N566QS

Part: DOOR FRAME — CHAFED (ZONE 200) · airframe 13,731 hrs · 10,396 cycles

EMERGENCY EXIT CUT OUT, HAS A CHAFE LOCATION ON AN EXISTING REPAIR ON INNER WEB BETWEEN F.S. 123.46 AND 131.04. RE COMPLIED WITH EXISTING AQRD ERO-868105 REV IR DATED 10/25/2016 TITLED: CHAFE REPAIR. REMOVED EXISTING REPAIR THAT WAS CHAFED BEYOND ALLOWABLE LIMITS ON INNER WEB BETWEEN F.S. 123.46 AND 131.04. FABRICATED AND INSTALLED NEW RH -002 DOUBLER REPAIR AND RE PROTECTED WITH EPOXY PRIMER.

Part: HINGE — CRACKED (ZONE 800) · airframe 12,741 hrs · 9,634 cycles

DURING 600HR DOOR INSPECTION PER TASK CARD TC-5XL-52-121102, FOUND THE AFT MAIN CABIN DOOR HINGE LOWER HALF IS CRACKED. REMOVED AND REPLACED THE AFT MAIN CABIN DOOR, HINGE HALF ASSEMBLY IAW CE 560XL SRM 51-40-03 AND AMM 52-10-00. OPERATIONAL CHECK GOOD.

Part: HINGE — CORRODED (ZONE 800) · airframe 12,741 hrs · 9,634 cycles

DURING 600HR DOOR INSPECTION PER TASK CARD TC-5XL-52-121102, NOTED SEVERE CORROSION ON THE FWD MAIN CABIN DOOR, FUSELAGE HINGE HALF ASSEMBLY. REMOVED AND REPLACED THE FWD MAIN CABIN DOOR, FUSELAGE HINGE HALF ASSEMBLY, IAW CE 560XL SRM 51-40-03 AND AMM 52-10-00. OPERATIONAL CHECK GOOD.

Part: METERING VALVE — DEFECTIVE · airframe 12,462 hrs · 9,432 cycles

DURING TAXI WHILE BRAKING THE RIGHT BRAKE PEDAL WENT COMPLETELY SOFT FOR A COUPLE SECONDS AND THEN STARTED WORKING AGAIN. REMOVED AND REPLACED THE BRAKE METERING VALVE. IAW CE560XL AMM 32-44-20. OPS CHECK GOOD.

Part: FIRE DETECTOR — DEFECTIVE (LT ENGINE) · airframe 11,163 hrs · 8,497 cycles

LEFT ENGINE FIRE DETECTION LIGHT: THE LEFT ENG FIRE PUSH LIGHT INTERMITTENTLY AND DIMLY FLASHED DURING FLIGHT MULTIPLE TIMES DURING THE SHORT 15 MIN FLIGHT. CLEAR AIR AT 3000 FEET. NO OTHER ABNORMALITIES WERE OBSERVED // SIGNOFF //REMOVED LEFT COWLINGS INSPECTED FIRE SENSOR IAW MODEL 560XL MM 26-11-00 NO DEFECTS NOTED INSTALLED COWLINGS IAW MODEL 560XL MM 71-11-00. REMOVED FIRE DETECTOR P/N:9912036-12 S/N:0825-758 INSTALLED NEW CUSTOMER SUPPLIED FIRE DETECTOR P/N:9912036-12 S/N:2125-553 IAW MODEL 560XL MM 26· 11-02 PERFORMED OPS CHECK IAW MODEL 560XL MM 26-11-00 OPS CHECK GOOD NO DEFECTS NOTED.

Part: VALVE — STICKING (PAX DOOR SEAL) · airframe 10,752 hrs · 8,182 cycles

UPON LANDING THE MAIN CABIN DOOR WAS EXTREMELY DIFFICULT TO OPEN. // SIGN OFF // FOUND THE ACCOUSTIC DOOR SEAL VALVE TO BE STICKING. CLEANED ACCOUSTIC DOOR SEAL VALVE. PERFORMED SEVERAL SUCCESSFUL OPS CHECKS OF THE MAIN CABIN DOOR. ALL WORK PERFORMED REF. CE-560XLS AMM 52-10-00.

Part: STRUT — NOT EXTENDED (NLG) · airframe 8,755 hrs · 6,683 cycles

ALL LANDING GEAR RETRACTION - GEAR WOULD NOT COME UP, GEAR UNSAFE WITH HYD PRESS LIGHT ILLUMINATED, RAN THE APPROPRIATE CHECKLIST CAME BACK AND LANDED WITHOUT EVENT. NOTE, IT WAS NOT AN OVERWEIGHT LANDING.//JACKED AIRCRAFT AND FOUND NOSE STRUT NOT FULLY EXTENDING. REPACKED OLEO IN ACCORDANCE WITH CE560XL CMM 32-20-01 PERFORMED SATISFACTORY GEAR FUNCTIONAL CHECK

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 8,471 hrs · 6,463 cycles

CABIN ODOR BURNING SMELL, COPILOT COMPLAINED ABOUT SOMETHING BOTHERING HIS EYES WHILE CLIMBING OUT WITH APU OFF AND I DIDN'T NOTICE ANYTHING AT THAT TIME. WHILE SITTING ON THE GROUND IN LAS APU ON WITH BLEED AIR ON WE BOTH COULD DETECT WHAT SMELLED LIKE A BURNING SMELL IN THE CABIN OUT OF THE OVER HEAD WEMACS. COMPLIED WITH 72-00-00 OIL SMELL/CABIN ODOR FAULT ISOLATION. FOUND SIGNIFICANT EVIDENCE OF JOINT COMPOUND STREAKING IN RT COMPRESSOR SECTION. REMOVED AND REPLACED RT ENGINE. INSTALLED RENTAL ENGINE. ALSO R&R OZONE CONVERTERS P/N: 9914523-2.

Part: CONVERTER — DIRTY (AC BAY) · airframe 8,464 hrs · 6,458 cycles

COCKPIT ODOR BURNING SMELL - AFTER TAXI OUT, WE SMELLED A SMOKY ODOR COMING FROM OVERHEAD GASPER VENTS. OPENED COCKPIT WINDOW TO VERIFY IT WAS NOT AN OUTSIDE SOURCE. WHEN WE WENT INTO CABIN TO CHECK, THE FRONT OVERHEAD VENTS HAD THE ODOR EVEN STRONGER. CLEANED AND DRIED BOTH CONVERTERS AND SOCKS.

Part: VALVE — FAILED (PARKING BRAKE) · airframe 5,292 hrs · 4,046 cycles

DURING PERFORMANCE A STATIC TAKE OFF, THE LT SEAT BRAKES WOULD NOT HOLD THE AIRPLANE. PERFORMED ENGINE RUNS AND VERIFIED DISCREPANCY. CHECKED FOR CORRECT BRAKE PRESSURE WITH BRAKES APPLIED, NO DEFECTS NOTED. CHECKED LEFT AND RIGHT SEAT BRAKE CABLE TENSIONS, NO DEFECTS NOTED. REMOVED AND REPLACED THE PARKING BRAKE VALVE. BLED BOTH BRAKES, SERVICED RESERVOIR AND ACCUMULATOR. BRAKES NOW HOLD AIRCRAFT FROM EITHER SEAT WITH BOTH ENGINES AT TO POWER. IAW AMM 32-42-03, 32-44-00 AND 32-44-10.

Part: CONTROLLER — FAULTY (FIRE DETECTION) · airframe 4,406 hrs · 3,360 cycles

DURING DECENT TO LANDING, THE RT ENG FIRE LIGHT WAS DIMLY FLICKERING ON & OFF, 1 SECOND ON THEN ABOUT 3 SECONDS OFF, UNTIL LANDING. PLACING THE RT THROTTLE TO IDLE TO DETERMINE IF THERE WAS A BLEED AIR LEAK, THE LIGHT STILL CONTINUED TO FLICKER. ON THE GND THE ROTARY TEST CHECKED NORMAL. VISUALLY INSPECTED RT ENG FIRE LOOP & WIRE HARNESS FROM PYLON TO ENG. PERFORMED RT ENG BLEED AIR LEAK CHECK AT POWER NO LEAKS NOTED AT THIS TIME. R & R RT ENG FIRE DETECTION CONTROLLER IAW CE-560XL MM 26-11-02. OPERATIONS CHECKED GOOD, PN OFF 9912036-12, SN OFF 0825-755, PN ON 9912036-12 & SN 1331-363.

Part: BUNGEE — DAMAGED (MLG) · airframe 3,330 hrs · 2,551 cycles

DURING LANDING ROLLOUT UNEVEN PRESSURE ON BRAKE APPLICATION. THE LT BRAKE PEDAL TRAVELED SIGNIFICANTLY FURTHER THAN THE RT PEDAL CAUSING A JERKING MOTION. AFTER EXITING THE RUNWAY (TRANSFER CONTROLS), PIC TAXIED IN AND NOTICED UNEVEN BRAKE PRESSURE AND A SIGNIFICANT LT BRAKE JERKING MOTION VEERING THE AIRPLANE TO THE LT. R & R NLG UPPER AND LOWER BARREL BEARINGS IAW MM 32-20-01 AND MM 32-20-01. R & R STEERING BUNGEE IAW MM 32-50-00. ALL GEAR OPS CHECKED AND TAXI CHECKED GOOD.

Part: MASTER CYLINDER — READS LOW (BRAKES) · airframe 2,438 hrs · 1,860 cycles

BRAKES ARE VERY SOFT UPON LANDING. ANTI-SKID NEVER ENGAGED ON WET RUNWAY. UPON INSPECTION OF THE BRAKE PRESSURE CYLINDER, NOTICED IT READ LOW. AT 55 DEGREES, SHOULD HAVE BEEN 625-650 AND READ 425. TROUBLESHOT SYS, FOUND BRAKE ACCUMULATOR LOW. SERVICED BRAKE ACCUMULATOR, CHECKED OPERATION OF BRAKES AND ANTI-SKID SYS. OPS NORMAL IAW AMM 12-13-02.

Part: DISPLAY — ERRATIC (HSI) · airframe 1,324 hrs · 993 cycles

STANDBY HSI INDICATIONS ERRACTIC ON BOTH HEADING AND CLIMB AND DESCENT INFORMATION. TESTED AND CONFIRMED ON INITIAL POWER-UP SYS OPERATED NORMALLY. TAXI CHECKED ACFT SYS AND FOUND INDICATOR WOULD ERRATICALLY TILT 5 DEGREES TO THE RT WHILE ACFT WAS STRAIGHT AND LEVEL. REMOVED BAD INDICATOR, PN 501-1741-2103, SN 2132A, AND INSTALLED AN EXCHANGE INDICATOR PN 501-1741-2065A. PERFORMED OPS CHECKS OF ATTITUDE AND HEADING WITH NO DEFECTS NOTED. STBY HSI OPS CHECKED GOOD. INDICATOR LIGHTING OPS CHECKED GOOD. WORK DONE IAW MM 34-22-02.

Part: MONOPOLE — FAILED (LT ENGINE) · airframe 179 hrs · 123 cycles

SHORTLY AFTER TAKEOFF, LT EEC FAILED WITH BOTH EEC'S IN MANUAL. LT ENGINE WOULD COMPRESSOR STALL WHEN N1 REDUCED BELOW 70 PERCENT AND N2 BELOW 85 PERCENT. NO NOTICEABLE RISE IN ITT WAS OBSERVED WITH POWER INCREASES. A SPLIT OF APPROX 2 INCHES IN POWER LEVERS TO MAINTAIN EQUAL THRUST; NR 2 POWER LEVER FWD OF NR 1. REPLACED N2 MONOPOLE IAW 545B MM 77-10-01. REPLACED BOV TORQUE MOTOR IAW PWC MM 75-30-01. REPLACED BOV TORQUE MOTOR ORIFICE IAW MM 71-00-00. LEAK & OPS CHECK GOOD.