N583QS
Registered owner: NETJETS SALES INC, OK (owner ≠ operator)
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
LEFT WHEEL BRAKE LOCKS WITH ANY BRAKE PEDAL APPLICATION GREATER THAN MODERATE CAUSING THE AIRCRAFT TO LURCH TO THE LEFT ON LANDING. CORRECTIVE ACTION: REMOVED FAILED LH BRAKE ASSY PN: 2-1601-1, S/N: 0403 AND INSTALLED AN OVERHAULED CUSTOMER SUPPLIED BRAKE ASSY P/N: 2-1601-1, S/N: 0254. VISUAL, LEAK AND OPERATIONAL TESTS SATISFACTORY. ALL WORK IAW CE560XLS MM:32-32-01
RIGHT MAIN LANDING GEAR INDICATOR BULB DID NOT ILLUMINATE WHEN EXTENDING GEAR. FOLLOWED CHECKLIST AND PERFORMED EMERGENCY GEAR EXTENSION BLOW DOWN WITH BOTTLE CORRECTIVE ACTION: POWERED AIRCRAFT AND FOUND RH MAIN LANDING GEAR INDICATOR NOT ILLUMINATED.TAPPED ON INDICATOR AND LIGHTS NOW ILLUMINATED. THIS CONFIRMED FAULTY BULBS. REPLACED ALL BULBS ON LANDING GEAR CONTROL UNIT. ALL INDICATORS OPS CHECK GOOD. JACKED ATRCRAFT FOR BLEEDING AND GEAR SWINGS. PERFORMED RESET OF THE GEAR AND BRAKE EMERGENCY PNEUMATIC BOTTLE AND SAFETIED WITH COPPER WIRE. SERVICED THE GEAR AND BRAKE EMERGENCY PNEUMATIC BOTTLE, CONNECTED GPU AND HYDRAULIC CART,PERFORMED SHORT CYCLE OF THE GEAR TO RESET SHUTTLE VALVES, CYCLED LANDING GEAR 20 TIMES UNTIL NO BUBBLES WERE NOTED ON CART SIGHT GLASS & CLEANED PNEUMATIC VENT LINES. VERIFIED GEAR & BRAKE BOTTLE SERVICE TO BE OK AND JACKED DOWN THE AIRCRAFT. ALL WORK PERFORMED IAW CE-560XL AMM 32-44-00, 32-1-00
ELEVATOR TRIM IS NOT WITHIN NORMAL FLIGHT RANGE AND UNABLE TO INPUT ENOUGH NOSE DOWN TRIM TO NEUTRALZE CONTROL FORCE. FULL FORWARD NOSE DOWN TRIM AND AIRCRAFT STILL HAS NOSE UP TENDENCY. ADJUSTED POSITION OF CONTROL WHEEL/TRIM INDICATOR TO COINCIDE WITH THE POSITION OF THE ELEVATOR ELEVATOR TRIM TABS AT NEUTRAL POSITION. VERIFIED TRIM TAB NEUTRAL SETTING, TRIM TAB TRAVELS REF. MM 27-31-00.
MAIN CABIN DOOR REQUIRES EXCESSIVE FORCE TO OPEN OR CLOSE. FROM THE CLOSED AND LOCKED POSITION, MOVING CABIN DOOR HANDLE TO THE OPEN POSITION IS MORE DIFFICULT THAN CLOSING. THE DOOR SHOWS 9 FLAGS CORRECTLY AND THE APPROPRIATE LIGHTS EXTINGUISH. PLEASE EVALUATE DOOR FOR PROPER RIGGING AND ALIGNMENT. CORRECTIVE ACTION: ARRIVED AT AC AND VERIFIED DISCREPANCY. COORDINATED WITH FBO TO POSITION AC INTO HANGAR. REVIEWED CABIN DOOR TS PROCEDURES AND GAINED ACCESS TO CABIN DOOR LINKAGE. FOUND THE AFT MIDDLE LATCH PIN WAS NOT MOVING AS FREELY AS THE OTHERS, CAUSING A BIND IN THE HANDLE. CLEANED AND LUBRICATED THE LATCH PINS AS REQUIRED AND CYCLED THE CABIN DOOR HANDLES SEVERAL TIMES. PERFORMED OPS CHECKS OF THE CABIN DOOR AND OPS CHECKS ARE SATISFACTORY. THE HANDLE OPERATION IS MUCH SMOOTHER WITH NO BINDING NOTED. NOTIFIED MCC, CLOSED ACCESS AND RETURNED AC TO ITS ORIGINAL CONFIGURATION. WORK PERFORMED IAW AMM 52-10-00. 01JUN2025.
REPEAT WRITE UP. WHEN OPENING THE CABIN, THE PRECATCH IS STILL ENGAGED. PUSH BUTTON FROM THE OUTSIDE OR THE HANDLE FROM THE INSIDE MUST BE USED TO OPEN THE DOOR. ATTEMPTED TO OPEN FOUR TIMES FROM THE EXTERIOR AND INSIDE THE CABIN. ADJUSTED PRE-CATCH IAW TC-5XL-52-141001-JIC DATED 1-12-15. MCD OPS CHECKS GOOD.
MAIN DOOR WILL NOT CLOSE UNDER NORMAL OPERATIONS. WITH THE DOOR FULLY OPEN THE HANDLE WILL MOVE TO THE LOCK POSITION WITH EASE. DURING OPS CHECK OF MED, DOOR BAYONETS GOT STUCK IN THE DOOR. DOOR WOULD NOT OPEN YET THE ENTRY HANDLE ROTATES. T. FURTHER DISSASSEMBLY OF DOOR FROM THE INSIDE REVEALED THAT THE BOTTOM AFT DOOR PIN WAS IN A BIND CAUSING THE DOOR TO BE STUCK. DOOR PIN WAS RELEASED MANUALLY ALLOWING THE DOOR TO BE RELEASED REMOVED TEMP INSTALLED STEPS, REMOVED MAIN CABIN DOOR, REF AMM 52-10-00. REMOVED AFT DOOR SIDE HINGE & LOCATED AND DRILLED/TEMP INSTALLED CUSTOMER SUPPLIED "NEW" .064 INCH SHIM PN:6611315-7 BETWEEN CABIN DOOR & HINGE. PARTIALLY REINSTALLED DOOR ENOUGH TO PROVIDE A TEST FIT OF DOOR HINGE. OPERATION OF DOOR IS BETTER ONCE CLOSED HOWEVER THE CABIN DOOR LEANS FORWARD ON THE TOP END OF THE DOOR. REMOVED DOOR ONCE AGAIN, REMOVED FWD HINGE AND LOCATED AND DRILLED/TEMP INSTALLED CUSTOMER SUPPLIED "NEW" .32 INCH SHIM, PN:6611315-6 IN ADDITION TO .064 INCH SHIM THAT WAS THERE. PARTIALLY REINSTALLED DOOR ENOUGH TO PERFORM TEST FIT. TEST FIT IS SUCCESSFUL, FUNCTIONALLY CHECKED OPERATION OF CABIN DOOR CLOSING OPERATION. REF 560XL AMM 52-10-00 & 20-10-00. PERFORMED CABIN PRESSURIZATION OF THE AIRCRAFT AND LEAK CHECK. ALL CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME. REF: CE-560XL AMM 21-30-00. CHECKED OPERATION OF CABIN DOOR SEVERAL TIMES. ADJUSTED UPPER BAYONETTE RECEPTICALS SEVERAL TIMES. OBSERVED THAT DOOR HAS NO CLEARANCE BETWEEN FORWARD EDGE AND FUSELAGE & THERE IS A LITTLE LESS THAN 1/8 INCH BETWEEN AFT EDGE AND FUSELAGE. REMOVED SHIM FROM AFT DOOR GUIDE & INSTALLED UNDER FWD GUIDE. THIS EQUALIZED THE GAP BUT MADE THE AFT EDGE PULL AWAY FROM THE FUSELAGE. REMOVED SHIM FROM AIRCRAFT. CURRENTLY THE DOOR WILL CLOSE AND LOCK BUT WITH SIGNIFICANT EFFORT. THE LOWER DOOR PIN SOCKETS (ECCENTRIC HOLES) MAY NEED ADJUSTMENT. NOTE, THE OUTSIDE LOCKING HANDLE IS NOT AS DIFFICULT TO LOCK THAN THE INSIDE. REF CE560XL AMM 52-10-00. FACE TO FACE TECH TURN OVER WAS GIVEN TROUBLESHOOTING OF MED REVEALED THAT THE DOOR PINS WERE NOT PROPERLY ALIGNED WITH THE LATCH PLATES. PERFORMED LATCH PLATE/ ECCENTRIC BEARING ADJUSTMENT ON ALL 6 DOOR LATCH PLATES. DOOR STILL HARD TO OPEN FROM INSIDE THE CABIN. REF CE-560XL AMM 52-10-00. DISSASSEMBLED DOOR ASSEMBLY TO FACILITATE FURTHER TROUBLESHOOTING. INSPECTED/ LUBRICATED ALL COMPONENTS AS NECESSARY. REF CE-560XL AMM 52-10-00. NO DEFECTS NOTED AT THIS TIME PERFORMED LATCH PLATE/ ECCENTRIC BEARING ADJUSTMENT AGAIN, THIS TIME ROTATING LATCH PLATES AS REQUIRED FOR BETTER FIT. LUBRICATED DOOR BAYONETS POST ADJUSTMENT. REF CE-560XL AMM 52-10-00. DURING OPS CHECK OF MED, DOOR BAYONETS GOT STUCK IN THE DOOR. DOOR WOULD NOT OPEN YET THE ENTRY HANDLE ROTATES. TECHNICIAN HAD TO EXIT VIA EMERGENCY EXIT. FURTHER DISSASSEMBLY OF DOOR FROM THE INSIDE REVEALED THAT THE BOTTOM AFT DOOR PIN WAS IN A BIND CAUSING THE DOOR TO BE STUCK. DOOR PIN WAS RELEASED MANUALLY ALLOWING THE DOOR TO BE RELEASED. WORK PERFORMED REF CE-560XL AMM 20-10-65 AND 52-10-00. DOOR STEP ASSEMBLY DISSASSEMBLED, HARDWARE BAGGED, AND EMERGENCY EXIT OPEN FOR ACCES IN EVEN THE DOOR GETS STUCK CLOSED. THE DOOR TRIM FROM THE FORWARD DOOR FRAME NEED TO BE REINSTALLED (HARDWARE ARE AT THE PRECATCH RED HANDLE) PERFORMED LATCH PLATE/ ECCENTRIC BEARING ADJUSTMENT ON ALL 6 DOOR LATCH PLATES. DOOR STILL HARD TO OPEN FROM INSIDE THE CABIN. REF CE-560XL AMM 52-10-00. ISOLATED THE AFT LOWER LATCH PIN BY TEMPORARILY REMOVING THE RECEPTICLE AND THE DOOR CLOSES FROM INSIDE WITH EASE. RE-INSTALLED THE LOWER AFT ECCENTRIC. ADJUSTED THE AFT SIDE ECCENTRICS SLIGHTLY INBD TO ASSIST THE LOWER LATCH PIN WITH ENGAGEMENT WITH PARTIAL SUCCESS. THE DOOR WILL CLOSE NOW WITHOUT GETTING STUCK. ADJUSTED PRE-CATCH INBOARD ONE CERRATION, PERFORMED LATCH PLATE/ ECCENTRIC BEARING ADJUSTMENT ON ALL 6 DOOR LATCH PLATES. DOOR STILL HARD TO CLOSE FROM INSIDE THE CABIN. PUT PRECATCH IN ORIGINAL POSTILLION AND PERFORMED LATCH PLATE/ ECCENTRIC BEARING ADJUSTMENT ON ALL 6 DOOR LATCH PLATES. DOOR STILL HARD TO CLOSE FROM INSIDE THE CABIN. REF CE-560XL AMM 52-10-00. FURTHER EVALUATION REQUIRED PRE CATCH HANDLE CAME LOOSE DURING ADJUSTMENT OF LATCH PLATES. NEEDS TIGHTENING. REMOVED THE DOOR TRIM FROM THE FORWARD DOOR FRAME TO GAIN ACCESS TO CABIND DOOR PRECATCH MECHANISM. TIGHTENED AND ADJUSTED THE PRECATCH. PERFORMED MULTIPLES OPS CHECKS AND NOTICED THE PRE-CATCH ENGAGES WITHOUT ANY ASSISTANCE BUT WHEN OPENING, THE PRE-CATCH DOES NOT AUTOMATICALLY DISENGAGE DUE TO THE PRE-CATCH PIN OVERLAPPING THE FRAME-SIDE LATCH-PLATE. REF AMM 52-10-01. TOOK MEASUREMENTS OF THE GAPS ON DOOR WITH THE FUSELAGE FROM OUTSIDE AND INSIDE. MEASURED THE GAPS ON DOOR LATCH PLATES AND FUSELAGE LATCH PLATES. SENT PHOTOS WITH THE GAPS MEASUREMENT TO TEAM 560 FOR ANY ADVISEMENT. REF CE-560XL AMM 52-10-00. SENT EMAIL TO TEAM 560 AND WAITING FOR RESPONSE. ALL TEAM 560 RECOMMENDATIONS C/W. FOR T/S VISIBILTY TO THE LOWER AFT PORTION OF THE DOOR FITMENT. DISCONNECTED SPADE DOOR/FAIRING. (HARDWARE ATTACHED TO PUSH/PULL RODS). THE AFT DOOR HINGE HALF NEEDS TO BE SHIMMED IN ORDER TO BRING THE DOOR UP AND FURTHER INTO THE DOOR OPENING, AS EVIDENCED BY THE PICTURES SENT VIA EMAIL TO WSA AND MCC. THIS ALSO EXPLAINS WHY THE LOWER AFT BAYONET WILL NOT ENGAGE THE RECEPTACLE WITHOUT DIFFICULTY. PER TEXTRON REQUEST VISUALLY INSPECTED THE DOOR PIN FITTING AND IT DOES NOT APPEAR TO HAVE BEEN RECENTLY REPLACED AND APPEARS TO BE IN THE CORRECT INSTALLATION ORIENTATION. PER MCC REQUEST, CHECKED COUNTER BALANCE CABLE TENSION AND IT CHECKED OUT BELOW 200# AT 166 WHICH IS GOOD PER CE560XL AMM 52-10-03. IN ADDITION TO INSTALLING THE AFT DOOR HINGE SHIM, THE HINGE BOLT BUSHINGS MAY NEED TO BE REPLACED AND LINE REAMED. REQUESTED CLARIFICATION ON HINGE AND SHIM INSTALLATION AND DOOR FITMENT FROM TEXTRON VIA EMAIL. TEMP INSTALLED STEPS TO FACILITATE INTERIOR MAINT. SEE PREVIOUS STEP FOR T/S DETAILS. WAITING ON INPUT FROM MCC/CESSNA REGARDING DOOR HINGE SHIM INSTALLATION MAINTENANCE REFERENCE/TECH DATA. TWO TECHNICIANS REQ'D-TROUBLESHOOTING-REMOVED TEMP INSTALLED STEPS, REMOVED MAIN CABIN DOOR, REF 560XL AMM 52-10-00. REMOVED AFT DOOR SIDE HINGE & LOCATED AND DRILLED/TEMP INSTALLED CUSTOMER SUPPLIED "NEW" .064 INCH SHIM PN:6611315-7 BETWEEN CABIN DOOR & HINGE . PARTIALLY REINSTALLED DOOR ENOUGH TO PROVIDE A TEST FIT OF DOOR HINGE. OPERATION OF DOOR IS BETTER ONCE CLOSED HOWEVER THE CABIN DOOR LEANS FORWARD ON THE TOP END OF THE DOOR. REMOVED DOOR ONCE AGAIN, REMOVED FWD HINGE AND LOCATED AND DRILLED/TEMP INSTALLED CUSTOMER SUPPLIED "NEW" .32 INCH SHIM, PN:6611315-6 IN ADDITION TO .064 INCH SHIM THAT WAS THERE. PARTIALLY REINSTALLED DOOR ENOUGH TO PERFORM TEST FIT. TEST FIT IS SUCCESSFUL, FUNCTIONALLY CHECKED OPERATION OF CABIN DOOR CLOSING OPERATION. REF 560XL AMM 52-10-00 & 20-10-00. CABIN DOOR NEEDS HINGES FINISH INSTALLATION/HILOKS INSTALLED & NEW HARDWARE INSTALLED. NEEDS ADJUSTMENT OF BAYONET RECEPTACLES & PRE-CATCH. NEEDS STEP AND TRIM REINSTALLATION. REMOVED ALL ATTACHING HARDWARE AND SUPPORTS AND CABLES TO REMOVE THE CABIN DOOR THAT WAS TEMP INSTALLED. REMOVED FWD AND AFT HINGES AND SHIMS FROM DOOR AND CLEANED AND DEBURED ALL PART FOR FINAL INSTALL. APPLIED SEALANT TO ALL SHIMS, HINGE, AND DOOR STRUCTURE FOR FWD AND AFT HINGE. INSTALLED FWD AND AFT HINGES WITH TEMPORARY FASTENERS CURE TIME UP AT 1100 07/26/2024 CLEANED RETORQUED ALL SIDE LATCHED IN DOOR FRAME STRUCTURE AND CLEANED ALL PRUSSIAN BLUE OFF OF STRUCTURE AND BONNETS AND LATCHES REMOVED TEMPORARY FASTENERS AND INSTALLED HILLOCKS ONE AT A TOME IN BOTH FORWARD AND AFT DOOR HINGES CLEANED AND PREPPED AND STAGED ALL NEW HARDWARE FOR INSTALL OF CABIN ENTRY DOOR. WORK DONE REF SRM 51-40-03 REINSTALLED CABIN ENTRY DOOR TO AIRCRAFT WITH CUSTOMER SUPPLIED NEW HARDWARE. HOOKED UP ACTUATING LEVER, SUPPORT STRUTS, AND OVERCENTER LINK. INSTALLED DOOR STEPS FWD AND AFT CLOSEOUTS AND FIXED STEP ASSEMBLY. INSTALLED TOP FOLDING STEP TO OPS CHECK DOOR LATCHING. AFTER FULL INSTALLATION OF DOOR ALL LATCH PLATES ARE OUT OF ADJUSTMENT. REMOVED ALL LATCHES AND ADJUSTED EACH ECCENTRICS UNTIL ACHIEVED PROPER DOOR FIT. LOCKED DOWN ALL LATCH PLATES AND PERFORMED MULTIPLE SATISFACTORY OPS CHECKS OF CLOSING AND OPENING OD CABIN ENTRY DOOR. REINSTALLED FWD DOOR LINER TRIM. SPADE DOOR STILL NEEDS TO BE INSTALLED AND E-HATCH DOOR INSTALLED THEN PRESSURIZATION OF DOOR SEAL AND LEAK CHECKS PERFORMED. WORK DONE REF CESSNA CE-560XL AMM 52-10-00. SPADE DOOR STILL NEEDS TO BE INSTALLED AND E-HATCH DOOR INSTALLED THEN PRESSURIZATION OF DOOR SEAL AND LEAK CHECKS PERFORMED. INSTALLED SPADE DOOR. NO DEFECTS NOTED AT THIS TIME. OPS CHECK GOOD. REF: CE·S60XL AMM 52-10-05. INSTALLED EMERGENCY EXIT DOOR. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. AMM 52-20-00 PERFORMED CABIN PRESSURIZATION OF THE AIRCRAFT AND LEAK CHECK. ALL CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME. REF: CE·560XL AMM 21-30-00. MAIN DOOR PRECATCH LEVER: THE PRECATCH LEVER WILL NOT STAY IN THE 90 DEGREE POSITION. TIGHTENED JAM NUT ON PRE-CATCH STEM & POSITIONED LEVER AT 90 DEGREES AND OPS CKD GOOD. REF AMM 52-10-00. ORIGINAL SUBMISSION: 7/22/2024
MAIN DOOR PRECATCH WILL NOT RELEASE MAIN CABIN DOOR. OUTSIDE PRECATCH BUTTON WILL NOT RELEASR DOOR. CONFIRMED DISCREPANCY. FOUND PRECATCH PLUNGER TO NOT BE FLUSH WHEN ACTUATED CAUSING IT TO REMAIN CAUGHT AND NOT RELEASING THE DOOR. ADJUSTED PRECATCH PLUNGER IAW AMM 52-10-01. OPERATIONAL CHECK PERFORMED NO DEFECTS NOTED.
MAIN CABIN DOOR IS UNABLE TO BE OPENED. REPEAT WRITE UP. DOOR DOES NOT APPEAR TO BE FLUSH TO AIRFRAME. FOUND MAIN CABIN DOOR PRECATCH DIMENSIONS OUT OF TOLERANCE. REMOVED FORWARD REFRESHMENT CENTER AND INTERIOR. TRIM PANEL TO GAIN ACCESS TO PRECATCH MECHANISM, ADJUSTED PRECATCH TO DIMENSIONS IAW NJA TCâ¢SXL-52â¢141001 DATED 1-12-15, REINSTALLED FORWARD REFRESHMENT CENTER AND INTERIOR TRIM PANEL. PE FORMED CABIN DOOR PRECATCH OPS CHECK IAW AMM 52-10-01, OPS CHECK GOOD.
THE DOOR DOES NOT OPEN WITH THE HANDLE. THE PRECATCH DOES NOT RELEASE THE DOOR WHEN THE MAIN HANDLE IS TURNED TO THE OPEN POSITION. CONFIRMED THE DISCREPANCY PERFORMED A GVI OF DOOR, PRECATCH LATCH AND SURROUNDING AREA. NO OBVIOUS DEFECTS WERE NOTED. PERFORMED TASK CARD TC-5XL-52-141001 STEP 1, B FAILED. PORFORMED MM 52-10-00 AND FOUND GUIDE BLOCKS ON FORWARD SIDE ARE WORN, BOTH ON DOOR & IN OPENING. ALSO NOTICED WHEN DOOR IS CLOSED & MOVING HANDLE TO LOCK POSITION THAT TOP OF DOOR SHIFTS FORWARD SO THERE IS ALMOST NO GAP. R & R FWD AND AFT BLOCK & FWD & AFT GUIDE ON THE MAIN ENTRY DOOR IAW SPM 20-10-00. PERFORMED SATISFACTORY OPS CHECK OF PRE-CATCH LATCH IAW MM 52-10-00 NO DEFECTS NOTED.
ELEVATOR CONTROL/TRIM: AT FLIGHT LEVEL 410 PITCH TRIM ANNUNCIATOR ILLUMINATED. RAN JAMMED ELEVATOR TRIM CHECKLIST. NOTICED WE HAD PARTIAL CONTROL OF THE TRIM USING THE ELECTRIC TRIM OR MANUAL. 10 MINUTES LATER WE TRIED USING THE TRIM AGAIN AND IT WAS COMPLETELY FROZEN. DURING DECENT THE TRIM STARTED WORKING AGAIN FULLY AS WE CAME THRU 11000 FT. IT WAS CHECKED ON THE GROUND AND SEEMS TO BE FULLY OPERATIONAL RESOLUTION: PERFORMED AN ELEVATOR TRIM TAB ACTUATOR LUBRICATION BY REMOVING PANELS 351AB AND 352AB TO GAIN ACCESS TO THE ACTUATORS ZERC FITTINGS, THEN CLEANED OFF ALL THE OLD GREASE THEN REAPPLYING THE PROPER AMOUNT OF GREASE. ALL WORK DONE !AW CE·S60XLS 12-21-01. NO DEFECTS NOTED.
ON DEPARTURE CLIMBING THROUGH 1000, FLASHING HYD PRESS WITH MASTER CAUTION. FLAPS STOPPED RETRACTING AT 7 WITH THE HANDLE IN FLAPS 0 POSITION. PERFORMED HYD QRH CHECKLIST. REMOVED LT FLAP ACTUATOR IAW MM 27-51-04. INSTALLED A REPAIRED FLAP ACT IAW MM 27-51-04 WITH NEW HARDWARE. WIRED LT FLAP ACTUATOR UP LIMIT SWITCH. ALL WORK IAW MANUAL 20-30-25. SPLICED X2 LT UP LIMIT SWITCH WIRING. INSTALLED & SAFTIED LT FLAP ACTUATOR ROD END. COMPLIED WITH LT FLAP ACTUATOR LOCKING PRESSURE ADJUSTMENT & FLAP INTERCONNECT LOOP CABLE ADJUST CHECK IAW MM 27-51-00, & MM 27-51-04. OPS FLAPS THRU CYCLES, ALL INDICATIONS NORMAL, NO HYD LEAKS NOTED, TRAVEL CHKS GOOD. VERIFIED LT ACT MAINT, SAFETIES, RIGGING & OPS CHECKS.
THE FORWARD EMERGENCY EXIT LIGHTS AT THE CABIN DOOR DO NOT ILLUMINATE WHEN THE MAIN BATTERY IS OFF AND THE AFT EMERGENCY LIGHTS ARE DIM.
BRAKE PRESSURE LIGHT: DURING VISUAL APPROACH LOWERED LANDING GEAR FOLLOWED BY ANTISKID INOP LIGHT, AFTER NORMAL LANDING TAXING ONTO FBO RAMP LO BRK PRESS LIGHT ILLUMINATED FLASHING, USED EMER BRAKE PULL TO STOP AIRCRAFT SHORT OF PARKING. //SIGNOFF// ALLER ARRIVING ON SITE TECH PERFORMED AN INITIAL POWER UP AND NOTED THE BRAKE PRESS LOW, AND ANTI-SKID WARNING LIGHTS ILLUMINATED. TECH CHECKED ANTI-SKID FAULT INDICATOR WITH NO FAULTS DETECTED IA W CE560XLS AMM 32-44-00. A GVI OF THE COCKPIT FOUND THE POWER BRAKE CB POPPED. TECH RESET THE POWER BRAKE CB WHICH IMMEDIATELY CAUSED THE POWER BRAKE HYDRAULIC PUMP TO OPERATE CHARGING THE BRAKE ACCUMULATOR AND EXTINGUISHING THE BRAKE PRESSURE LOW AND ANTI-SKID WARNING LIGHTS. TECH IS IN WORK PERFORMING POWER BRAKE OPS AND ANTI-SKID OPS CHECKS IAW CE560XLS AMM 32-44-00 AND 32-44-20. OPS AND FUNCTIONAL CHECKS GOOD NO DEFECTS NOTED. MCC REQUEST TECHS REMOVE AND REPLACE BRAKE HYDRAULIC PUMP MOTOR FOR PRECAUTIONARY PURPOSES. REMOVED BRAKE HYDRAULIC PUMP MOTOR AND INSTALLED OVERHAULED CONDITION BRAKE HYDRAULIC PUMP MOTOR IAW CE560XLS AMM 32-44-20. PERFORMED POWER BRAKE AND ANTISKID OPS AND FUNCTIONAL CHECK IAW CE560XLS AMM 32-44-00 AND 32-44-20. OPS AND FUNCTIONAL CHECKS GOOD NO DEFECTS NOTED.
MAIN DOOR: MAIN DOOR WILL NOT OPEN UNTIL PRE-CATCH IS ACTUATED. *** CORRECTIVE ACTION *** ADJUSTED MED PRECATCH CABLE PER NJA MODEL 560XL TC-SXL-52-141001. ADJUSTED CAM OPENINGS IN DOOR FRAME FOR EASIER OPERATION. WORK PERFORMED AS PER CESSNA 560XL AIRCRAFT MAINTENANCE MANUAL 52·10·00, NO DEFECTS NOTED AT THIS TIME.
MAIN DOOR PRECATCH: WHEN OPENING THE LOCKED MAIN CABIN DOOR FROM THE INSIDE OR THE OUTSIDE THE PRE-CATCH WILL NOT RELEASE UNLESS PHYSICALLY PRESSED. ATTACHED VIDEOS ALSO INTERMITTENTLY WHEN THE DOOR IS CLOSED JUST ON THE PRE-CATCH WE ARE NOT ABLE TO MOVE THE PRE-CATCH LEVER TO RELEASE THE DOOR FROM THE INSIDE. // SIGNOFF // REMOVED THE DOOR STEP AND LUBRICATED THE HANDLE AND DOOR ( BAYONETS. LUBED THE PRECATCH PLUNGER. REMOVED THE TRIM PANEL AND LUBED THE PRECATCH ASSY. PULLED HANDLE AND NO DEFECTS NOTED ON THE PLUNGER. CLOSED THE DOOR FROM THE INSIDE WITH THE DOOR NOT LOCKED AND VERFIED THE DOOR CAUGHT PRECATCH. PULLED INNER PRECATCH HANDLE AND VERIFIED THE DOOR OPENED. TRIED A FEW TIMES WITHTHE SAME RESULTS. CLOSED THE DOOR FROM THE OUTSIDE AND VERIFIED THE PRECATCH WAS ENGAGED. PRESSED PRECATCH BUTTON AND VERIFIED THE DOOR OPENED. DOUBLE CHECKED THE PLUNGER GUIDE THAT MATES WITH THE PRECATCH LATCH AND IT WAS NOT CATCHING PREVENTING THE DOOR FROM OPENING. TECH WILL CHECK A FEW MORE TIMES AFTER LETTING TO DOOR SIT. CONTACTED MCC AND CONTROLLER WANTED CHECK DONE AFTER PRESSURIZING. ENERGIZED THE APU AND CHECKED MED AFTER INFATING SEALS AND PRECATCH FUNCTIONED NORMAL AND TRIED GOING FROM LOCKED TO OPEN AND CHECKED GOOD. PRESSURIZED THE ACFT USING THE APU AND DEPRESSURIZED. RE-CHECKED THE MED AND THE PRE-CATCH FUNCTIONED. PLACED ACFT BACK INTO NORMAL CONFIGURATION. WORK DONE IAW CE-560XLS M.M. 21-30-00,52-10-00, AND TEXTRON AVIATION CE-560XLS CABIN DOOR PRECATCH TROUBLESHOOTING VIDEO.
MAIN DOOR PRECATCH: WHEN DOOR IS CLOSED AND LOCKED WITH THE PRE-CATCH ENGAGED. UPON OPENING THE DOOR FROM INSIDE OR OUTSIDE THE PRE-CATCH WILL NOT RELEASE // SIGNOFF// CONFIRMED DISCREPANCY. GAINED ACCESS TO PRE-CATCH MECHANISM AND ADJUSTED PRE-CATCH CABLE UNTIL INTERIOR PLUNGER IS FLUSH WITH THE SOCKET SO THAT CAN NOT CATCH THE DOOR WHEN THE HANDLE IS IN THE OPEN POSITION. IAW CE-560XLS AMM CHAPTER 52-10-01 CLEANED ORE-CATCH MECHANISM AND LUBED IT. PERFORMED SEVERAL OPERATIONAL CHECKS AND CHECKED GOOD . NO OTHER DEFECTS NOTED.
MAIN DOOR PRECATCH: DOOR WOULD NOT RELEASE OF THE PRE-CATCH WHEN TRYING TO EXIT WITH PASSENGERS. IT OPENED AFTER ABOUT THREE ATTEMPTS IT FINALLY RELEASED OFF THE PRE-CATCH AND OPENED. WHEN COMING BACK TO THE DOOR LOCKED FROM THE OUTSIDE THE DOOR WOULD NOT RELEASE FROM THE P CATCH WHEN DOOR LEVER MOVE TO THE UNLOCK POSITION // SIGNOFF // ADJUSTED CABIN DOOR PRECATCH WITH REF TO CE-560XLS AMM 52-10--00, OPS CHECK GOOD AT THIS TIME, NO DEFECTS NOTED.
MAIN DOOR: REPEAT WRITEUP: AMBER "CABIN DOOR" ANNUNCIATOR LIGHT ILLUMINATED AT 6,000 FEET ON INITIAL CLIMB. NOTE: THE "PRESS SYSTEM SELECT" LEVER HAS BEEN LEFT IN THE "MANUAL" POSITION AS PER THE CHECKLIST. ADJUSTED DOOR PLUNGER STRIKER PLATE UNTIL DOOR LOCK SWITCH ACTUATION WAS SATISFACTORY. OPS CHECK GOOD. ALL WORK DONE IAW C#-560XL AMM, 52-70-00
MAIN DOOR: MAIN CABIN DOOR. WHEN OPENING THE MAIN CABIN DOOR FROM THE OUTSIDE, THE HANDLE UNLOCKS DOOR, BUT PRE-CATCH DOES NOT RELEASE. DOOR WILL NOT OPEN. PUSHING THE PRE CATCH RELEASE BUTTON ALLOWS THE DOOR TO OPEN. REPEAT ITEM FROM 5/12/21.///SIGN-OFF///FOUND DOOR FRAME BRACKET WITH 3 SHEARED RIVETS. REMOVED AND REPLACED 3 RIVETS IAW MODEL 560 XL SRM 51-40-03. OPS CHECK GOOD.
BOTH FLAP EXTENSION FAIL - ON APPROACH FLAPS WHERE SELECTED TO 15. "HYD PRESS" LIGHT INITIALLY ILLUMINATED NORMAL. THEN STARTED TO FLASH WITH THE "MASTER CAUTION" LIGHT. THE FLAPS NEVER TRAVELED PASS 3 DEGREES. WE MOVED THE FLAP SWITCH BACK TO FLAPS 0 DEGREE. THE FLAPS TRAVELED BACK TO 0 DEGREES AND THE "HYD PRESS" LIGHT EXTINGUISHED. WE DIVERTED, RAN THE APPROPRIATE CHECKLISTS AND LAND WITH NO FLAPS. ALL OTHER HYDRAULIC SYSTEMS WORK NORMALLY. // SIGNOFF //REMOVED AND REPLACED THE LH FLAP ACTUATOR IAW CE-560XL AMM 27-51-04-2. LEAK CHECK AND PS CHECK GOOD.
AFTER ENGINE START, THERE WAS A NOTICEABLE FUEL SMELL COMING IN THROUGH THE AIR VENTS WHICH EVENTUALLY DISSIPATED. WHILE TAXIING OUT THE TOWER CALLED AND STATED THAT WE HAD SOME SMOKE COMING OUT OF THE LEFT ENGINE. I GOT OUT TO LOOK AND IT WAS A GRAYISH WHITE SMOKE. I CHECKED THE RIGHT ENGINE AND THERE WAS NO SMOKE. AFTER INCREASING THE POWER ON THE LEFT ENGINE FOR A FEW MINUTES (WE THOUGHT IT MIGHT BE TYPE I/IV DEICE FLUID BURNING OFF) WE CHECKED AGAIN, BUT THE SMOKE WAS STILL EMANATING FROM THE LEFT ENGINE EXHAUST. WE TAXIED BACK TO THE FBO AND CHECKED THE ENGINE ONE MORE TIME PRIOR TO SHUTDOWN AND THE SMOKE WAS STILL THERE. IT WAS A VERY NOTICEABLE AMOUNT OF SMOKE. ALL ENGINE INSTRUMENTS WERE INDICATING NORMAL IN THE COCKPIT. **SUPPLEMENTAL INFORMATION - FOUND EVIDENCE OF FUEL LEAK AT RT TOP (NR 1) FUEL NOZZLE TRANSFER TUBE OUTER SHROUD. REMOVED T/R, EXHAUST SHROUD AND MIXER AND AFT BYPASS DUCT. DISASSEMBLED FUEL MANIFOLD, REMOVED NOZZLES AND INLET FUEL MANIFOLD ASSEMBLY. REPLACED ALL PACKINGS AND GASKETS. RE-INSTALLED SAME AS REMOVED FUEL NOZZLES AND INLET FUEL MANIFOLD ASSEMBLY. REASSEMBLED FUEL MANIFOLD ASSEMBLY. REINSTALLED AFT BYPASS DUCT, EXHAUST SHROUDAND MIXER AND THRUST REVERSER ASSEMBLY. PERFORMED ENGINE GROUND RUNS, LEAK AND OPERATIONAL CHECKS, AND 5 POINT RUNS. ALL ENGINE PARAMETERS WITHIN EMM LIMITS. NO SMOKE OBSERVED DURING ANY GROUND RUNS TODAY. IAW EMM71-00-00, 05-10-00, 72-00-00, 72-70-01, 72-50-03, 73-10-04, 73-10-07 AND AMM78-31-00.
FOUND MULTIPLE AREAS OF CORROSION ON THE LH MAIN LANDING GEAR TRUNNION P/N 6641501-7L, REPLACED WITH NEW TRUNNION.
PWR BRKS CB POPPED. ANTISD INOP ANNUNCIATOR ILLUMINATED. RESET CB ONCE AND IT POPPED AGAIN. AFTER 5 MIN TAXI, LO BRK PRESS ANNUNCIATOR ILLUMINATED FOLLOWED BY LOSS OF BRAKES. DRAINED AND FLUSHED BRAKE SYSTEM HYDRAULIC FLUID AND SERVICED RESERVOIR TO CORRECT LEVEL IAW AMM 12-12-02. BLED LEFT AND RIGHT BRAKES IAW AMM 32-44-00. PERFORMED GROUND RUN TAXI CHECK IAW AMM 71-00-04 WITH NO BRAKE SYSTEM DEFECTS NOTED.
ON TAXI OUT, THE CB POPPED OUT FOR THE POWER BRAKES, AFTER A FEW MINUTES, RESET CB AND RETURNED TO RAMP. AFTER STOPPED ON RAMP, PULLED CB FOR POWER BRAKES. INSPECTED POWER BRAKE AND ANTI-SKID BRAKE SYSTEM, NO DEFECTS NOTED. IAW CUSTOMER REQUEST, REPLACED HYDRAULIC BRAKE PUMP ASSY, PN: 640931, SN: 6768 AND ANTI-SKID POWER PACK MOTOR ASSY, PN: MP50B-1, SN: 2996.
AFTER TURNING XFEED OFF, THERE WAS A LOW FUEL PRESS LIGHT, THEN MASTER CAUTION, THEN R BOOST PUMP ON. RAN CHECKLIST N2 THEN M5 & COULD NOT GET R BOOST LIGHT TO EXTINGUISH. R BOOST PUMP LEFT ON IAW M5 CHECKLIST. R & R RT MOTIVE FLOW SHUTOFF VLV IAW MM 28-21-06. OPERATIONS & LEAK CHECKED GOOD.
IMMEDIATELY AFTER TAKEOFF, A GRINDING COULD BE FELT IN THE YOKE WHILE APPLYING FORWARD OR AFT MOVEMENT. VIBRATION WAS FELT IN FLOOR AT THE SAME TIME. NO GRINDING DURING FLIGHT CONTROL CHECK ON GROUND. GRINDING IS EXCESSIVE. REMOVED AND REPLACED THE ELEVATOR SCRUD DRIVE, OPS CHECKED GOOD IAW AMM 22-11-01.
DURING APPROACH AND LANDING THE "GREEN" LEFT MLG LIGHTS NEVER ILLUMINATED. RAN THE "GEAR WOULD NOT EXTEND" CHECK LIST TO MAKE SURE IT WAS DOWN AND LOCKED. REPLACED 2 BULBS FOR THE GREEN LT MLG INDICATION IAW MM 33-10-00, OPS TEST GOOD. RESET EMERGENCY BLOWDOWN BOTTLE CONTROL ARM AND RESERVICED BLOWDOWN BOTTLE IAW MM 12-13-00. PERFORMED LANDING GEAR FUNCTIONAL TEST IAW 33-01-00, WITH NO DISCREPANCIES NOTED AT THIS TIME.
ON GEAR DOWN, RECEIVED GEAR UNSAFE LIGHT, NO LIGHT FOR LT MLG & GOT GREEN LIGHT FOR NOSE & RT MAIN. "HYD PRESS ON" LIGHT REMAINED ON. RAN "MLG WILL NOT EXTEND" CHECK LIST. NO CHANGE IN GEAR INDICATIONS. ON DOWN WIND LEG 1500 FT AGL, GOT NORMAL GEAR DOWN INDICATIONS & HYD PRESS LIGHT WENT OUT. LANDED WITHOUT INCIDENT. ON TAXI-IN LT "LOW HYD FLOW" LIGHT ILLUMINATED FOR APPROX 5 SEC THEN WENT OUT. ON POST FLT, NOTICED HYD RESERVOIR INDICATOR IN TAILCONE AT MAX OVERFULL LINE. R & R LT MLG ACTUATOR. ALL WORK IAW MM CH 32-30-04. BLED HYD SYS. PERFORMED GEAR OPS, CHECK 10 TIMES. OPS CHECK GOOD. PERFORMED ENGINE RUNS. OPS CHECK GOOD.
ELECTRIC TRIM WILL NOT TRIM NOSE UP FROM EITHER THE PILOT OR CO PILOT ELECTRIC TRIM. MANUAL TRIM WORKS FULL TRAVEL. REMOVED LT AND RT ELEVATOR TRIM TAB ACTUATORS DUE TO STIFF TRIM. INSTALLED NEW ACTUATORS IAW MM CH 27-32-02, OPS CHECKED AND TRAVEL CHECKED GOOD. LT (P/N: 6660161-13); RT (P/N: 6660161-14).