N696QS

Part: HOSE — LEAKING (ZONE 700) · airframe 6,381 hrs · 4,232 cycles

UPON REACHING END OF RUNWAY 34 WE HEARD A THUD WHEN SETTING PARKING BREAK AND GOT A PARK BRAKE LOW PRESS AMBER CAS MESSAGE. THERE WAS A PUDDLE UNDER RIGHT MAIN WHEN WE TURNED AROUND TO TAXI BACK TO RAMP AND THERE IS FLUID ON RIGHT MAIN STRUT. CORRECTIVE ACTION: REPLACED BRAKE HOSE. OPS CHECK GOOD. IAW AMM 32-10-05, 32-42-00, 32-44-10.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 5,665 hrs · 3,732 cycles

ALL INTERIOR AND EXTERIOR LIGHTS ASSOCIATED WITH BATTERY PACK #3 FAIL TO ILLUMINATE WITH PREFLIGHT TEST AND ASSOCIATED QRH CHARGING PROCEDURE WITH 60 MINUTES OF TOTAL CHARGING. TROUBLESHOT THE #3 BATTERY PACK G-SWITCH TO HAVE BEEN TRIPPED WHEN RESET THE PACK ALLOWED THE LIGHTING TO STAY ILLUMINATED ONLY WITH AIRCRAFT BATTERY POWER APPLIED. PERFORMED BATTERY EXERCISE PROCEDURE #3 BATTERY WOULD NOT HOLD A CHARGE REMOVED #3 EMERGENCY BATTERY PACK P/N 2503 S/N 42182 INSTALLED CUSTOMER SUPPLIED NEW BATTERY PACK P/N 2503 S/N 49688 PERFORMED BATTERY EXERCISE PROCEDURE NO DEFECTS NOTED OPERATIONS CHECKS SATISFACTORY WORK PERFORMED IN REFERENCE TO AMM 33-50-06, AND RADIANT POWER CORP SIL -CBS2S-1-2024-001 REV A.

Part: BATTERY PACK — FAULTY (ZONE 200) · airframe 5,286 hrs · 3,486 cycles

DURING PRE-FLIGHT WITH THE AIRCRAFT BATTERIES OFF AND ALL GEN SOURCES OFF AND THE EMER LIGHT SWITCH IN ARM, ONLY SOME OF THE INTERIOR LIGHTS WERE ILLUMINATED. WE COMPLETED 2- 30MINUTE CHARGING SESSIONS USING THE APU FOR A TOTAL OF 60 MINUTES OF CHARGING ACCORDING TO THE QRH. AFTER 60 MINUTES OF CHARGING WITH AIRCRAFT BATTERIES OFF AND GENERATOR SOURCES OFF AND THE EMER LIGHT SWITCH IN ARM, THE REAR BULKHEAD EXIT SIGN, LAV SEAT EXIT SIGN AND LAV AISLE LIGHT ARE INOP. WITH BATTERIES OFF AND GEN SOURCES OFF AND EMER LIGHT SWITCH IN THE ON POSITION, NO EMERGENCY LIGHTS ILLUMINATE THEREFORE WE CANNOT MEL ACCORDING TO THE OPERATIONAL PROCEDURES OF THE MEL. CORRECTIVE ACTION; REPLACED FAULTY #4 BATTERY AS PER CE-680A AMM 33-50-06 PARA 5 (C) PERFORMED AN OPERATIONAL CHECK AS PER CE-680A AMM 33-50-00 WITH NO DEFECT NOTICE AT THIS TIME.

Part: BUSHING — OUT OF ADJUST (MAIN DOOR)

MAIN DOOR: EVALUATE MAIN ENTRY DOOR FOR PROPER ADJUSTMENT. IN THE OPEN POSITION, FORWARD HINGE AREA APPEARS TO RUB. MED HAS NORMAL FUNCTION IN ALL OTHER RESPECTS. CORRECTIVE ACTION: ADJUSTED FWD ADJUSTMENT BUSHING. AND ADJUSTED HINGE EXCENTRIC AND LOCKING PLATE IAW CE-680A MM 52-10-00

Part: SEAL — DIRTY (MAIN DOOR) · airframe 5,127 hrs · 3,363 cycles

MAIN DOOR: MAIN DOOR BINDS WHEN CLOSING AND WILL NOT OPEN FREELY. I HAVE TO FORCE THE DOOR TO MAKE IT FREE FALL CORRECTIVE ACTION: CLEANED MAIN DOOR SEALS AND SUROUNDING AREA OF MAIN DOOR APPLIED LUBE TO THE MAIL DOOR SEAL AND MAIN DOOR SURROUND, PERFORMED A SATISFACTORY OPS CHECK OF THE MAIN DOOR OPEN AND CLOSE REF CE-680A, AMM 52-10-00. ACCESSED MAIN DOOR AND FOUND LOWER PART OF THE INNER SEAL HANGING OUT OF POSTION AND NOT SECURED PROPERLY. RESCURED INNER SEAL PROPERLY REF CE680A AMM 52-10-00.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 5,114 hrs · 3,352 cycles

EMERGENCY LIGHT FAILED POST FLIGHT SEAT 3 AND OVERWING RIGHT SIDE. SEE PREVIOUS WRITE UP REPLACED #2 EMERGENCY BATTERY PACK REF. CE680A MM 33-50-00 & 33-50-06. OPS CHECK GOOD.

Part: BATTERY PACK — DEFECTIVE (ZONE 200) · airframe 5,113 hrs · 3,351 cycles

EMERGENCY LIGHTING: DURING EMER LIGHT CHECK IN ARM. NO EMER LIGHTS WORK. WITH EMER LIGHT SWITCH ON. EXIT LIGHT OVER MAIN DOOR NOT ON. OVERHEAD AT SEAT 3 AND 10 NOT ON. WHEN FULL AIRCRAFT POWER IS AT 28 VOLTS , ALL EMER LIGHTS ON. CORRECTIVE ACTION: REMOVED AND REPLACED #1 EMERGENCY BATTERY PACK IAW CE-680A MM 33-50-06. OPS CHECK GOOD.

Part: DOOR — OUT OF TOLERANCE (ZONE 800) · airframe 5,066 hrs · 3,315 cycles

MAIN DOOR: MAIN ENTRY DOOR IS BINDING AND FAILS TO OPEN ON ITS OWN. IT ONLY OPENS ABOUT 1" AND THEN HAS TO BE PULLED/PUSHED BEYOND THAT POINT. CORRECTIVE ACTION: FOUND CABIN DOOR TO BE OUT OF CLEARANCE SPECIFICATION FWD AND AFT FROM AIRCRAFT TO DOOR FRAME. PERFORMED CABIN DOOR RIGGING IAW CESSNA 680A 52-10-00. DOOR POST RIGGING OPS CHECK GOOD.

Part: BRAKE — FAULTED (LT MLG) · airframe 4,909 hrs · 3,201 cycles

LEFT MLG BRAKE GRABBING & MAKING A GRINDING NOISE AFTER LANDING & TAXI IN. SINGLE POINT JACKED LT MLG TO ROTATE NR 1 WHEEL ASSEMBLY & IT ONLY MADE IT ONE & A HALF ROTATIONS. NR 2 WHEEL ASSY SPUN FREELY. REMOVED NR 1 WHEEL ASSEMBLY & MOVED BRAKE ASSY BY HAND. BRAKE ASSY MOVED BY HAND WITH EXCESSIVE FORCE. REMOVED BRAKE ASSY & INSTALLED AN OVERHAULED BRAKE ASSY, BLED BRAKES & CHECKED HYD RESERVOIR. NO SERVICING OF RESERVOIR NEEDED. DOWN JACKED AIRCRAFT;. NO OTHER DEFECTS NOTED. ALT WORK DONE IAW MM 7-10-10 SINGLE POINT JACKING, 32-40-05: MAIN LANDING GEAR WHEEL ASSEMBLY. REMOVAL/INSTALLATION, 32-45-02: MAIN LANDING GEAR BRAKE ASSEMBLY - REMOVAL/INSTALLATION, AND 32-42-00: BRAKE BLEEDING

Part: SWITCH — DAMAGED (UNKNOWN) · airframe 4,162 hrs · 2,720 cycles

ON TAXI OUT CABIN DOOR OPEN APPEARED. RAN THE QRH AND MESSAGE DID NOT CLEAR. FOUND INNER HANDLE PUSH BUTTON WIRING OPEN TO GROUND. REPAIRED BROKEN WIRE AT SPLICE ACO28. RE-PINNED BROKEN WIRE, IAW WM 52-10-01. OPS CHECK GOOD IAW AMM 52-70-15. INSPECTED WIRE HARNESS FOR ANY OBVIOUS DEFECTS, NONE WERE FOUND CHECKED SWITCHES FOR PROPER ADJUSTMENT, FOUND THE SECURING PAWL DOOR PROX SWITCH TO BE DEFECTIVE, REMOVED AND REPLACED THE PAWL SENSOR, THE PCB AND THE UPPER DOOR HARNESS IAW AMM CH 24-60-25, AND 52-70-25 OP'S CK GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 3,833 hrs · 2,492 cycles

CABIN EMERG LIGHT: NONE OF THE CABIN EMER LIGHTS WILL ILLUMINATE WITH THE EMER LTS SWITCH IN THE ON POSITION. CABIN EMER LIGHTS WILL ILLUMINATE AS EXPECTED WITH EMER LTS SWITCH IN ARM. SEEMS IT HAS BEEN WRITTEN UP IN RECENT PAST. REPLACED #4 EMERGENCY BATTERY FUSE. OPS CHECK GOOD

Part: CHARGER — DEFECTIVE (ZONE 100) · airframe 3,754 hrs · 2,446 cycles

LIGHTS TESTED NORMAL FIRST FLIGHT OF DAY YESTERDAY & TODAY. WHILE IN MDW, ANOTHER LATITUDE CAPTAIN ASKED TO CHECK EMER LIGHTS TO COMPARE BRIGHTNESS, TURNED OUR EMER LIGHTS SWITCH ON AND NOTHING ILLUMINATED. CONTACTED MX AND ASKED TO ATTEMPT W2 POWER DOWN, WHICH I DID, AND AGAIN NO ILLUMINATION OF ANY LIGHTS. REMOVED INOP BATTERY CHARGER AND INSTALLED A NEW BATTERY CHARGER IAW MM 33-50-06. OPS CHECK GOOD NO DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 3,754 hrs · 2,446 cycles

CABIN EMERG LIGHT: TESTED NORMAL FIRST FLIGHT OF DAY YESTERDAY AND TODAY. WHILE IN MDW, ANOTHER LATITUDE CAPTAIN ASKED IF HE COULD CHECK EMER LIGHTS TO COMPARE BRIGHTNESS, WHICH I COMPLIED WITH. HE TURNED OUR EMER LIGHTS SWITCH ON AND NOTHING ILLUMINATED. I TRIED IT MYSELF AND SAME EFFECT. I CONTACTED MX AND HE ASKED ME TO ATTEMPT W2 POWER DOWN, WHICH I DID, AND AGAIN NO ILLUMINATION OF ANY LIGHTS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 3,696 hrs · 2,410 cycles

CO-PILOT SIDE, RIGHT WINDSCREEN IS CRACKED. PICTURES ATTACHED.

Part: BATTERY — INOPERATIVE · airframe 3,500 hrs · 2,271 cycles

EMERGENCY LIGHTS BATTERY: EMERGENCY BATTERY PACK TWO ASSOCIATED LIGHTS ARE NOT ILLUMINATING DURING PREFLIGHT CHECK///SIGN OFF/// REMOVED #2 EMERGENCY BATT PACK, BATTERY CHARGER SYSTEM P/N CBS28-1 S/N 005313 DUE TO INTERNAL FAILURE. INSTALLED REPAIRED BATTERY CHARGER SYSTEM P/N CBS28-1 S/N 008094 AS REQUIRED. PERFORMED AND FOUND OPERATIONAL TEST SATISFACTORY. CLOSED ACCESS. WORK DONE IRW CE-680A AMM 33-50-0

Part: MODULE — DEFECTIVE (MLG HANDLE) · airframe 3,327 hrs · 2,167 cycles

LANDING GEAR BLOWDOWN BOTTLE SERVICE: UPON LANDING, GEAR WOULD NOT EXTEND. YELLOW DN WAS DISPLAYED ON GEAR ICAS ALONG WITH GEAR DISAGREE CAS MESSAGE. RAN QRH, BLEW DOWN HANDLE WAS USED TO LOWER NOSE GEAR. MAIN GEAR UPLOCK HANDLE USE TO LOWER MAIN GEAR. LANDED WITH THREE GREEN DISPLAYED. REMOVED INOP LANDING GEAR HANDLE MODUEL AND INSTALLED OVERHAULED LANDING GEAR HANDLE UNIT IAW 32-30-30. PERFORMED OPS CHECK, OPS CHECK GOOD. SERVICED HYDRAULIC RESERVOR !AW 12-10-30. NO DEFECTS NOTED. ORIG SUBMISSION DATE: 12/30/2022

Part: UPLOCK SWITCH — DAMAGED (NLG) · airframe 3,200 hrs · 2,099 cycles

25 MINUTES INTO FLIGHT LEVELING OFF AT 39000, HEARD & FELT A BUMP IN NOSE GEAR. FOLLOWED IMMEDIATELY BY NOSE GEAR INDICATOR GOING TO YELLOW CROSSHATCHINGS. FOLLOWED IMMEDIATELY BY A AMBER GEAR DISAGREE N EICAS INDICATION. COMPLIED WITH QRH & CONTINUED TO DESTINATION. DECENDING THROUGH 3000 FEET, INDICATION EXTINGUISHED. EXTENDED GEAR ON SCHEDULE WITH NO PROBLEMS & LANDED NORMALLY. FOUND NO DEFECTS, CW GEAR BUMP TROUBLESHOOTING IAW MM 32-00-00 & FOUND THE UP-LOCK SWITCH WAS OUT OF ADJUSTMENT. MEASUREMENT ON SWITCH PLUNGER SHOULD HAVE BEEN 0.15 INCH +/- 0.03 INCH & ACTUALLY MEASURED .07 INCH, R & R THE SWITCH IAW MM 32-32-10 OPS CHECKED GOOD.

Part: MODULE — DEFECTIVE (ZONE 100) · airframe 3,032 hrs · 1,992 cycles

FLAPS FAIL AMBER CAS: WHEN FLAP RETRACTION WAS ATTEMPTED AFTER TAKEOFF, AMBER FLAPS FAIL CAS MESSAGE ILLUMINATED. FLAP HANDLE WAS AT UP AND FLAPS WERE INDICATING AT 1. FLAPS ARE IN THE FLAPS 1 POSITION. QRH PROCEDURE WAS ACCOMPLISHED BUT, DID NOT CLEAR THE ALFUNCTION. PERFORMED ARES DOWNLOAD AND SENT DATA TO TEXTRON, CHECKED CMC FOR FAULT, NO FAULTS LOGGED IN HISTORY, CHECKED CAS HISTORY SCREEN AND FOUND TWO FLAP FAIL MESSAGES POSTED ON 9/25/22 BOTH INDICATE ALERT ID2787, CHECKED M/M FOR FAULT ISOLATION AND FOUND NO GUIDANCE, CHECKED FCU AN SCREEN AND FOUND BIT 2 AND 6 LOGGED NOT CONFIDENT THESE FAULTS ARE ACTIVE BECOUSE THEY HAVE BEEN LOGGED FOR A LONG TIME ACCORDING TO ARES DATA, RESETT BIT CODES AND RAN FLAPS THRU TWO FULL CYCLES WITH NO FAILURES, NO BIT CODES RETURNED, RECEIVED HISTORY FROM NJA AMCC SHOWING 6 PREVIOUS FLAP FAILS DATING BACK TO 7/22/22, DOWNLOADED ARES FILES FOR CURRENT AND PREVIOUS FAILURES, REVIEWED ARES ON PC, DATA SHOWED ALL PREVIOUS AND CURRENT FLAP FAILS HAPPENED IN THE AIR WHEN FLAPS WERE SELECTED FROM 1 TO 0, ALL OCURANCES SHOWED FLAPS WERE COMMANDED TO MOVE FROM 1 TO 0 WITH HIGH AMP SPIKE ON LEFT GEN WITH NO FLAP MOVEMENT, CONTACTED TEAM 680 SUPPORT LINE AND TALKED TO BRYAN AFTER HE REVIEWED ARES DATA, HIS RECOMENDATION WAS TO VERIFY PROPER FLAP OPERATION AND CHECK FOR ANY SIGNS OF FLAP MECHANICAL ISSUES, RAN FLAPS THRU 25 CYCLES CONTINUOSLY WITH NO FAILURES AND IMMEDIATLY CHECKED TEMP OF ALL 12 ACTUATORS AND ALL FLEX DRIVE CABLES USING LASER THERMOMETER, ALL TEMPS WERE UNIFORM RANGING FROM 87-92 DEG F, NO SIGNS OF BINDING OR OBSTRUCTION, PERFORMED GENERAL VISUAL INSPECTION OF ALL FLAP TRACKS AND ROLLERS, NO DEFECTS NOTED. CHECKED BIT CODES AGAIN AND NO CODES FLAGGED. 9/26/22 D.P PERFORMED 10 MORE FULL FLAP CYCLES WITH NO FAILURES, CONTACTED NJA AMCC AND ASKED IF THEIR REP WOULD REVIEW ARES DATA FOR ANY FURTHER GUIDANCE, WAS ADVISED THAT THEIR REP OBSERVED FLAP POWER RELAY WAS INTERMITTENTLY SHOWING OPEN AND CLOSED AT TIMES

Part: BATTERY — DEFECTIVE (ZONE 100) · airframe 2,447 hrs · 1,553 cycles

EMERG EXIT SIGN/LIGHT: MAIN ENTRY DOOR EXIT SIDE WILL NOT EXTINGUISH. SEAT 10 EMER LIGHT IS ALSO ON. // SIGNOFF// REMOVED FAULTY #1 EMERGENCY BATTERY AND REPLACED WITH REPAIRD EMERGANCY BATTERY REF CESSNA 680A AMM 33-50-06 AND RESET INTERIA SWITCH ON #1 BATTERY REF CESSNA 680A AMM 33-50-11 PREFORMED OPS CHECK REF CESSNA 680A AMM 33-50-00 OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME

Part: NONE — CHIPPED (ZONE 700) · airframe 2,063 hrs · 1,333 cycles

CHIPPED PLATING ON RIGHT MAIN LANDING GEAR AXLE P/N 6741032-5. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ32727M1 REV. B DATED DECEMBER 6, 2021; 680A-0227 (N696QS) RIGHT MAIN LANDING GEAR AXLE PLATING DAMAGE (CHIPPED).

Part: BYPASS SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 302 hrs · 187 cycles

FUEL FLTR BYPASS L AMBER CAS ILLUMINATED - IN CRUISE FLIGHT DURING LEFT TANK TO RIGHT ENGINE CROSSFEED: "FUEL FILTER BYPASS L" AMBER CAS MESSAGE ILLUMINATED. CROSSFEED WAS DISCONTINUED AND LANDED AS SOON AS POSSIBLE PER QRH. MESSAGE REMAINED ON UNTIL SHUTDOWN AND NO ENGINE ANOMALIES WERE NOTED. //TECS PERFORMED ENG RUNS ON THE AIRCRAFT AND FOUND A 2ND HARD FALL. CAS MESSAGE RAN ENGINE T0 DUPLICATE THE ORGINAL. DISCREPANCY. TECS PERFORMED AN ARES DOWNLOAD AND SENT INFORMATION OFF T0 CESSNA TEAM 680 FOR REVIEW. CESSNA DETERMINED THAT BOTH FUEL. FILTERS AND FUEL BY PASS SWITCES WOULD REQUIRE REPIACEMENT. REMOVED AND REPLACED #1 AND #2 FUEL FILTERS IN REF TO PW306D/PW306D1 MM73-10-03 TECHS POWERED UP AIRCRAFT. NO CAS MESSAGES PRESENT. RAN ENGS AND ALLOWED THEM TO STABILIZE . NO CAS MESSAGES PRESENT.TAXIED AIRCRAFT TO AN APPROVED RUN UP LOCATION . SET AIRCRAFT UP IN THE CONFIGURATION THAT THE CREW HAD WHEN THE FAULT OCCURED ( CROSSFEED SET COMMENTS: TO LH TANK TO RH ENG). THE ONLY DIFFERENCE BEING WEIGHT ON WHEELS INSTEAD OF FLYING . WHILE PERFOMMING RUNS TECHS TECHS RECEIVED A "FUEL CROSSFEED" AMBER CAS MESSAGE . MESSAGE WOULD DISAPPEAR WHEN TURNED TO NORMAL POSITION AND WOULD TUM WHITE WHEN IN THE RH TANK TO LH ENG. TAXIED AIRCRAFT BACK TO RAMP AND SHUT DOWN . POWERED THE AIRCRAFT BACK UP AND PERFORMED A ARES DOWNLOAD. SENT THE DOWNLOADS TO TEAM 680 FOR REVIEW. THE CONCLUSION WAS MADE TO REPLACE BOTH BY PASS SWITCHES AND BOTH FUEL FILTERS .BYPASS SWITCHES DUE IN AT 1300. AND FUEL FILTLERS REMOVED AND REPLACED#I AND #2 ENGINE FUEL FILTER IMPENDING BYPASS SWITCHES IN REF TO PWC 306D/306DL MM 73~ I 0-03 REMOVED AND REPLACED# I AND #2 FUEL FILTERS IN REF TO PW306D/PW306DI MM7~J0-03 TECHS PERFORMED ENGINE RUN FOR LEAK CHECK, NO LEAKS FOUND. TECHS CLOSED UP# I AND #2 ENGINE COWLING AND CLOSED AIRCRAFT.

Part: ENGINE — POWER LOSS (LEFT) · airframe 12,270 hrs · 9,761 cycles

WITH EEC IN MANUAL, TAKEOFF POWER OBTAINED. DURING CLIMB, NOTICED LARGE THROTTLE SPLIT AND NOTICED THAT THE LEFT ENGINE NOT DEVELOPING TAKEOFF THRUST. CONTINUED CHECKING THROUGH CLIMB ONLY GOT 85% N1 101% N2 WITH THROTTLE TO FORWARD STOP.

Part: CABLE — FRAYED · airframe 11,659 hrs

THIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO BE UNSERVICEABLE PER AMM CHAPTER 20-10-04. NEW CABLE ASSEMBLY INSTALLED.

Part: CABLE — BROKEN · airframe 11,659 hrs

THIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO BE UNSERVICEABLE PER AMM CHAPTER 20-10-04. NEW CABLE ASSEMBLY INSTALLED

Part: HOSE — BLOWN (MLG) · airframe 11,659 hrs

DURING A SCHEDULED MAINTENANCE GEAR SWING THE RT GEAR UP-LOCK HOOK EXTEND HOSE ASSY, BLEW A HOLE IN IT ABOUT .5 INCH FROM THE SWEDGED FITTING HOSE END. THIS IS THE HOSE END THAT ATTACHES TO THE UP-LOCK ACTUATOR FITTING. NO MAINTENANCE PERSONNEL WERE HURT OR DAMAGE TO AIRCRAFT, BUT THE MAIN WHEEL ASSY WAS REPLACED DUE TO SKYDROL CONTAMINATION. NEW HOSE ASSY INSTALLED.

Part: COALESCER BAG — ODOR · airframe 10,761 hrs · 8,561 cycles

MILDEW SMELL AT FLIGHT LEVEL 410. R & R WATER SEPARATOR CONDENSER SOCK IAW AMM 21-51-00. OPS & LEAK CHECKED GOOD.

Part: BRAKE SYS — CONTAMINATED (MLG) · airframe 9,600 hrs · 7,624 cycles

UPON LANDING BRAKES WERE EVENLY APPLIED BUT ASYMMETRICAL BRAKING WAS EXPERIENCED, ACFT PULLED TO THE LT, BRAKES WERE RELEASED & ACFT DIRECTION OF TRAVEL WAS CORRECTED & BRAKES WERE EVENLY APPLIED AGAIN & AGAIN THE ACFT PULLED TO THE LT, WE WERE ABLE TO CLEAR THE RUNWAY & BRAKES WERE EVENLY APPLIED AT TAXI SPEED WITH NO ASYMMETRY, WE WERE ABLE TO TAXI TO THE RAMP WITH NO FURTHER ISSUES. BLED BRAKE SYS IAW MM CH 32-42-00. RAN ACFT & TAXIED. OPERATIONS & LEAK CHECKED SATISFACTORY.

Part: SKIN — CORRODED (WINGS) · airframe 9,334 hrs · 7,419 cycles

CORROSION DAMAGE WAS FOUND AT MULTIPLE LOCATIONS BETWEEN WS 117.9 AND 184.9 ON THE LT AND RT UPPER OTBD WING SKINS AND THE LT AND RT T/E SKINS. AFTER BLENDING TO REMOVE ALL CORROSION, THE MINIMUM REMAINING THICKNESSES OF THE AFFECTED SKINS WERE RECORDED FOR EACH DAMAGE LOCATION.

Part: BLADES — DAMAGED (ENGINE) · airframe 8,984 hrs · 7,113 cycles

ACCOMPLISH BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. ACCOMPLISHED PREINDUCTION GROUND PERFORMANCE RUN AND TRANSIENT VIBRATION SURVEY. ACCOMPLISHED A BORESCOPE INSPECTION OF THE COMBUSTION LINER NUTS. ACCOMPLISHED SI 35-2013 INSPECTION SB 30419 LINER. DISCOVERED TWO NUTS MISSING. DISCOVERED IMPART DAMAGE TO THE HPT AND LPT BLADES. ACCOMPLISHED REPAIRS. HPT DISK ASSY 30J3202-01 SN A002XADS: DISASSEMBLED AND VISUALLY INSPECTED. DISCOVERED 25 UNSERVICEABLE BLADES ( IMPACT DAMAGE) ASSEMBLED 45 ORIGINAL BLADES AND 25 NEW BLADES TO THE ORIGINAL SERVICEABLE HPT DISK WITH NEW SEALS.

Part: BRACKET — CRACKED (ZONE 100) · airframe 8,149 hrs · 6,436 cycles

RUDDER AUTOPILOT CABLE BRACKET AT AFT CANTED BULKHEAD IS CRACKED ON INBD RIVET LINE. R & R RUDDER AUTOPILOT CABLE BRACKET IAW SRM 51-40-03 AND MM 22-11-01.

Part: LINE — CHAFED (LT BRAKE) · airframe 8,149 hrs · 6,436 cycles

LEFT BRAKE LINE FWD OF COPILOTS RT RUDDER PEDAL IS CHAFED DUE TO RUDDER PEDAL CONTACT. R & R LT BRAKE LINE ASSY FWD OF COPILOTS RT RUDDER PEDAL IAW MM 20-10-06.

Part: PITOT TUBE — OBSTRUCTED (PILOTS) · airframe 7,215 hrs · 5,688 cycles

BOTH PILOTS PFD'S DISPLAYED AN AMBER IAS MESSAGE AFTER PASSING THROUGH 160 KTS. AT MINIMUM LT PILOTS IAS INDICATING 160, RT PILOTS INDICATING 166 & STANDBY INDICATING 167. ACCELERATED TO 200 KTS, SPLIT INCREASED TO ABOUT 9 KTS BETWEEN PRIMARY IAS INDICATORS WITH RT SIDE SHOWING FASTER THAN LT. DECELERATED THROUGH 160 KTS FOR LANDING, SPLIT WENT BACK DOWN TO ABOUT 5 KTS. INSPECTED PITOT TUBES AND FOUND A SMALL ROCK IN PILOTS PITOT. PURGED PITOT SYS AND REMOVED DEBRIS. WHILE PERFORMING LEAK CHECK FOUND PILOTS STATIC SYS LEAK AT DRAIN. R & R O-RING IAW THE MM 34-11-08. LEAK CHECK WAS COMPLIED WITH IAW MM 34-11-08. PITOT STATIC SYS LEAK CHECK WAS PERFORMED IAW THE FAR 91-411.

Part: UNKNOWN — SMOKE · airframe 5,836 hrs · 4,559 cycles

SMOKE IN THE COCKPIT CAME THROUGH THE GASPER FANS WITH THE APU RUNNING ON THE GROUND.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 5,836 hrs · 4,559 cycles

SMOKE IN THE COCKPIT CAME THROUGH THE GASPER FANS WITH THE APU RUNNING ON THE GROUND.

Part: WATER SEPARATOR — DIRTY (APU) · airframe 5,836 hrs · 4,559 cycles

BOROSCOPE COMBUSTION SECTION FOUND IT TO BE GOOD. INSPECTED INTAKE COLD EXHAUST ALSO FOUND THEM TO BE GOOD. REMOVED OLD WATER SEPARATOR. INSTALLED NEW WATER SEPARATOR. IAW MM CH 21-51-00. RAN APEX ELS SYS IAW MM CH 21-11-00 WITH NO DEFECTS NOTED.

Part: ACTUATOR — DEFECTIVE (LT MLG) · airframe 4,299 hrs · 3,356 cycles

ON DEPARTURE AFTER RAISING THE GEAR, THE GEAR UNLOCK LIGHT ON AND THE GREEN NOSE GEAR LIGHT ILLUMINATED. RECYCLED THE GEAR AND HAD THE SAME INDICATION. EXTENDED GEAR AND GOT THREE GREEN. LT GEAR DOWN AND LANDED. REMOVED DEFECTIVE NOSE GEAR ACTUATOR AND INSTALLED INSPECTED CUSTOMER SUPPLIED NLG ACTUATOR. OPS CHECK AND LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. WORK DONE IAW CE-560XL AMM CHAPTER 32-30-03.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 4,201 hrs · 3,272 cycles

LT WINDSHIELD SHATTERED. RECEIVED LT FAULT, SELECTED OFF, LT O'HEAT WINDSHIELD, ARCED AND SHATTERED, DIVERTED. [SUP 4-19-07] REPLACED WINDOW IAW MM 56-11-00

Part: TRANSMITTER — MALFUNCTIONED (LT ENG OIL PRESS) · airframe 4,107 hrs · 3,215 cycles

DURING POWER REDUCTION TO IDLE AT 10.000 FT, LT ENGINE OIL PRESSURE DROPPED TO BELOW 20 PSI AND JUMPED BACK AND FORTH TO 40 PSI. ON POWER INCREASE, PRESSURE STAYED AROUND 30 PSI. ENGINE WAS LEFT AT IDLE UNTIL COMPLETION OF FLIGHT. LOWERED NR 1 ENGINE COWLING. INPSECTED FOR OIL LEAKS. NO LEAKS NOTED. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER. ADDED .5 QTS OF OIL (2380) RAN NR 1 AND 2 ENGINES. OPS CHECK GOOD IAW CE560XL M/M 79-30-00, AND MM 05-10-00. LEAK CHECK GOOD. CLOSED COWLING.

Part: TRANSDUCER — INOPERATIVE (RT MLG) · airframe 2,475 hrs · 1,915 cycles

ON TAKEOFF ROLL, APPROACHING 60K MASTER CAUTION LIGHT ILLUMINATED WITH ANTI-SKID ANNUNCIATOR LIGHT SWITCHES PROPER POSITION, TAKEOFF ABORTED. T/S TO BAD RT WHEEL TRANSDUCER. INSTALLED NEW TRANSDUCER OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE 560 XL M/M 32-40-00.