N643QS
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
WHEN MAIN CABIN DOOR IS OPEN THE TOP MIDDLE RED DOOR LOCK LIGHT IS NOT LIT. TRIED SEVERAL TIMES CLOSING AND LOCKING DOOR AND CABIN DOOR ANNUNCIATOR WILL NOT EXTINGUISH. TRIED VENT DOOR PROCEDURE PER MAINTENAINCE AND CABIN DOOR ANNUNCIATOR WILL NOT EXTINGUISH. LUBRICATED MED MOVING PARTS. OPS CHECK GOOD. IAW AMM 52-10-00.
CAPTAIN RUDDER PEDAL: DURING TAXI AND WHILE STATIONARY, WE GET A NOISE IN WHEN YOU MOVE RUDDER PEDALS BACK AND FORTH. YOU CAN HERE THE NOISE FROM THE OUTSIDE IN THE NOSE GEAR WELL. IT APPEARS TO BE COMING FROM THE DAMPNER CYLINDER. CORRECTIVE ACTION; VERIFIED THE DISCREPANCY AND SUSPECT THE BUNGEE IS CAUSING THE ISSUE. REPLACED BUNGEE. ADJUSTED ROD END AND SECURED JAM NUT. INSTALLED NEW BOLT AND SELF LOCKING NUT. APPLIED SOME LUBRICATION AS WELL TO THE FORK AND THE CROSS STEERING. PERFORMED OPS CHECK AND OPS CHECKED GOOD OF NOISE. REFERENCE CE-560XLS M.M. 32-50-00.
VERTICAL STABILIZER RH SKIN CRACK (REF AQRD ENGINEERING REPAIR ORDER # ERO-982598)
MAIN DOOR: MAIN CABIN DOOR FLAG SHOWS LOCKED WHEN THE DOOR IS OPEN/UNLOCKED CORRECTIVE ACTION: A REMOVED MCD STEP AND ADJUSTED MIDDLE FWD POSITION SITE AS REQUIRED TO MOVE INTO AND OUT OF SITE HOLE. OPS CK IS GOOD. REINSTALLED MCD STEPS. REF 560XL MM CH 52-10-02.
IN FLIGHT AT 180 KIAS WITH AUTOPILOT ON AT 5000¿ SELECTED FLAPS 15, NOTICED NORMAL TRIM FOR FLAPS & STAB MOVEMENT, THE HYD PRESS STARTED FLASHING WITH ASSOCIATED MASTER CAUTION. NOTICED FLAPS HAD ONLY TRAVELED BETWEEN 0-7 DEGREES. CONFIRMED FLAP HANDLE IN CORRECT POSITION, CYCLED TO 0 DEGREES, STAB & FLAPS MOVED NORMALLY & RETRACTED. SELECTED FLAPS 7, & HAD SAME ISSUE WITH HYD PRESS & FLAPS INDICATING BETWEEN 0 & 7 DEGREES. ELECTED TO LAND WITH FLAPS 0 & COMPLETED ASSOCIATED QRC. T/S TO RIGHT FLAP CONTROL VALVE REMOVED & REPLACED FLAP ACUATOR IAW AMM 27-51-04 OPS CHECKED GOOD.
IN CRUISE FLIGHT HAD LOW BREAK PRESS AND ANITSKID INOP ANNUNCIATOR ILLUMINATE. COMPLETED QRH AND LANDED USING EMERGENCY PHEUMATIC BREAK SYSTEM. REMOVED AND REPLACED PCB NZ004 IN ACCORDANCE WITH CE-560XL MM 24-51-02. COMPUED WITH LANDING GEAR FUNCTIONAL TEST IN ACCORDANCE WITH CE-560XL MM 32-01-00. COMPUED WITH ANTI-SKID OPERATIONAL CHECKS IN ACCORDANCE WITH CE-560XL MM 32-44-00. ALL OPERATIONAL\ FUNCTIONAL CHECKS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
EXIT SIGN OVER MAIN CABIN DOOR AND EXIT SIGNS LEFT AND RIGHT OF MAIN CABIN DOOR INOP. PERFORMED OPS CHECKED OF EMERG. LIGHTING SYSTEM FOUND FWD EMERG. LIGHTS NOT COMING ON WITH LIGHT SWITCH IN THE ON POSITION. REPOSITION BATTERY PACK & OPS CHECK FWD EMERG. LIGHTS CAME ON & AFT EMERG. LIGHTS DID NOT COME ON. POWER UP ACFT &CHARGE BATTERY PACK FOR A HOUR & HALF. PERFORMED OPS CHECK OF EMERG. LIGHTS & AFT EMERG. LIGHTS FLICKER & THEN OFF. BATTERY PACK FAILED. REPOSITION BATTERY PACK BACK TO ORIGINAL POSITION, R & R FWD BATTERY PACK. POWER UP ACFT & CHARGE THE BATTERY PACK. PERFORMED SATISFACTORY OPS CHECK OF EMERG. LIGHTING SYSTEM IAW AM M 33-50-01.
MAIN CABIN DOOR STEPS DROP APPROX 1¿ WHEN STEPPING ONTO THEM. THE DOOR HANDRAIL IS LOCKING DOWN BUT DOESN¿T FEEL LIKE IT¿S GOING FULLY OVER CENTER AND FEELS SPONGY WHEN YOU LOCK THE HANDRAIL DOWN. INSIDE FEELS NORMAL. INSPECTED TO FIND MISSING SPACER IN UPPER OVERCENTER LINK ROD END. INSTALLED NEW SPACER AND ADJUSTED CABIN DOOR OVERCENTER LINK. OPS CHECKS GOOD. REF: CE-560XL AMM 52-10-01.
RIGHT EXTERIOR EMERG LIGHT: RIGHT SIDE FURTHEST AFT EMERGENCY LIGHT INOP. LIGHT BELOW EMERGENCY EXIT DOOR. // SIGNOFF// REMOVED INOP AFT WING EMERGENCY LED LIGHT ASSY AND REPLACED WITH A NEW LED LIGHT ASSY IAW CE-560XLS AMM 33-50-04. OPERATIONAL CHECK GOOD WITH NO FURTHER DEFECTS NOTED. PART NUMBER OFF/ON OWL-100-04. SERIAL NUMBER OFF/ON 115007351/ 115011019
MAIN DOOR HANDLE: ONCE THE MAIN CABIN DOOR IS COMPLETELY CLOSED WITH THE DOOR HANDLE; UPON SUBSEQUENT OPENING, CANNOT GET THE DOOR TO OPEN WITHOUT RELEASING THE PRE-CATCH LEVER. // SIGNOFF// OPENED UP MED DOOR FROM THE OUTSIDE AND OPS CHECKED DOOR, NO DEFECTS NOTED. PERFORMED OPS CHECK OF MED DOOR FROM INSIDE AND HAD TROUBLE OPENING THE MED DOOR, INSPECTED GUIDE RODS AND FOUND DEBRIS ON GUIDE RODS. CLEANED AND RE LUBRICATED GUIDE RODS & PERFORMED OPS CHECK, OPERATIONAL CHECK, CONTACTED MCC AND NOTIFIED THEM OF FINDINGS WORK PERFORMED WITH REFERENCE TO CE·560XLS AMM 52·10·00
CLAFING WAS FOUND AT F.S. 337.625 ON EXISTING INTERIOR REPAIR DOUBLER AT RH SURROUND DOUBLER, EMERGENCY EXIT LOCATION. EMERGENCY EXIT SURROUND DOUBLER CHAFFING REPAIRED IAW AQRD ERO-971959 REV: IR DATED 5/11/22 TITLED N643QS EMERGENCY EXIT SURROUND DOUBLER CHAFFING, APPROVED ON FFA FORM 8110-3 DATED 16 MAY 2022.
DURING PREFLIGHT - SHORTLY AFTER STARTING APU, THE COCKPIT AND CABIN FILLED WITH SMOKE. *** APU PLACED ON MEL REPAIR IN FUTURE *** // SIGNOFF // REMOVED & REPLACED APU ASSEMBLY IAW CE-560XL MIM 49-10-00. LEAK & OPS CHECK GOOD. . S/N P-204 REMOVED UNSERVICEABLE WITH TSN: 13521.5 / CSN: 17015
RIGHT MLG LANDING GEAR EXTENSION: DURING GEAR EXTENSION, THE L MAIN AND NOSE GEAR EXTEND AND LOCK NORMALLY, THE HYD PRESS ANNUNCIATOR THEN EXTINGUISHES AND THE R MAIN GEAR DID NOT EXTEND AND LOCK FOR UPWARDS OF 20 SECONDS. THE RED UNLOCK LIGHT WAS ILLUMINATED UNTIL THE R MAIN SHOWED LOCKED. NO OTHER HYDRAULIC SYSTEMS WERE IN USE AT THE TIME. THE GEAR RETRACTED NORMALLY AFTER TAKEOFF. IT SEEMS THAT THE HYD EXTENDS THE L MAIN AND NOSE AND THEN STOPS. THE R MAIN THEN JUST FREE FALLS WITH NO PRESSURE BEHIND IT. REMOVED RH MLG ACTUATOR IAW CESSNA 560XL MM 32-30-04 (REV 46) AND REPLACED WITH A REPAIRED MLG ACTUATOR IAW MM 32-30-04 (REV 46) STEPS 1 THRU 3A THR B (1) THRU (7). PERFORMED A FUNCTIONAL CHECK OF THE LANDING GEAR NOTICED ACTUATOR LEAKING AT SUPPLY LINE UNION AND B NUT. INSTALLED NEW ORING AND WHITE RETAINER AND RE-INSTALLED UNION ELBOW. PERFORMED LEAKS CHECK . NO LEAKS NOTED. BECAUSE IT IS A NEW ACTUATOR BEING INSTALLED REMOVED ACTUATOR END ATTACHING TO GEAR. PERFORMED MAIN GEAR CAMBER ADJUSTMENT. REINSTALLED ACTUATOR AND PERFORMED FUNCTIONAL CHECK REF AMM 32-30-04. OPS CHECK GOOD. SWUNG QEARS 10 TIMES TO COMPLETE BLEEDING OF SYSTEM. QEARS NOW EXTENDS AT 5.08 SECONDS. AND RETRACTS AT 5.58 SECONDS. DOWN JACKED AIRCRAFT AND SERVICED RESERVOIR. NO OTHER DEFECTS NOTED .
CABIN ODOR - ACM PRODUCES A WET SOCK SMELL WHEN RUNNING IN WARM HUMID CONDITIONS.//SIGNOFF// GAINED ACCESS AND REMOVED OLD CONDENSER BAG P/N: 83237-12, 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 21-51-00
SHORTY AFTER TO A VISIBLE SMOKE WITH ENVIRONMENTAL SMELL APPEARED IN THE COCKPIT, DISSIPATED AFTER APU SHUTDOWN. BY TIME WE LANDED SMOKE AND SMELL WHERE GONE. ALL APPROPRIATE COMPANY PROCEDURES AND FAR'S WHERE COMPLIED WITH. REMOVED AND REPLACED THE APU. RAN THE APU AND OPENED THE BLEED AIR VALVE AND WITHIN 30 SECONDS THE CABIN FILLED WITH SMOKE. REMOVED APU ACCESS DOOR AND PERFORMED GVI AND DID NOT FIND ANY OBVIOUS DEFECTS. NO SIGNS OF OIL OVER SERVICE OR LEAKAGE. ALSO NO SMOKE CAN BE SEEN COMING FROM THE APU WHILE RUNNING. NOTIFIED MCC OF ALL FINDINGS AND THEY CONFIRMED THAT THEY WANT THE APU REPLACED. ALL WORK WAS COMPLETED IAW CE-560XL AMM 49-00-00. AIRCRAFT WAS POSITIONED ON A SLIGHT HILL ON THE RAMP WHERE THE CG OF THE AIRCRAFT WAS IN QUESTION WITH REMOVING THE APU. COORDINATED WITH FBO TO HAVE AIRCRAFT MOVED TO A LEVEL AREA ON THE RAMP. SEE SQUAWK 2.7 FOR APU REMOVAL AND INSTALLATION. PERFORMED OPERATIONAL CHECK OF APU BLEED AIR IAW AMM 49-10-00 AFTER INSTALLATION OF NEW APU; ALL OPS CHECKS GOOD; NO SMOKE NOR ABNORMAL SMELLS WERE NOTED. NO OTHER DEFECTS NOTED AT THIS TIME.
ALL LANDING GEAR RETRACTION - AFTER TAKEOFF SELECTED GEAR UP. RED UNLOCK LIGHT ILLUMINATED. PERFORMED APPROPRIATE CHECKLIST. ON EXTENSION THREE GREEN LIGHTS ON THE GEAR. DECLARED AN EMERGENCY AND RETURNED FOR AN OVERWEIGHT LANDING AT 19900 POUNDS. ACCOMPLISHED A UPLOCK SWITCH INSPECTION ON ALL GEAR WITH SATISFACTORY RESULTS. PREPPED RIGHT HAND ENGINE FOR HYDRAULIC MULE OPERATION. PERFORMED MULTIPLE GEAR SWINGS WITH THE UNLOCK LIGHT REMAINING ILLUMINATED WITH THE GEAR IN THE RETRACTED POSITION. ALSO NOTED THE LOW HYD ANNUNCIATOR ILLUMINATING DURING THE GEAR SWING.PERFORMED AN INSPECTION OF THE HYDRAULIC RESERVOIR WITH THE INDICATION BELOW THE REFILL MARK. ACCOMPLISHED HYDRAULIC SERVICING AS REQUIRED. WITH THE GEAR IN THE RETRACTED POSITION PERFORMED A VISUAL INSPECTION OF THEUPLOCKS AND NOTED THE RIGHT HAND GEAR UPLOCK ACTUATOR NOT IN THE FULL LOCKED POSITION. SPOKE WITH TEAM XL WITH FINDINGS AND RAN THROUGH A GEAR CYCLE WITH THEM ON THE PHONE AS REQUESTED AND WITH FINDINGS AT HAND SUSPECTED THE RIGHT HAND GEAR UP LOCK ACTUATOR TO BE AT FAULT. REMOVED THE UNSERVICEABLE RIGHT HAND GEAR UPLOCK ACTUATOR (P/N: 5527504-3 S/N: 3312). INSTALLED AN RIGHT HAND GEAR UPLOCK ACTUATOR (P/N:5527504-3 S/N:5151) AND ACCOMPLISHED BLEEDING PROCEDURES WITH SATISFACTORY RESULTS. ACCOMPLISHED LANDING GEAR OPERATIONAL CHECKS WITH THE UNLOCK LIGHT REMAINING ILLUMINATED. COMPLETED ADDITIONAL INSPECTION OF THE GEAR IN THE RETRACTED POSITION WITH THE RIGHT HAND GEAR NOT RETRACTING FULLY INTO THE WHEEL WELL NOT FULLY ENGAGING THE UPLOCK. SPOKE WITH TEAM XL WITH ACCOMPLISHED TASK AND FINDINGS AND RECOMMENDED TO INSPECT THE GEAR FOR BINDING AND INTERFERENCE WITH THE GEAR IN THE RETRACTED POSITION. COMPLETED INSPECTION AS REQUESTED WITH NO DEFECTS OR INTERFERENCE NOTED. PERFORMED THE LANDING GEAR TROUBLESHOOTING AND FOUND IN THE PROCESS THAT THE RIGHT HAND RETRACT ACTUATOR HAD ROTATED FROM THE JAMNUT. UPON FURTHER INVESTIGATION NOTED THAT THE LOCK HAD BROKE ALLOWING THE ACTUATOR PISTON TO ROTATE. ROTATED THE RETRACT ACTUATOR BACK TO THE JAM NUT AND ACCOMPLISHED AN ADDITIONAL LANDING GEAR OPERATIONAL CHECK WITH SATISFACTORY RESULTS. SPOKE WITH MCC AND ORDERED A RETRACT ACTUATOR WITH ASSOCIATED PARTS. COMPLETED THE REMOVAL PROCEDURES FOR THE RIGHT HAND RETRACT ACTUATOR (P/N:9912537-4 S/N:1141B) WHILE AWAITING THE REPLACEMENT ACTUATOR TO ARRIVAL. ONCE ARRIVED INSTALLED AN INSPECTED SERVICEABLE RIGHT HAND RETRACT ACTUATOR(P/N:9912537-6 S/N:1742 ) AND ACCOMPLISHED THE BLEEDING PROCEDURES. SERVICED THE HYDRAULIC SYSTEM AS REQUIRED. COMPLETED THE LANDING GEAR OPERATIONAL CHECK WITH SATISFACTORY RESULTS WITH NO DUPLICATION OF THE UNLOCK LIGHT ILLUMINATING WITH THE GEAR IN THE RETRACTED POSITION AND THE UPLOCK FULLY ENGAGING. ACCOMPLISHED THE RIGHT HAND MAIN GEAR CAMBER ADJUSTMENT CHECK WITH NO ADJUSTMENT REQUIRED. PERFORMED A LANDING GEAR OPERATIONAL CHECK AND MULTIPLE CYCLES OF THE GEAR WITH SATISFACTORY RESULTS AND NO DUPLICATION OF THE UPLOCK LIGHT ILLUMINATING WITH THE GEAR RETRACTED. ACCOMPLISHED THE DOWN JACKING PROCEDURES AS REQUIRED. ALL MAINTENANCE ACCOMPLISHED IAW CE-560XLS AMM CH. 07-10-01, 12-12-01, 32-01-00, 32-30-05, 71-00-04, CE-560XLS WDM CH. 32-30-01, 32-30-00, 32-10-00, AND 32-30-04.
COCKPIT ODOR - DIRTY SOCK SMELL. NOTICED DURING DESCENT APU OFF. REMOVED AND REPLACED WATER SEPARATOR CONDENSER BAG AND PERFORMED SYSTEM OPERATIONAL CHECK. NO DEFECTS NOTED. REF: CE 560XL MM 21-51-00
HYDRAULIC PUMP - CLIMBING THROUGH 2000 FEET THE MASTER CAUTION AND HYDRAULIC PRESS ANNUNCIATORS ILLUMINATED. UPON BEGINNING THE EMERGENCY CHECKLIST, THE MASTER CAUTION, LOW HYDRAULIC FLOW RIGHT AND HYDRAULIC PRESS ILLUMINATED. CHECKLIST WAS COMPLETED. LANDING WAS NORMAL. UPON POST FLIGHT, THE HYDRAULIC RESERVOIR IS ABOVE FULL. //SIGNOFF// REMOVED PART NO: 24195-LAA REMOVED SERIAL NO: 4752 DUE TO FAILURE. INSTALLED NEW PUMP IAW CESSNA 560XL MAINTENANCE MANUAL CHAPTER 29-11-03. OPERATIONAL AND LEAK CHECK GOOD.
ON TAXI OUT, POWER BRAKE CIRCUIT BREAKER TRIPPED. RESET ONCE AND IT TRIPPED AGAIN. R & R POWER BRAKE MOTOR. REMOVED PN: MP50B-1, SN:4642, INSTALLED MP50B-1, SN:2658. OPS CHECKED GOOD.
FOUND THE ENGINE FIRE DETECTION WIRE HAD BEEN CONTACTING THE AIRFRAME LT SIDE YOKE, ENGINE ATTACH YOKE, IN THE AREA WHERE THE FIRE DETECTION WIRE IS ROUTED ON THE INBD SIDE OF THE ENGINE AROUND THE ENGINE FLANGE, FAN CASE TO ENGINE INTERMEDIATE CASE. THE FIRE DETECTION WIRE HAD WORN A GROOVE IN THE YOKE. THE FIRE DETECTION WIRE IS UNSERVICEABLE DUE TO A FLAT SPOT WORN INTO IT. THE DISPOSITION OF THE YOKE IS CURRENTLY WITH MFG ENGINEERING.
IN FLIGHT ON TWO SEPARATE OCCASIONS AFTER GND DE ICE WITH TYPE 1 FLUID. ONCE 45 MIN INTO FLIGHT THE 2ND TIME 5 MIN INTO FLIGHT. WING ENG ANTI-ICE WAS SELECTED & A VERY STRONG ACRID SMELL FILLED COCKPIT & WENT AWAY AFTER A FEW MINUTES. THE SMELL WAS VERY DIFFERENT THAN THE NORMAL SMELL WE GET ON TAKEOFF AFTER DE-ICING.
WITH APU BLEED AIR RUNNING THERE IS A STRONG PUNGENT MILDEW ODOR. CLEANED ACM WATER SEPERATOR SOCK IAW MM 12-19-02. NO DEFECTS OR LEAKS NOTED.
DURING TAXI BRAKE CHECK, LEFT BRAKE GRABS SEVERELY AND PULLS AIRCRAFT LEFT ON BOTH SIDES (PILOT AND COPILOT). NO LEAKS FOUND AROUND BRAKE ASSEMBLY. NO LEAKS FOUND AROUND BRAKE ASSY. REMOVED BROKEN LT BRAKE VALVE LEVER RETURN SPRING AND INSTALLED A NEW SPRING. PERFORMED TAXI CHECK WITH NO DEFECTS NOTED, REF AMM 32-40-00.
ON TAXI, ANTI SKID LIGHT ILLUMINATED FOR ABOUT 1-2 SECONDS AND WENT OUT. SLOWED ACFT AND BRAKES SEEMED FINE. CONTINUED TO DECELERATE THE ANTI-SKID LIGHT ILLUMINATED AGAIN ALONG WITH THE MASTER CAUTION CAME ON. APPLIED THE BRAKES AND THE PEDALS WENT TO THE FLOOR WITH NO RESPONSE. PLANE SWERVED ABRUPTLY LEFT. FOUND RT ANTI-SKID WIRE BUNDLE CHAFED THROUGH. R & R WIRE BUNDLE ASSY WITH A NEW UNIT. COMPLETED ANTI-SKID SYS OPS CHECK, OPS CHECKED GOOD. COMPLETED AIRCRAFT FOD AND DAMAGE INSPECTIONS, ALL CHECKS GOOD. ALL WORK DONE IAW MM 32-42-07 & MM 5-50-00.
CLIMBING THRU APPROX 15,000' & APPROX 250KTS THE MASTER CAUTION LIGHT CAME ON THEN WENT OFF. A FEW SECONDS LATER THE STAB MISCOMPARE LIGHT CAME ON MOMENTARILY (APPROX 2 SECONDS). CHECKED THE FLAP HANDLE AND INDICATOR- THEY WERE BOTH IN THE 0/UP POSITION. DISENGAGED THE AUTO PILOT TO FEEL FOR ANY FLIGHT LOADS, STRAIGHT AWAY THE ACFT PITCHED DOWN APROX 15-20 DEGREES. EXTENDED SPEED BRAKES AND SLOWED TO BELOW 200 KTS- AT NO TIME IN THE DESCENT WAS ANY CAUTION LIGHT ON ON THE ANNUC PANEL. DURING THE DESCENT, WAS TRIMMING BACK FOR APPROX 30 SECONDS ON THE ELECTRIC PITCH TRIM. BY APPOX 8000' & 190 KTS, WERE IN LEVEL FLIGHT AND THE FLIGHT LOADS FELT NORMAL. EXTENDED FLAPS AND GEAR AND LANDED WITHOUT INCIDENT. ON THE RAMP, RAN THE FLAPS FROM 0-35 DEGREES 2 TIMES WITH ALL INDICATIONS NORMAL. FROM TAKEOFF TO APPROX 3000' (3 MINS), HAND FLEW THE ACFT , ALL FLIGHT LOADS WERE NORMAL.
STARTING THE APU WITH BLEEDS ON, SMOKE POURED OUT OF THE OVERHEAD WEMAKS AND FLOOR AREA. WITH ENGINES STARTED AND APU OFF SMOKE WAS NOT PRESENT. CONFIRMED THE APU IS THE SOURCE OF THE SMOKE. PREPARED APU TO BORESCOPE APU BORESCOPE COMPRESSOR INLET, NOTED ENGINE OIL PUDDLED AT COMPRESSOR INLET, MFG CONTACTED US AND WAS CONDEMING THE APU AND WILL CONTACT OPERATOR TO GET ORDER, REFER DISC. NR16 FOR APU REPLACEMENT.
STARTING THE APU WITH BLEEDS ON, SMOKE POURED OUT OF THE OVERHEAD WEMAKS AND FLOOR AREA. KLAX-KCLT.
LANDING GEAR IND UNSAFE (LEFTSIDE- NOGREEN- RED UNLOCK ON). INSTALLED REPAIRED LT MAIN LANDING GEAR ACTUATOR, PERFORMED CAMBER CHECK, SLOW CYCLE GEAR AND PURGED AIR FROM SYSTEM, SERVICED EMERGENCY AIR BOTTLE, CYCLED GEAR NUMEROUR TIMES, OPS CHECK GOOD. REF FESSNA MM 32-30-04, 32-10-00, & 32-01-00.
AFTER T/O, EEC MANUAL R ANNUNCIATOR ILLUMINATED, RAT DIGITS DISAPPEARED TO BE REPLACED BY AMBER DASHES, AND R ENGINE N1 RPM DECREASED BY APPROX 10 PERCENT. REMOVED INOP RIGHT ENGINE BOV TORQUE MOTOR AND INSTALLED AN OVERHAULED TORQUE MOTOR. INSTALLED A NEW ORIFICE SIZE. ALL RUN CHECKS GOOD PER EMM 75-30-01. NEW ORIFICE SIZE-30J1296CL48.
RT EEC FAILED DURING TAKE-OFF, ENGINE INDICATIONS WERE IN TRANSIENT LIMTS. [07-09-07] DOWNLOADED RIGHT EEC AND FOUND CODE F1-10 DISPLAYED FOR BLEED VALVE TORQUE MOTOR. CHECKED WIRING BETWEEN TORQUE MOTOR AND EED NO DEFECTS NOTED. REMOVED AND REPLACED TORQUE MOTOR WITH OVERHAULED UNIT USING NEW PARTS. GROUND RAN ENGINE RAN ENGINE. OPS AND LEAK CHECK WAS GOOD. WORK PERFORMED PER PWA 545 MM.
NOTICEABLE VIBRATION OF CONTROL COLUMN DURING TAKEOFF,CLIMB,REDUCED DURING. CRUISE AND BEGINS TO BE MORE NOTICEABLE DURING DECENT AND LANDING. TROUBLESHOT ELEVATOR SYSTEM. FOUND LEFT AND RIGHT ELEV. TRIM TAB BEARINGS TO HAVE EXCESSIVE PLAY. REMOVED AND REPLACED L/R TRIM TAB BEARINGS WITH NEW UNITS. SYSTEM CHECKS GOOD AT THIS TIME. IAW CE560 XLS M/M
DURING APPROACH, BOTH ENGINE FIRE LIGHT SWITCHES FLASHED SIMULTANEOUSLY MULTIPLE TIMES. UNABLE TO DUPLICATE, CLEANED CONNECTORS ON ROTARY TEST SWITCH. TESTED ANNUNCIATOR IAW MM 31-11-00 ALL TESTS NML
RUDDER PEDALS BIND WHEN DEFLECTED EITHER SIDE OF NEUTRAL. PEDALS ALSO HAVE A BINDING SOUND WHEN DEFLECTED EITHER SIDE OF NEUTRAL. VERIFED NOISE, FOUND STEERING BUNGEES LOOSE AND DRY. CLEANED, LUBED, AND RESECURED STEERING BUNGEES. TAXI AIRCRAFT. STEERING OPS CHECKED GOOD AND NO BINDING NOISE HEARD. WORK DONE IAW CE560XL AMM CHAPTER 32-50-00.
NO (GREEN LIGHT) INDICATION ON RT MAIN LANDING GEAR. PERFORMED APPROPRIATE CHECKLIST USING EMERGENCY EXTENSION, BLOW DOWN UNSUCCESSFUL, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT GEAR INDICATOR BULBS OPS CHECKED GOOD, IAW MM 33-10-01. PERFORMED GEAR FUNCTIONAL CHECK, CHECKED GOOD IAW MM 32-01-00.