N618QS

Part: NONE — NONE · airframe 14,193 hrs · 10,944 cycles

MAIN DOOR VISUAL INDICATOR: TOP LEFT CABIN DOOR PIN INDICATOR FLAG IS NOT CENTERED ABOUT 1/4 OF THE WAY OUT OF THIS SITE WINDOW //SIGNOFF// REMOVED MED STEPS AND GAINED ACCESS TO LOCKING PINS AND LINKAGES AND FLAGS. !PERFORMED A GVI OF THE LOCKING FLAG INDICATORS AND FOUND DEBRIS TO NOT LET FLAG TRAVEL COMPLETELY TO CENTER. REMOVED AND CLEANED DEBRIS FROM LOCKING FLAG AND PERFORMED AN OPS CHECK OF THE DOOR AND FLAG IS NOW CENTERED. OPS CHECK GOOD, WORK DONE REF CESSNA CE-560XL AMM 52-10-00. NO FURTHER DEFECTS NOTED

Part: BOLT — BACKED OUT (PAX DOOR) · airframe 13,481 hrs · 10,412 cycles

ENTRANCE STAIR HARDWARE: FORWARD TELESCOPING MAIN DOOR BRACE HAS ATTACHMENT HARDWARE THAT IS BACKING OUT. INSPECTED PIN AND CONFIRMED WRITE-UP. RE-SECURED PIN AS REQUIRED, USING ORIGINAL HARDWARE, I.R.W. CE-560XLS AMM 52-10-01-2. THE DOOR AND TELESCOPE ROD OPERATE NORMAL.

Part: FRAME — CHAFED (TAILCONE) · airframe 13,088 hrs · 10,133 cycles

REPAIR OF TAILCONE FRAME(S)CHAFE DAMAGE. ENGINEERING REPAIR LETTER DQ26014M1 DATED 06/11/2020, TAILCONE FRAME(S)CHAFE DAMAGE.

Part: STIFFENER — DEBONDED (ZONE 200) · airframe 13,088 hrs · 10,133 cycles

DISBOND, ENGINE BEAM, STIFFENERS, AFT. FIELD REPAIR FR-560-5506-7762 DATED 03/05/2020, DISBOND, ENGINE BEAM, STIFFENERS, AFT WITH FAA FORM 8100-9 DATED 03/06/2020.

Part: CONDENSER — DIRTY (CABIN AIR) · airframe 12,967 hrs · 10,049 cycles

COCKPIT ODOR - ON DESCENT INTO PBI WITH POWRAN APU AND HAD NO ODOR. RAN RIGHT ENGINE ONLY AND NO ODOR. RAN LEFT ENGINE ONLY AND NO ODOR. REPOSISTION AIRCRAFT AND PERFORMED POWER RUNS ONE AT A TIME AT POWER AND EITHER ENGINE DID NOT PRODUCE A MUSTY ODOR. // SIGNOFF//GAINED ACCESS AND REMOVED OLD CONDENSER BAG P/N: 83237-121 NSN AND INSTALLED A NEW CONDENSER BAG P/N:83237-12, NSN. PERFORMED APU AND ENGINE RUNS AGAIN WITH NO ODOR. NO FURTHER DEFECTS NOTED. ALL WORK IAW CE-560XLS MM 21-51-00ER AT CLOSE TO IDLE WE HAD A STRONG DIRTY SOCK ODOR IN THE COCKPIT

Part: ENGINE — CONTAMINATED · airframe 12,874 hrs · 9,974 cycles

COCKPIT ODOR - REPEAT WRITEUP. DURING TAKEOFF WITH THE APU OFF WE GOT A BAD ODOR OF SOME SORT OF CHEMICAL SMELL. POSSIBLY OIL? DEFINITELY NOT EXHAUST OR BAD SOCK OR MUSTY SMELL. SMELL WAS WORST AT HIGH POWER SETTING. WITH APU ON WHILE ON THE GROUND AND TAXI OUT WE COULD NOT SMELL ANYTHING UNUSUAL. REMOVED AND REPLACED THE LT OZONE CONVERTER. REMOVED AND REPLACED THE RT OZONE CONVERTER. PERFORMED A LEAK CHECK, NO LEAKS NOTED. WORK COMPLETED IAW AMM 21-71-00. REMOVED AND REPLACED THE WATER SEPARATOR CONDENSER SOCK. LEAK AND OPS CHECKED GOOD IAW ECS AND WATER SEPARATOR OPERATION AND MAINTENANCE MANUAL4-404. NO FURTHER ODORS NOTED IN COCKPIT OR CABIN. ACCOMPLISHED BORESCOPE INSPECTION OF THE LT ENGINE AND FOUND MINOR AMOUNT OF JOINT COMPOUND STREAKING IN ONE LOCATION ONLY. NO OTHER DISCREPANCIES NOTED AT THIS TIME. WORK COMPLETED IAW EMM 72-00-00. REMOVED AND REPLACED THE LT ENGINE. PERFORMED OPERATIONAL LEAK CHECKS AND PERFORMANCE RUNS SATISFACTORILY. WORK COMPLETED IAW AMM 71-00-00 & EMM 71-00-00 & 72-00-00. ACCOMPLISHED BORESCOPE INSPECTION OF THE RT ENGINE AND FOUND SIGNIFICANT AMOUNT OF JOINT COMPOUND STREAKING IN MULTIPLE LOCATIONS. NO OTHER DISCREPANCIES NOTED AT THIS TIME. WORK COMPLETED IAW EMM 72-00-00. REMOVED AND REPLACED THE RT ENGINE. PERFORMED OPERATIONAL LEAK CHECKS AND PERFORMANCE RUNS SATISFACTORILY. WORK COMPLETED IAW AMM 71-00-00 & EMM 71-00-00 & 72-00-00.

Part: ENGINE — CONTAMINATED (LT & RT) · airframe 12,873 hrs · 9,973 cycles

COCKPIT ODOR - AT FL410 STARTED TO GET A JET EXHAUST ODOR IN THE COCKPIT. BOTH CREWMEMBERS STARTING EXPERIENCE NAUSEOUS SYMPTOMS. CONTINUED BUT STARTED AN EARLY DESCENT. ONCE BELOW 10,000FT, SYMPTOMS IMPROVED AND THE SMELL DISSIPATED. THE APU WAS OFF DURING THE ENTIRE EVENT. DEFINITELY NOT EXHAUST OR BAD SOCK OR MUSTY SMELL. SMELL WAS WORST AT HIGH POWER SETTING. WITH APU ON WHILE ON THE GROUND AND TAXI OUT WE COULD NOT SMELL ANYTHING UNUSUAL. REMOVED LT OZONE CONVERTER AND INSTALLED A NEW CONVERTER. REMOVED RT OZONE CONVERTER AND INSTALLED A NEW CONVERTER. PERFORMED LEAK CHECK, NO LEAKS NOTED. ALL WORK COMPLETED IAW AMM 21-71-00. REMOVED AND REPLACED THE WATER SEPARATOR CONDENSER SOCK WITH NEW. LEAK AND OPS CHECKED GOOD IAW ECS AND WATER SEPARATOR OPERATION AND MAINTENANCE MANUAL4-404. NO FURTHER ODORS NOTED IN COCKPIT OR CABIN. ACCOMPLISHED BORESCOPE INSPECTION ON LT ENGINE AND FOUND MINOR AMOUNT OF JOINT COMPOUND STREAKING IN ONE LOCATION ONLY. NO OTHER DISCREPANCIES NOTED AT THIS TIME. ALL WORK COMPLETED IAW EMM 72-00-00. REMOVED THE LT ENGINE AND INSTALLED INSPECTED SERVICEABLE ENGINE. PERFORMED OPERATIONAL LEAK CHECKS AND PERFORMANCE RUNS SATISFACTORILY. ALL WORK COMPLETED IAW AMM 71-00-00 & EMM 71-00-00 & 72-00-00. ACCOMPLISHED BORESCOPE INSPECTION OF THE RT ENGINE AND FOUND SIGNIFICANT AMOUNT OF JOINT COMPOUND STREAKING IN MULTIPLE LOCATIONS. NO OTHER DISCREPANCIES NOTED AT THIS TIME. ALL WORK COMPLETED IAW EMM 72-00-00. REMOVED RT ENGINE AND INSTALLED INSPECTED SERVICEABLE ENGINE. PERFORMED OPERATIONAL LEAK CHECKS AND PERFORMANCE RUNS SATISFACTORILY. ALL WORK COMPLETED IAW AMM 71-00-00 & EMM 71-00-00 & 72-00-00.

Part: SERVICE DOOR — CRACKED (LAV SERVICE) · airframe 12,095 hrs · 9,402 cycles

LEVEL 1 CORROSION ON TOILET SERVICE DOOR AROUND LATCHES AND FOUND A CRACK IN DOOR BELOW FWD LATCH.

Part: LINK — CORRODED (LT MLG) · airframe 12,095 hrs · 9,402 cycles

DURING THE REMOVAL OF THE LT MLG TRAILING LINK HINGE PIN FOUND THE ATTACHING CLEVIS POINTS TO BE CORRODED. REMOVED CORRODED LT MLG TRAILING LINK AND INSTALLED A NEW LINK.

Part: ACCESS PANEL — CRACKED (VERTICAL STAB) · airframe 12,095 hrs · 9,402 cycles

REMOVED CRACKED VERTICAL STABILIZER ACCESS PANEL 340ER AND INSTALLED NEW P/N 5531005-3.

Part: DETECTOR — MALFUNCTIONED (RT NACELLE) · airframe 10,632 hrs · 8,295 cycles

RIGHT ENGINE FIRE LIGHT DIMLY FLICKERED ON AND OFF OVER TEN TIMES ON APPROACH AND LANDING. ANTI-ICE ON OVER OFF MADE NO DIFFERENCE NOT DID MODERATE POWER TO IDLE. TROUBLESHOT THE R ENGINE FIRE DETECTION SYSTEM AND INSPECTED RT ENGINE FIRE DETECTION SYSTEM IAW AMM 26-11-00 WITH NO DISCREPANCIES NOTED. SWAPPED THE LEFT AND RIGHT FIRE DETECTION CONTROL UNITS FOR CONVENIENCE IAW AMM 26-11-02.

Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 3 · airframe 10,371 hrs · 8,100 cycles

CENTER WING TO FUSELAGE, FWD ATTACH FITTING HAS DEEP CORROSION ON THE BOTTOM.

Part: COMPUTER — MALFUNCTIONED · airframe 8,490 hrs · 6,633 cycles

CLIMBING THRU 20,000 FT AT 220 KTS, THE PITCH ANNUNCIATOR ILLUMINATED ON THE PFD. DISCONNECTED THE AUTOPILOT WHICH RESULTED IN THE ACFT PITCHING UP RAPIDLY. TRIM WAS ROLLED FULL FWD AT THE TIME. SLOWED ACFT & THE BACK FORCES DISAPPEARED BELOW 200 KTS. PITCH TRIM COULD NOT BE MOVED ANY FURTHER FWD DURING THE INCIDENT. IT APPEARED TO BE AT THE FWD STOP. TESTED PITCH SYSTEM USING MANUAL, ELECTRIC TRIM AND USING AUTOPILOT THUMBWHEEL AND COULD NOT FIND ANY PROBLEMS. CHECKED FOR ERROR CODES FROM THE LAST THREE FLIGHTS AND COULD NOT FIND ANY PITCH SYSTEM ERRORS. REMOVED & REPLACED IAC615. OPS CHECKS PERFORMED IAW MM 34-26-00. OPS CHECKED GOOD. LOAD CURRENT NAV DATABASE AND AIRCRAFT DATABASE. CONFIGURED THE FMU'S TO MATCH THE CONFIGURATION OF THE FMU'S THAT WAS REMOVED. OPS CHECKED GOOD.

Part: BEARING — FROZEN (ELEVATOR) · airframe 8,126 hrs · 6,365 cycles

DURING ELEVATOR REMOVAL, NOTICED THAT A NUMBER OF ELEVATOR ATTACHMENT BEARINGS ARE FROZEN AND REQUIRE REPLACEMENT.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 6,794 hrs · 5,289 cycles

DURING A SHARP RT TURN AT TAXI, CO-PILOT`S RT BRAKE PEDAL LOST PRESSURE, & NEEDED TO BE PUMPED TO STOP ACFT FROM A 1 OR 2 MPH. CAPTAIN`S SIDE NEEDED A LOT OF MOVEMENT TO GET PRESSURE AFTER ACFT STOPPED. COPILOT`S RT PEDAL NEEDS A LOT MORE MOVEMENT TO GET PRESSURE THAN THE RIGHT. INSPECTED BRAKES, FOUND NORMAL, NO LEAKS NOTED. BLED BRAKES SYS IAW MM 32-44-00. OPS & LEAK CHECKED NORMAL.

Part: ACTUATOR — INOPERATIVE (LT MLG) · airframe 6,409 hrs · 2,657 cycles

FAILED TO GET LT MAIN GEAR LIGHT UPON EXTENDING MLG. JACKED A/C, REMOVED NR 2 ENG HYD PUMP TO FACILITATE HYD PWR W/ROBO MULE, REMOVED & REPLACED LT MLG ACTUATOR, SWING GEAR MULTIPLE TIMES NO DEFECT NOTED. DOWNJACKED A/C, REINSTALLED NR 2 ENGINE RAN, OPS & LEAK CHECKED. NO DEFECTS NOTED. ALL WORK DONE IAW CESSNA 560XLS MM 32-30-04, 32-01-00, 29-11-03-01, 7-10-01, 12-12-01

Part: SWITCH — FAILED (NLG) · airframe 753 hrs · 547 cycles

AFTER GEAR RETRACTION, UNLOCK LIGHT REMAINED ILLUMINATED. HYD PRESS AND STAB MISCOMPARE LIGHTS ALSO REMAINED ILLUMINATED. GEAR EXTENDED NORMALLY. UNLOCK LIGHT EXTINGUISHED. STAB MISCOMPARE LIGHT EXTINGUISHED. REMOVED AND REPLACED STBY AIRSPEED SWITCH AND TESTED IAW 27-40-00. LEAK TESTED STANDBY STATIC/PITOT SYSTEM IAW 34-11-09. GEAR OPERATES PROPERLY. PITOT/STATIC SYSTEM LEAK CHECK PERFORMED IAW FAR 91.411 ON 7-9-05.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 608 hrs · 443 cycles

RIGHT FRONT WINDSHIELD SHATTERED DURING FLIGHT. REMOVED RT RAIN SHROUD, REMOVED RT HEATED WINDSHIELD, INSTALLED NEW SEAL ON NEW WINDSHILED IAW MM 56-11-00. PERFORMED STEP C1-C8 RETORQUED BOLTS IAW 560XL MM 56-11-00. PERFORMED FUNCTIONAL CABIN PRESSURIZATION LEAK CHECK IAW 560XL M.M. 21-30-00 STEP C1-C16, & C26-C29. LEAK CHECKED GOOD. REMOVED JUMPER & RECONNECTED OUTFLOW VALVE, REMOVED PLUG FROM CABIN ALT. DIFF. PRESS. GUAGE, REMOVED SERVICE AIR CONNECTOR & RE-CAPPED LINE. OK TO CLOSE OUTFLOW VALVE ACCESS. OK TO INSTALL RAIN SHROUD