND RETURNED AIRCRAFT: TO ORIGINAL CONFLGURATLON. NO FURTHER DEFECTS NOTED. ALL WORT< DONE !AW AMM 32-34-00, 12-10-30, 32-30--00
MAIN DOOR - WHEN UNLOCKING MAIN CABIN DOOR, IT NO LONGER UNLATCH ON ITS OWN AND REQUIRE AN EXCESSIVE AMOUNT OF PULLING/PUSHING TO OPEN IT. // SIGNOFF // COMPLIED WITH MED RESET PROCEDURES, PERFORMED MED OPERATIONAL CHECKS SEVERAL TIMES WITH SATISFACTORY RESULTS. MED WORKS NORMAL. WORK DONE IN REF TO CES·FT·680A-3036 SECTION 6.2.3.3.2, AND AMM CH.52· 10-00. NO DEFECTS NOTED.
DISPLAY UNIT - DURING FLIGHT INTERMITTENT HOT ELECTRICAL ODOR IN COCKPIT. AMLCD VERY HOT TO THE TOUCH. FOUND AMLCD VERY HOT TO THE TOUCH . REMOVED AND REPLACED AMLCD IAW CE-560XL M/M 77-40-00. OPS CHECK GOOD. PERFORMED ENG RUNS NO ABNORMAL ELECTRICAL SMELL NOTED IN AIRCRAFT INSTALLED AMLCD REMOVED SERVICEABLE FROM AIRCRAFT N698QS P/N 10644D02M05 S/N 04090426REMOVED AMLCD 10644D02M05 S/N 04050396A
DURING INSPECTION, FOUND THE LT OUTBOARD FLAP IS DELAMINATED. INSTALLED A REPAIR IAW MM 57-50-01, AND 27-51-00.
WHILE CLIMBING, THE RT THRUST REVERSER UNLOCK LIGHT CAME ON FOLLOWED BY THE ARM LIGHT. TURNED ON THE EMERGENCY STOW SWITCH PERFORMED MEMORY ITEMS FOLLOWED BY THE CHECKLIST. DECLARED THE EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE RIGHT THRUST REVERSER INBD AND OTBD STOW SWITCHES WITH NEW AND REACTIVATED THE LT AND RT THRUST REVERSER AND OPS CHECKED GOOD IAW CMM 78-30-1 AND AMM 78-31-00-3.
DURING CLIMBOUT AT APPROXIMATELY 12,000 FT, THE RT ENGINE OIL PRESSURE WENT TO ZERO. IT WAS IMMEDIATELY FOLLOWED BY A RED MASTER WARNING LIGHT AND A LOW OIL PRESSURE LIGHT. AFTER COMPLETING THE EMERGENCY CHECKLIST, THE GAUGE RETURNED TO NORMAL WITH A REDUCED THRUST SETTING. ON POST FLIGHT, RT ENGINE OIL QUANTITY WAS BELOW MINIMUM AND THERE IS A TRACE OF OIL ON THE LOWER AFT SECTION OF THE COWLING. AS PER RECOMMENDATION OF PWC: REMOVED RT ENGINE AND INSTALLED AN INSPECTED SERVICEABLE RT ENGINE. PERFORMED LEAK AND OPERATIONAL CHECKS WITH NO DEFECTS NOTED. ALL WORK PERFORMED IAW AMM 71-00-00 AND EMM 72-00-00.
APU ON & BLEED ON, TEMP WENT RAPIDLY TO 250 DEGREES & THEN AIR DUCT O'HEAT ANNUNCIATOR ILLUMINATED, FOLLOWED BY A VERY STRONG ACRID SMOKY SMELL IN THE CABIN. BLEED AIR WAS TURNED OFF & FULL MANUAL COLD SELECTED, BUT THE SMELL OF SOMETHING BURNING CONTINUED. APU WAS SECURED. NEED EVALUATION FOR COLLATERAL DAMAGE. R & R THE TEMP CONTROL DISPLAY UNIT IAW MM 21-51-00. SYS OPERATIONS CHECKED GOOD.
NR 1 DISPLAY UNIT INOPERATIVE, NOTICED SMOKE AS WELL. REMOVED AND REPLACED THE NR 1 DISPLAY UNIT, OPS CHECKED GOOD. NO DEFECTS NOTED, WORK COMPLETED IAW MM 31-50-01.
RIGHT ENGINE OIL PRESSURE WENT TO 17 PSI INFLIGHT. SHUTDOWN ENGINE. R & R THE ENGINE & OPS & LEAK CHECKED GOOD. PERFORMED A 5 POINT PERFORMANCE CHECK.
RIGHT AFTER LIFTOFF, EXCESSIVE FWD PRESSURE REQUIRED (FULL FWD TRIM AND BOTH HANDS ON YOKE APPLYING FWD PRESSURE). AFTER FLAP/STAB RETRACTION AND 200KTS A/S, ACFT WAS ABLE TO BE FLOWN WITH ONE HAND WHILE MAINTAINING FULL FWD TRIM. LEVELING AT 14,000 AND >250 KTS, THE REQUIRED FWD PITCH WAS BEYOND NORMAL OPERATIONS. DECREASE IN AIRSPEED WAS ONLY MEANS TO REGAIN PITCH CONTROL WHILE MAINTAINING FULL FWD PITCH TRIM. NO ANNUNCIATORS ILLUMINATED. HYD PRESS ANNUNCIATORS APPEARED NORMAL. FOUND TRIM CONTROL WHEEL POINTER GROOVE CRACKED OUT. R & R TRIM WHEEL. ADJUSTED POINTER AND CHECKED FOR NO TAKEOFF INDICATIONS IAW MM 27-31-00.
THE NOSE WHEEL GREEN LIGHT WOULDNâT GO OUT AFTER THE GEAR WAS SELECTED UP. REMOVED & REPLACED ACTUATOR, COMPLIED WITH GEAR ANGLE, RETRACTION, LEAK & BLOWDOWN CHECKS IAW MM 32-30-03, 32-20-00 & 32-01-00. SERVICED PNEUMATIC RESERVOIR IAW MM 12-13-01. OPS CHECKS GOOD.
LT EEC FAILED DURING TO ROLL. REMOVED AND REPLACED NR 1 ENGINE SERVO VALVE. PERFORMED OPERATIONAL CHECK AND NO DEFECTS NOTED AT THIS TIME REF MM 75-30-01 & 71-00-00.
AFTER ROTATION, THE YAW DAMPER WOULD NOT ENGAGE AND WHEN WE TURNED LT, THE LT RUDDER PEDAL WOULD NOT MOVE. AFTER ENGAGING AND DISENGAGING THE YAW DAMPER THE RUDDER OPERATED NORMALLY. ON THE GROUND WE COULD FEEL AND HEAR GRINDING SOUND IN THE RUDDER PEDALS WHILE TAXIING. [SUP 05-03-07] REMOVED AND REPLACED THE AUTOPILOT CONTROLLER IAW THE CESSNA 560XL MAINTENANCE MANUAL 22-11-03. OPS CHECK OF THE AUTOPILOT CONTROLLER GOOD IAW THE HONEYWELL PRIMUS 1000 INTEGRATED AVIONICS SYSTEM TEST AND FAULT ISOLATION MANUAL FOR THE EXCEL.
CAPT`S WINDSHIELD SHATTERED.
ACCELERATING THROUGH 250KTS, FELT EXCESSIVE VIBRATION. UPON LANDING, FOUND THAT THE RT TR BUCKET NOT FLUSH WITH ENGINE COWLING. M2B- REACTIVATED RT TR UPON APPLYING HYDRAULIC PRESS. RT BUCKET CLOSED FLUSH WITH ENGINE COWL. INSPECTED TR FOR DAMAGE AND CYCLED RT TR SEVERAL TIMES AS PRECAUTION. NO DAMAGE NOTED RT BUCKET NOW FLUSH WITH ENG COWL.
AFTER SETTING T/O POWER ON DEPARTURE ROLL RUDDER PEDALS BECOME VERY STIFF (FEELS LIKE YAW-DAMP IS ON). ABORTED TAKEOFF AT STP AFTER REACHING 60 KIAS. A/C TAXI'S NORMAL AND RUDDER BIAS TEST WAS NORMAL. REMOVED AND INSTALLED A NEW RUDDER BIAS ACTUATOR, OPS CHECK GOOD IAW CE560XL M/M 27020-05.
ON TAKEOFF WITH THROTTLE IN THE T/O DETENT, THE LT ENGINE ITT EXCEEDED 720 DEG CELSIUS WITHIN 10 SECS. THE LT ITT INDICTED 724 DEG CELSIUS AND WAS STILL SLOWLY INCREASING. LT THROTTLE REDUCED TO CLIMB. DETENT AND ITT INDICATION IMMEDIATLY DECREASED BELOW 720DEG CELSIUS. NO OTHER PROBLEMS OBSERVED. PERFORMED 5 POINT PERFORMANCE RUN AND CHECK BOV POSITION. CHECKED RESISTANCE ON ITT HARNESS IAW PWA 545A MM 71-00-00. NO DEFECTS NOTED. OCF REQUESTED PER TECH REP.
NO TAKEOFF LIGHT WILL NOT GO OUT ON GROUND, HORN SOUNDS WHEN POWER IS ADVANCED ALL ASSOCIATED SYSTEMS CHECKED / NO PROBLEMS INDICATED. FOUND STAB POSITION SWITCHES OUT OF ADJUSTMENT AND CORROSION ON SPEED BRAKE SWITCH CONNECTORS. ADJUSTED HORIZONTAL STAB POSITION SWITCHES NR 6 & 7. CLEANED SPEED BRAKE CONNECTORS PROO1 & PLOO1. OPS CHECK NO TAKEOFF WARNING SYSTEM . OPS CHECK NORMAL. WORK PERFORMED IAW CE-560 XL M.M. CHAPT 27-40-00 AND CHAP 27-61-00.