N306QS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,287 hrs · 9,601 cycles

EMERGENCY EXIT WINDOW SHADE IS FAILED IN AN 80% CLOSED POSITION INHIBITING VISIBILITY IN THE EVENT OF AN EMERGENCY EGRESS. ATTEMPTED TO OPEN THE SHADE USING ALL THREE CONTROL PANELS (GALLEY, SEAT 6 AND LAV PANELS.) ///SIGN-OFF/// ADJUSTED WINDOW SHADE. NO DEFECTS NO1ED. OPS CHECKED GOOD. IAW MODEL 680 AMM 25-20-25.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 14,109 hrs · 9,462 cycles

DIFFICULT TO OPEN / CLOSE THE MAIN CABIN DOOR FROM OUTSIDE OF ACFT. REQUIRES BOTH HANDS & ESTIMATED 40 PLUS POUNDS OF FORCE TO MOVE DOOR HANDLE DOWN. UPPER 4 GUIDE ROLLERS APPEAR TO BE HAVE ACCESS WEAR. PERFORMED ADJUST OF MED UPPER & LOWER LATCH ROLLERS IAW AMM 52-10-00. PERFORMED OPS CHECK OF MED IAW 52-10-00. CHECK GOOD. DOOR OPERATES NORMALLY. PERFORMED OPS CHECK OF STEP LIGHTS. CHECK GOOD. PERFORMED FINAL OPS CHECK OF CABIN DOOR. CABIN DOOR DIFFICULT TO OPEN ONCE AGAIN. PERFORMED ADJUSTMENTS OF UPPER & LOWER LATCH ROLLERS. AFTER FINAL ADJUSTMENTS, PERFORMED OPS CHECKS OF CABIN DOOR. OPS CHECK GOOD AT ALL TIMES. NO FURTHER DEFECTS NOTED.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,610 hrs · 9,144 cycles

EMERGENCY LIGHTS DO NOT COME ON WITH THE SWITCH IN ON. THEY DO COME ON IN ARM. HOWEVER, THE AFT OVER-WING AND THE LAV EXIT LIGHT DO NOT COME ON UNTIL SHIP POWER IS AVAILABLE. TROUBLESHOT DISCREPANCY DOWN TO #4 EMERGENCY BATTERY & CHARGER SYSTEM. REMOVED & REPLACED #4 EMERGENCY BATTERY & CHARGER SYSTEM WITH REPAIRED UNIT. OPS CHECK GOOD. IAW MM 33-50-10 FOR MX PERFORMED.

Part: STRUT — BROKEN (PAX DOOR) · airframe 13,460 hrs · 9,030 cycles

MAIN HANDLE WAS UNLOCKED. DOOR WAS PUSHED SLIGHTLY AND CREW MEMBER GRABBED RIGHT DOOR ASSIST HANDLE WHEN LOUD SNAP WAS HEARD JERKING HANDLE FROM HIS HAND AND DOOR CRASHED TO FULL OPEN. STRUT BROKEN AND UNABLE TO CLOSE DOOR. REMOVED AND REPLACED DAMAGED FWD STRUT ASSY SUPPORT. REMOVED DAMAGED STRUT ASSY SUPPORT FWD. INSTALLED NEW STRUT ASSY SUPPORT FWD. PERFORMED OPS CHECKS ON MAIN DOOR, OPS CHECKS WERE SATISFACTORY. WORK PERFORMED IAW AMM 52-10-30.

Part: STRUT — DETERIORATED (NLG) · airframe 10,769 hrs · 7,193 cycles

CHROME FINISH IS DETERIORATING AND PITTING IN NLG LOWER BARREL ASSEMBLY. REMOVED EXISTING LOWER BARREL ASSEMBLY AND INSTALLED NEW CUSTOMER SUPPLIED LOWER BARREL ASSEMBLY IN THE SAME LOCATION. REF. CESSNA 680 CMM 32-20-01.

Part: FITTING — CORRODED (VERTICAL STAB) · airframe 10,769 hrs · 7,193 cycles

REPAIRED CORROSION ON VERTICAL STABILIZER AFT SPAR, LT SPAR CLIP APPROXIMATELY 11 INCHES ABOVE LOWER RUDDER HINGE BY MECHANICAL BLENDING, PERFORMING NDT, TREATING, PRIMING, AND TOP COATING PER REPAIR MEMO.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 10,643 hrs · 7,104 cycles

OILY BLEED AIR SMELL IN COCKPIT AND CABIN WITH ACM RUNNING. STARTS WHEN APU BLEED AIR IS TURNED ON AND CONTINUES INFLIGHT. AFTER A 1 HOUR FLIGHT WITH APU OFF SMELL WAS STILL PRESENT IN COCKPIT. ****** CORRECTIVE ACTION ***** ACCOMPLISHED VISUAL & BORESCOPE INSPECTION OF APU WITH NO DEFECTS NOTED. ACCOMPLISHED TASK CARD#: TC-680-21-120905M ECS DUCT BURN OUT PROCEDURE AS OUTLINED IN TASK CARD. REMOVED AND REPLACED COALESCER WITH CUSTOMER SUPPLIED PART, PIN: 83237-12, SIN: NIA. IAW: MM CHAP.12-19-00. LEAK & OPERATIONALLY CHECKS GOOD. ALSO CHECKED APU OIL SERVICE, OIL SERVICE CHECKED GOOD. IAW: MM CHAP. 12-20-49, AND ENGINE/SYSTEM MM CHAP. 49-00-00. RAN APU 1 .5 HRS. WITH NO OIL SMELL NOTED, ALSO RAN BOTH ENGINES FOR AN HOUR WITH NO OIL SMELL NOTED.

Part: SWITCH — INTERMITTENT (RT MLG) · airframe 10,440 hrs · 6,964 cycles

RIGHT MLG LANDING GEAR RETRACTION - AFTER TAKEOFF RT MAIN GEAR GREEN DOWN LIGHT REMAINED ILLUMINATED. AFTER A COUPLE MINUTES THE LIGHT WENT OUT. THE CREW IS CERTAIN THE RT GEAR WAS UP AS NORMAL. NO RED LIGHT WAS OBSERVED DURING THIS EVENT (RED INDICATED LIGHT MEANS LANDING GEAR MISCOMPARE). TROUBLESHOT TO RIGHT HAND MAIN LANDING GEAR DOWNLOCK SWITCH. JACKED AIRCRAFT, AND REMOVED AND REPLACED SWITCH. ADJUSTED SWITCH, GEAR SWINGS GOOD AT THIS TIME WITH NO ISSUES. OPS CHECKS GOOD AT THIS TIME. DOWN JACKED AIRCRAFT. APPLIED SEALANT TO SWITCH, ENSURED IT WAS CURED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 10,382 hrs · 6,920 cycles

COCKPIT SMOKE - IN CRUISE AT 43,000 FEET WITH THE TEMPERATURE FOR THE CABIN AND COCKPIT SELECTED FULL COLD, THE CREW NOTICED A HOT SMOKY SMELL AND SAW A LIGHT, UNIFORM DISTRIBUTION OF GRAY SMOKE THROUGHOUT THE CABIN AND COCKPIT. IN ACCORDANCE WITH THE EMERGENCY/ABNORMAL CHECKLIST WE SELECTED THE LEFT PRESSURE SOURCE SELECTOR AND THE SMOKE CLEARED. //SIGNOFF//PER TROUBLE SHOOTING TREE, NO FAULT CODES PRESENT, NO CAS MESSAGES PRESENT INSPECTED OIL LEVEL FOUND WITHIN I MRTS. INSPECTED LP COMPRESSOR IAW MM CHAPTER 72-3~1 WITH NO DEFECTS NOTED. INSPECTED AGB OVERBOARD BREATHER TUBE 72-62--01, NO DEFECTS NOTED. MM CHAPTER 72-00-00 TABLE 101 FIGURE 112. COMPHED WITH CABIN/COCKPIT TEMP CONTROL SYSTEM CHECK IAW MM CHAPTER 21-61--00 VENFIED ALL VALVES ARE FULLY OPENING AND CLOSING. OPS CHECK GOOD COMPLIED WITH ENGINE RUNS ON BOTH LEFT AND RIGHT PER PILOTS POH DISCREPANCY DID NOT DUPLICATE. ALL OPS AND LEAK CHECKS GOOD NO DEFECTS NOTED

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 9,829 hrs · 6,545 cycles

RT MLG RETRACTION DID NOT RETRACT, RT MLG FAILED TO RETRACT WHEN THE LANDING GEAR HANDLE WAS SELECTED UP. GREEN RT GEAR INDICATION REMAINED ILLUMINATED FOR ABOUT 5 MINUTES AFTER THE LANDING GEAR HANDLE WAS SELECTED UP. RED UNLOCK LIGHT DID NOT ILLUMINATE. LANDING GEAR RETRACTED ON ITS OWN. LANDING GEAR EXTENDED PROPERLY. TECHS JACKED AND SWUNG GEAR MULTIPLE TIMES. PERFORMED GVI OF GEAR WELLS WITH NO DISCREPANCY FOUND. ALL FUNCTIONS OF THE GEAR WARNING SYSTEM INDICATIONS AND GEAR EXTENSIONS AND RETRACTION OPERATIONS ARE CHECKING NORMALLY. CONTACTED MANUFACTURER THIS CONFIRMED SYSTEM IS WORKING PROPERLY. TECHS COULD NOT DUPLICATE DISCREPANCY ON GROUND. ALL WORK PERFORMED IN REF TO 32-10-00, 32-20-00 32-00-00 MM

Part: COMPRESSOR — STALLED (ENGINE) · airframe 8,404 hrs · 5,584 cycles

DURING TAKEOFF ROLL ABOVE 80 KTS, THE AIRCRAFT YAWED TO THE LEFT ACCOMPANIED BY A COMPRESSOR STALL SOUND IN THE COCKPIT. ABORTED TAKEOFF AT HIGH SPEED, BRAKES AND TIRES ALSO REQUIRE INSPECTION. PERFORMED VISUAL INSPECTION OF ALL BRAKES AND TIRES WITH NO DISCREPANCIES NOTED. CHECKED ALL TIRE PRESSURES WITH NO DISCREPANCIES NOTED. PERFORMED VISUAL INSPECTION OF RUDDER BIAS ACTUATOR WITH NO DISCREPANCIES NOTED. PERFORMED OPERATIONAL CHECK OF RUDDER BIAS WITH NO DISCREPANCIES NOTED. ALL WORK PERFORMED IAW AMM 27-20-10, 32041099, PERFORMED BORESCOPE INSPECTION OF LH ENGINE WITH NO SIGNIFICANT FINDINGS. PERFORMED OPS CHECKS OF RT AND LT BOV'S WITH NO DISCREPANCIES NOTED. PERFORMED LH AND RH POWER ASSURANCE CHECKS WITH NO DISCREPANCIES NOTED. ALL WORK PERFORMED IAW EMM 72-00-00, AND 71-00-00.

Part: B-NUT — LOOSE (APU) · airframe 5,895 hrs · 3,936 cycles

DURING TAKEOFF WITH ENGS & APU RUNNING, ODOR OF FUEL & EXHAUST IN COCKPIT. SMELL DISSIPATED ABOUT 2000 FEET AGL. SHUTDOWN APU, ODOR DID NOT REOCCUR DURING FLIGHT. RAN APU, LT & RT ENGS TO TAKEOFF POWER. COULD NOT DUPLICATE DISCREPANCY. INSPECTED ENGS FOR FUEL LEAKS, NO LEAKS FOUND. INSPECTED APU, FOUND FUEL NOZZLE AT THE 5 O'CLOCK POSITION B NUT & CONNECTING FUEL LINE B NUT LOOSE. TIGHTENED B NUTS & RAN APU FOR LEAK CHECK. LEAK CHECKS GOOD IAW MM 49-30-06. LEAK & OPERATIONS CHECKED GOOD, CLOSED ACCESS ITEMS. COMPLIED WITH TASK CARD TC-680-21-120905M ECS DUCT BURN OUT.

Part: ATTACH ANGLE — CORRODED (TAILCONE) · airframe 5,746 hrs · 3,825 cycles

CORROSION WAS FOUND UNDER NUTPLATES ON LT SIDE OF APU INLET FAIRING ATTACHMENT. REPAIRED LT & RT LOWER RUDDER FAIRING ATTACHMENT ANGLES IAW ERO-593764 REV IR, DATED JULY 15, 2014. FAIRING ANGLE REPAIR THIS IS CONSIDERED A MINOR REPAIR. SDR COMPLETED.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 5,423 hrs · 3,607 cycles

NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. INDICATED GREEN WITH RED UNLOCK ILLUMINATED. LOWERED HANDLE GEAR INDICATED ALL THREE GREEN WITH NO RED UNLOCK, LANDED NORMALLY. JACKED AIRCRAFT, RAN GEAR NUMEROUS TIMES, COULD NOT DUPLICATE. CLEANED UP LOCK SWITCHES AND LUBRICATED. CLEANED AND LUBRICATED DOWN LOCK SWITCHES. CHECKED SWITCH RIGGING. RIG CHECK GOOD. CHECKED NOSE STRUT SERVICE, STRUT SERVICE GOOD. REF CE-680 MM 20-00-0. AND 32-20-00.

Part: STEERING UNIT — MALFUNCTIONED (NLG) · airframe 3,812 hrs · 2,570 cycles

AFTER TAKEOFF, AND LANDING GEAR RETRACTION, NOSE GEAR INDICATOR REMAINED GREEN ACCOMPANIED BY THE RED UNLOCK LIGHT. CREW FOLLOWED ALL CHECKLISTS AND RETURNED FOR LANDING WITHOUT FURTHER INCIDENT. TROUBLESHOT TO BAD NOSE WHEEL STEERING UNIT REMOVED AND REPLACED NWS UNIT IAW CE-680 M/M CHAPTER 32-50-00. ADJUSTED NWS CABLES IAW MM 32-50-00. TRAVEL CHECKS GOOD, RIGGING AND OPS CHECKED GOOD IAW 32-50-00. RETRACT CENTERING AND LEAK CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 3,228 hrs · 2,171 cycles

DURING CLIMB OUT NOTICED OIL ODOR. ODOR DISSIPATED AND REOCCURED 20 MINUTES LATER. MOST NOTABLE FROM COCKPIT SIDE WEMACS. LESSER ODOR IN CABIN, 15 MINUTES LATER ODOR DISSIPATED ONLY TO REOCCUR UPON LANDING. RAN BOTH ENGINE ON GROUND WITH ACM IN THE OFF POSITION AND NO ODOR WAS NOTED IN CABIN OR COCKPIT. RAN ENGINES AND APU, NO ODOR NOTED. INSPECTED ENGINE INLETS EXHAUSTS AND DIFUSERS. NO OIL RESIDUE NOTED. INSPECTED APU INLET, EXHAUST DRAIN TUBES AND BLEED AIR TUBED. NO OIL RESIDUE NOTED. INSPECTED WATER SEPARATOR AND DOWN STREAM BLEED AIR PLUMBING. NO OIL RESIDUE NOTED. PERFORMED OPS & LEAK CHECKED GOOD. WORK DONE IN REF MM 49-00-00.

Part: STRUT — DISCHARGED (NLG) · airframe 2,261 hrs · 1,540 cycles

AFTER TAKEOFF THE GEAR HANDLE WOULD NOT MOVE. RECEIVED WOW MISCOMPARE MESSAGE. AFTER A FEW MINUTES THE CAS MESSAGE WENT OUT. RAISED THE GEAR HANDLE: NOSE LIGHT EXTINGUISHED, RT AND LT MAIN AND RED UNLOCK LIGHT REMAINED ON. PUT THE GEAR HANDLE BACK DOWN. FOUND WHEEL SQUAT SWITCH NOT MAKING CONTACT DUE TO NOSE STRUT EXTENSION. SERVICED NOSE STRUT IAW MM 32-20-00. PERFORMED NUMEROUS GEAR SWINGS WITH NO DEFECTS NOTED.

Part: STEERING UNIT — FAILED (NLG) · airframe 2,010 hrs · 1,379 cycles

AFTER TAKEOFF THE NOSE GEAR WOULD NOT RETRACT. R & R NOSE STEERING UNIT IAW MM 32-60-00. OPS CHECKED GOOD. GEAR SWINGS OPS CHECKED GOOD.

Part: CHIP DETECTOR — CONTAMINATED (OIL SYSTEM) · airframe 1,420 hrs · 968 cycles

RT OIL PRESSURE INIDCATION WENT BELOW 20 PSI. RED OIL PRESSURE LIGHT ILLUMINATED. ENGINE SHUTDOWN ACCOMPLISHED. REMOVED CHIP DETECTOR, FOUND FUZZ. REMOVED OIL FILTER, TOOK SOAP SAMPLE. REMOVED STARTER GEN & SEAL, FOUND RUBBER DEBRIS ON SHAFT. DOWNLOADED EDU'S. COMPLIED WITH SB 25353R1. REINSTALLED ALTERNATOR & STARTER GEN IAW MM 24-20-10 & 80-10-00. PERFORMED ENG OIL FLUSH. DRAINED OIL FROM GEARBOX & INSTALLED NEW OIL FILTER. RAN ENGS AT 80 % FOR 10 MINS. REMOVED & INSTALLED NEW FILTER & CHIP DETECTOR; NO DEBRIS NOTED. DRAINED & SERVICED OIL. RAN ENGS AT 80 % FOR 10 MINS. REMOVED AND REINSTALLED OIL FILTER & CHIP DETECTOR, NO DEBRIS FOUND. . RAN ENG'S LEAK CKD GOOD IAW MM 72-00-00.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 568 hrs · 403 cycles

AFTER DEPARTURE, THE NOSE WHEEL FAILED TO RETRACT. THE GREEN NOSE WHEEL LIGHT AND RED GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. JACKED ACFT AND PERFORMED LANDING GEAR ADJUSTMENT TEST IAW 32-00-00 AND NOTED NLG WILL RETRACT BUT NOT LOCK IN THE UP POSITION. DISCONNECTED NLG DOOR ROD END AND PERFORMED GEAR SWING WITH NLG NOW LOCKING IAW MCC, CHECKED NLG STRT SERVICING WITH NO DEFECTS FOUND. COMPLIED WITH NLG EXTENSION AND RETRACTION IAW MM 32-30-00. RECONNECTED BOTH NOSE GEAR DOORS PUSH RODS AND COMPLIED WITH FOLLOW ON GEAR SWINGS USING HYD. TESTED WITH NO DEFECTS NOTED.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 568 hrs · 403 cycles

AFTER DEPARTURE, THE NOSE WHEEL FAILED TO RETRACT. THE GREEN NOSE WHEEL LIGHT AND RED GEAR UNSAFE LIGHTS REMAINED ILLUMINATED.

Part: PITOT LINE — OBSTRUCTED · airframe 110 hrs · 82 cycles

COPILOTS A/S INDICATOR WAS NOT INCREASING ABOVE 35 KTS. PILOTS INDICATOR WAS INDICATING 80KTS. CHECK TWICE WITH SAME RESULTS. FOUND AIRSPEED LAGGING ON CO-PILOTS SIDE INCREASING AND DECREASING LEAK CKS GOOD. SUSPECT BLOCKAGE. DISCONNECTED AND FLUSHED LINE. REMOVED BLOCKAGE. RECONNECTED LINE LEAK AND OPS CHECK GOOD. IAW MM 34-11-00 LEAK CHECK IAW FAR 91.411.

Part: INDICATOR — READS LOW (AIRSPEED)

COPILOTS A/S INDICATOR WAS NOT INCREASING ABOVE 35 KTS. PILOTS INDICATOR WAS INDICATING 80KTS. CHECK TWICE WITH SAME RESULTS. (A)

Part: BRAKE ASSY — UNKNOWN (RIGHT) · airframe 6,991 hrs · 6,030 cycles

RT BRAKE PEDAL ON CO-PILOT SIDE IS SOFT. CAPTAIN SIDE BRAKES ARE GOOD. REMOVED LT MASTER CYLINDER, INSTALLED NEW UNIT. REMOVED RT CO-PILOTS MASTER CYLINDER & INSTALLED NEW UNIT. REMOVED PUMP RELAY AND INSTALLED NEW RELAY. BLED BRAKES IAW C560 MM 32-42-00 FOR ALL OTHER WORK REF C560 MM 32-42-02 BRAKE SYSTEM OPERATES NORMALLY.

Part: BRAKE — INADEQUATE · airframe 6,987 hrs · 6,028 cycles

WHEN BOTH BRAKE PEDALS ARE DEPRESSED, THE RT ONE IS MUCH SOFTER THAN THE LT. THIS HOLDS FOR BOTH THE CAPTAIN AND FIRST OFFICER RESPECTIVE SIDES. VISUALLY INSPECTED RT BRAKE ASSY AND LINES. PERFORMED BRAKE BLEED ON RT SIDE IAW MM 32-42-00. TAXIED ACFT AND BRAKE SYSTEM PERFORMED NORMAL. NO LEAKS NOTED.

Part: GCU — INOPERATIVE (LEFT) · airframe 6,219 hrs · 5,186 cycles

ON GROUND AT PBI, LEFT GENERATOR WILL NOT TAKE ANY LOAD EVEN WHEN RIGHT GENERATOR IS IN THE OFF POSITION. PAX SAID THERES WAS A ELECTRICAL SMELL IN BACK IF AIRCRAFT. REMOVED INOP LT GCU P/N51525-001F. INSTALLED REPAIRED CUSTOMER SUPPLIED GCU P/N51525 -001F S/NY1463. OPS CHECK GOOD WITH NO DEFECTS NOTED. ALL WORK DONE IAW CESSNA CITATION ULTRA 560 MM CH 24-31-01.

Part: SENSE LINE — LEAKING (COMPRESSOR P3) · airframe 5,331 hrs · 4,661 cycles

LEFT ENGINE FLAMED OUT (STOPPED RUNNING) APPROXIMATELY 7-10 MINUTES AFTER A NORMAL START. THROTTLE WAS AT IDLE AND HAD NOT BEEN MOVED. ADJUSTED FCU AND FDU LINKAGES PER PRATT & WHITNEY JT15D-5D MM CHAPTER 73-20-01. OPERATIONAL CHECK SATISFACTORY. FOUND COMPRESSOR DELIVERY P3 LINE LEAKING. REMOVED AND REPLACED P3 LINE WITH A MANUFACTURED LINE FROM PRATT & WHITNEY. DOT APPROVAL 4-58 PER PRATT & WHITNEY JT15D-5D MM CHAPTER 73-10-04. LEAK CHECK SATISFACTORY.

Part: WARNING LIGHT — ILLUMINATED (AOA HEATER) · airframe 5,109 hrs · 4,464 cycles

AOA HEATER ANUNCIATOR ILLUMINATED WITH PITOT/STATIC HEAT ON, ABORTED TAKEOFF. OPS CHECKED AOA HEATER SEVERAL TIMES. COULD NOT DUPLICATE DISCREPANCY. NO DEFECTS FOUND AT THIS TIME.

Part: CONTROL LEVER — MALFUNCTIONED (THROTTLE) · airframe 4,741 hrs · 4,169 cycles

LEFT ENGINES SHUTS DOWN WHEN THROTTLE BROUGHT BACK TO FLIGHT IDLE. SUSPECT QUADRANT SWITCH. RAN ACFT, FOUND IDLE TO LOW. PERFORMED POWER CONTROLS ADJUSTMENT, SET IDLE, FLIGHT IDLE ADJUSTMENTS. CHECKED TAKEOFF POWER AND CUTOFF. OPS CHECK GOOD ALL IAW CE560 MM 71-01-03.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 4,738 hrs · 4,167 cycles

LEFT ENGINE SHUTDOWN WHEN THROTTLES WERE BROUGHT IDLE. PERFORMED LT ENGINE RUN OPERATIONAL CHECK AND NO DEFECTS NOTED. REMOVED LT LOWER COWLING TO INSPECT FUEL CONTROL, STARTER GENERATOR, AND INSPECTED QUADRANT AND NO DEFECTS WERE NOTED. COULD NOT DUPLICATE SQUAWK. ALL WORK DONE IAW CE 560 ULTRA MM CHAPTER 71-01-02, 73-30-03, 24-31-00 & 76-11-00.

Part: BRAKE — MALFUNCTIONED (ANTI SKID SYS) · airframe 3,249 hrs · 2,962 cycles

NO BRAKING ACTION WITH LT OR RT PEDALS. ANTI-SKID LIGHT ILLUMINATED ONCE EMERGENCY BRAKING WAS SELECTED. FOUND FAULTY LT ANTI-SKID TRANSDUCER, REPLACED AND BLED SYSTEM.