FLEXJET, LLC

Operated by FLEXJET LLC (per NTSB report)

Operated by FLEXJET LLC (per NTSB report)

CREW RECEIVED SPOILER FAIL CAS ON LANDING. REPLACED FCE #2. RIGGED FCE #2 AND PERFORMED OPERATIONAL CHECKS. NO FAULTS FOUND. WORK PERFORMED IAW EMB-505 AMM 27-03-01.

CREW RECEIVED GND SPLR FAIL AND SPOILER FAIL CAS MESSAGES ON LANDING WHILE BRAKING. REPLACED #2 FCE IAW EMB-505 AMM 27-03-01. RIGGING AND OPS CHECKS GOOD.

CREW REPORTS LOUD CABIN SQUEALING NOISE DURING CLIMB BETWEEN 6000 FT AND 7000 FT DURING ENGINE AND WING ANTI ICE SELF-TEST. THE NOISE LASTED 5-10 SECONDS AND DISSIPATED ENTIRELY AFTER SELF-TEST CONCLUSION. DURING DESCENT, CREW TESTED ANTI-ICE AT DIFFERENT ALTITUDES AND CONFIGURATIONS AND CONCLUDED THAT NOISE WOULD ONLY PRESENT ITSELF WHEN ANTI-ICE ALL WAS ACTIVE BELOW 12,000 FT. NOISE BECAME MORE PROMINENT AT LOWER ALTITUDES AND WAS HEARD ONLY ON THE LEFT SIDE OF THE AIRCRAFT. REPLACED LH WING CENTER LEADING-EDGE PICCOLO TUBE. REPLACED LT WING INBOARD LEADING-EDGE ASSEMBLY. NO DEFECTS NOTED DURING AND LEAK CHECKS OF WING ANTI-ICE SYSTEM. WORK COMPLETED IAW 57-40-00 + 30-12-00.

PRIOR TO THE DEPARTURE, CREW RECEIVED SWPS FAULT, PTRIM NML FAIL, GND SPLR FAIL CAS MESSAGES. YELLOW X APPEARED OVER SPOILER AND PITCH TRIM ON MFD. REPLACED FCE #2 IAW EMB-505 AMM 27-60-00. RIGGING AND OPS CHECKS GOOD.

DURING CRUISE, CREW RECEIVED GND SPLR FAIL CAS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED AND RIGGED FCE2. OPS CHECK GOOD. WORK PERFORMED IAW AMM 27-03-01.

AIR TURN BACK DUE TO PITCH TRIM ACTUATION ON PILOT SIDE WORKED UNTIL REACHING 3.0 TRIM SETTING THEN STOPPED FUNCTIONING DURING TAKEOFF. PITCH TRIM WAS SET TO 5.3. CREW TRIED TO MOVE TWO TIMES WITH THE PILOT’S CONTROL TO NO AVAIL, THEN ACTIVATED CO-PILOT CONTROL AND MOVED THE TRIM SETTING TO UNDER 3.0. UNDER 3.0, THE PILOT TRIM WORKED NORMAL IN BOTH UP AND DOWN MOVEMENT. AIRCRAFT LANDED WITHOUT INCIDENT AT KTEB. FOUND RELAY MOUNT BRACKET NOT PROPERLY GROUNDED TO AIRCRAFT STRUCTURE. RE-BONDED TO AIRCRAFT STRUCTURE AND REPLACED RELAY K211. RE-RACKED JB3 AND VERIFIED PIN CONDITION AND RETENTION. WORK PERFORMED IAW WM 27-12-07 AND AMM 24-63-09. OPS CHECK GOOD AT THIS TIME.

DIVERTED TO KMRY DUE TO AN ELECTRICAL BURNING SMELL IN THE CABIN. DURING CRUISE, THE PIC NOTED A RED X APPEAR OVER COM2 WHICH THEN EXTINGUISHED AND REAPPEARED MULTIPLE TIMES SHORTLY THEREAFTER. THE CREW OBSERVED SMOKE EMANATING FROM THE GLARESHIELD PROMPTING THEM TO DON THEIR OXYGEN MASKS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED GIA 2 IAW EMB 505 AMM 31-41-05. ALL FOLLOW-ON CHECKS PASSED.

COFFEE POT OVER HEATED CAUSING STRONG BURNING SMELL IN FLIGHT. CREW PULLED AND COLLARED HOT JUG 1 AND 2 CIRCUIT BREAKERS. COFFEE POT WAS THEN SECURED IN AFT BAGGAGE AREA. REPLACED COFFEE POT IAW EMB-505 AMM 25-31-02. HOT JUG 1 AND 2 CIRCUIT BREAKERS RESET AIRCRAFT RETURNED TO NORMAL CONFIGURATION.

REJECTED TAKEOFF DUE TO PACK TEMP HIGH CAS, PACK FAIL CAS, AND VISIBLE SMOKE IN CABIN. CREW TAXIED BACK TO THE FBO WITHOUT INCIDENT. FOUND BROKEN BLADE ON ACM. REPLACED ACM AND PRECOOLER. PERFORMED OPS AND BLEED CHECKS. ALL CHECKS SATISFACTORY AT THIS TIME. WORK COMPLETED IAW CL 300 AMM 21-51-15, 21-52-13, 21-52-00.

DURING CLIMB A SMALL AMOUNT OF SMOKE BEGAN EMANATING FROM THE LOWER LEFT CORNER OF THE CAPTAIN-SIDE WINDSHIELD NEAR THE CONTROL PANEL AREA. THE CREW OBSERVED THAT THE ODOR WAS METALLIC AND CONSISTENT WITH AN ELECTRICAL OR HEATING SOURCE AND IMMEDIATELY CEASED AFTER THE WINDSHIELD HEAT SYSTEM WAS DEACTIVATED. AIRCRAFT LANDED AT KMDW WITHOUT INCIDENT. REPLACED LEFT WINDSHIELD ASSEMBLY. PERFORMED SATISFACTORY WINDSHIELD ANTI-ICE CHECKS AND PRESSURIZATION LEAK CHECKS WITH NO FURTHER DEFECTS NOTED IAW BD-100 AMM 56-11-01.

AIR TURN BACK DUE TO SMOKE IN CABIN DURING CLIMB BETWEEN 12000 AND 15000 FT. CREW NOTED THAT THE ODOR SEEMED TO BE COMING FROM BEHIND THE LT CIRCUIT BREAKER PANEL. AIRCRAFT LANDED WITHOUT INCIDENT AT KSFB. REPLACED THE NR 1 VHF 4000 IAW AMM 23-11-01. PERFORMED SATISFACTORY ELECTRICAL BONDING TEST IAW SPM 51-80-00. PERFORMED SATISFACTORY OPSL TEST OF THE NR 1 VHF IAW BD-100 23-11-00.

P TRIM NML FAIL CAS DISPLAYED. REPLACED FCE NR 2 IAW AMM 27-03-01. OPS CHECKS GOOD. NO FAULTS NOTED AT THIS TIME.

ON DECENT CREW RECEIVED GND SPLR FAIL AND PTRIM NML FAIL CAS MESSAGES. EXECUTED QRH, NO RESET POSSIBLE, LANDED ON BACK-UP TRIM. REPLACED #2 FCE IAW EMB 505 AMM 27-03-01. RIG AND OPERATIONAL CHECKS GOOD.

DURING CRUISE, CREW LOST TWO SMART PROBES. AN EMERGENCY WAS DECLARED & DECISION MADE TO CONTINUE TO THEIR DESTINATION: KDAL. ON APPROACH, TOWER NOTIFIED CREW THAT IT APPEARED THAT A PANEL WAS MISSING FROM THE NOSE SECTIONT. ACFT LANDED WITHOUT INCIDENT AT KDAL. FOUND THE RAT ATTEMPTED & FAILED TO DEPLOY. STOWAGE DOOR WAS FULLY OPEN, BUT RAT EGRESS BLOCKED WHEN A FAN BLADE CONTACTED THE EDGE OF THE DOOR OPENING. PERFORMED HIDDEN DAMAGE INSPECTION OF THE RAT BAY IAW AMM 05-41-00. FOUND DENT ON THE RAT DOOR LANDING SKIN NEAR DOOR SEAL FWD LOWER AREA. PERFORMED A PERMANENT REPAIR OF THE RAT DOOR LANDING SKIN NEAR DOOR SEAL FWD LOWER AREA IAW SRM 51-10-05, 51-10-03, 51-22-013, 51-22-04, & 51-22-05. PERFORMED RAT DOOR OPEN & CLOSING CHKS IAW AMM 24-23-00. NO DEFECTS NOTED. FOUND NICKS ON 1 RAT BLADE. REPLACED THE RAT WITH A REPAIRED UNIT IAW AMM 24-23-01. REPLACED RAT UPLOCK ASSLY IAW AMM 24-23-05. RIGGING, OPS TEST, FUNCTIONAL TEST ALL CHKD GOOD. PERFORMED RAT MANUAL-RELEASE HANDLE & CABLE ASSY ADJUST IAW AMM 24-23-07. PERFORMED RAT DEPLOYMENT ACTUATOR ADJUST IAW AMM 24-23-03. PERFORMED MULTIPLE RETRACTIONS & DEPLOYMENTS WITH NO DEFECTS.

YELLOW X NOTED DURING PITCH TRIM MOVEMENT IN PRIMARY. REPLACED NR 2 FCE IAW AMM 27-03-01.

SWPS FAULT, GNS SPLR FAIL, PTRIM NML FAIL, SPOILER FAULT CAS ILLUMINATED IN FLIGHT. REPLACED FCE # 2 IAW EMB 505 AMM 27-60-00. ALL OPS AND RIGGING PROCEDURES SATISFACTORY. NO DEFECTS NOTED AT THIS TIME.

ON START UP, FLAP FAIL CAS ILLUMINATED AND FLAP INDICATOR ON MFD SHOWED YELLOW. CYCLED FLAPS AND MESSAGE REMAINED. REPLACED FCE 1 IAW EMB 505 AMM 27-03-01. RIGGING/OPS CHECK GOOD.

FCE 2 CB POPPED WITH RELATED CAS MESSAGES. ATTEMPTED RESET WAS NOT SUCCESSFUL. REPLACED FLIGHT CONTROL ELECTRONIC (FCE) 2 IAW P300 AMM 27-3-01. OPS CHECK GOOD.

DURING CRUISE, CREW RECEIVED SWPS FAULT, FLAPS FAIL, PTRIM BKP FAIL AND SPOILER FAULT. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FCE 1 IAW EMB 505 AMM 27-03-01. FCE 1 RIGGING / OPS CHECK GOOD AND NO CAS MESSAGE ILLUMINATED.

DURING CRUISE, CREW RECEIVED SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL AND SPOILER FAULT. THE FLAPS WERE RETRACTED AT THE 0 POSITION. CAS MESSAGES REMAINED ON FROM CRUISE, LANDING AND SHUTDOWN. REPLACED FCE #1 AND OPS/RIGGED TESTED WITH NO FURTHER DEFECTS IAW PHENOM 300 AMM 27-03-01.

WHILE DOING THE FLIGHT CONTROL CHECK AFTER STARTUP, GND SPOILER FAIL CAS. REPLACED FCE #2 IAW EMB 505 AMM TASK 27-03-01-400-801. RIGGING AND OPS CHECK SATISFACTORY AT THIS TIME.

BINDING NOTED ON TWO SEPARATE FULL RIGHT RUDDER FULL RIGHT BRAKE APPLICATIONS. ACCOMPLISHED A GIV OF THE CONTROL PEDALS IAW AMM 27-01-02 AND THE RUDDER FORWARD TORQUE TUBE IAW AMM 27-21-06. FOUND THE TOP BRACKET HOLDING THE CENTER RUDDER FORWARD TORQUE TUBE FLEXING / MOVING WHEN THE RUDDER IS MOVED FULL RIGHT AND FULL LEFT. REPLACED THE MOUNTING HARDWARE TO THE AIRFRAME FROM THE CENTER RUDDER FORWARD TORQUE TUBE TOP BRACKET AND APPLIED TORQUE TO 42 IN-LBS IAW AMM 27-21-05. NO FURTHER DEFECTS NOTED.

GENERATOR 1 FAILED AT FL430 AFTER LANDING AT KPRB. ENGINE 1 LOST ALL OIL. REPLACED FAILED LH GENERATOR. REPLACED DAMAGED LTD. WORK COMPLETED IAW EMB PRAETOR AMM 24-31-01. INSTALLED REPLACEMENT BEARINGS ONTO #1 ENGINE GENERATOR AGB GEAR SHAFT IAW HONEYWELL AS907-3-1E LMM 72-61-01. REPLACED #1 ENGINE AGB GENERATOR CARBON SEAL IAW AS907-3-1-E LMM 12-61-01. OPS AND LEAK CHECKS GOOD. PERFORMED ENGINE POWER RUNS. ALL OPS AND LEAK CHECKS ARE SATISFACTORY AT THIS TIME. INSPECTED AGB DEBRIS MONITORS POST ENGINE RUNS AND NOTED NO DEFECTS.

CREW RECEIVED SPOILER FAULT ON GEAR RETRACTION. AIRCRAFT LANDED WITHOUT INCIDENT AT PLANNED DESTINATION. REPLACED #2 FCE IAW AMM 27-03-01. RIG AND OPERATIONAL CHECKS GOOD.

MICROWAVE SMOKED WHILE HEATING WET TOWEL. REPLACED THE MICROWAVE IAW G450 AMM 25-37-02. OPS CHECK GOOD.

BURNING SMELL ON DESCENT ACCOMPANIED BY VERY WARM AIR. AIRCRAFT LANDED WITHOUT INCIDENT AT KSSI. AFTER LANDING, CREW RECEIVED AMBER PACK TEMP HIGH CAS ON SYNOPTIC. REPLACED AIR CYCLE MACHINE. PERFORMED SUCCESSFUL OPS CHECK AND LEAK CHECK IAW CH 300 AMM 21-52-13.

PTRIM BKP FAIL CAUTION CAS ILLUMINATED ON ROTATION; REMAINED ON AFTER POWER CYCLE AT DESTINATION. REPLACED FCE IAW AMM 27-03-01. PERFORMED FLAP SYSTEM ELECTRONIC RIGGING. OPERATIONAL TESTS SATISFACTORY.

ON TAKEOFF ROLL, THE LEAD PASSENGERS SEAT BROKE CAUSING PASSENGER TO FALL BACKWARD. SHORTLY AFTER THE CREW WAS NOTIFIED THAT THE FORWARD-FACING MIDDLE SEAT WOULD NOT REMAIN UPRIGHT. THE SEAT DID NOT RESTRICT ANY EMERGENCY EXIT, EGRESS ROUTE, OR MAIN AISLE. AIRCRAFT LANDED SAFELY AT KSNA WITHOUT INCIDENT. REPLACED L/H FWD MIDDLE FACING SEAT RECLINE ACTUATOR IAW GOODRICH CMM 25-25-68. SEAT RECLINE OPS CHECK GOOD AND SEAT RESTORED TO NORMAL CONFIGURATION.

DURING SCHEDULED MAINTENANCE WHILE RE-TENSIONING AILERON CABLE, DISCOVERED LH WING CABLE SAWING THROUGH PULLEY BRACKET. REPLACED LH AILERON WING PULLEY BRACKET IAW CL300 SRM 51-40-08 AND 51-42-36. LH WING AILERON CABLE REPLACED AND TENSIONED IAW AMM 27-11-35-000/400-801.

DURING CRUISE, JUST PRIOR TO DESCENT, CREW RECEIVED GND SPLR FAIL, PTRIM NORMAL FAIL, AND SPOILER FAULT CAS. AN AMBER ‘X’ ILLUMINATED ON THE PTRIM INDICATOR AND SPOILER INDICATOR. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FCE NR 2. COMPLETED ELECTRONIC RIGGING OF SPOILERS. OPS CHECKED OF FCE NR 2 SYSTEMS. ALL CHECKED GOOD. WORK COMPLETED IAW AMM 27-03-01.

DIVERTED DUE TO PTRIM NML FAIL CAS ON CLIMBOUT. CREW FOLLOWED THE QRH, DISENGAGED THE AUTOPILOT, AND USED BACKUP PITCH TRIM BEFORE LANDING WITHOUT INCIDENT. NO FAULTS NOTED DURING INITIAL OPS CHECKS. SWAPPED FCE 1 AND FCE 2. FLAP FAIL CAS MESSAGE POSTED AFTER FCE SWAP AND WOULD NOT CLEAR. REPLACED FCE 1. RIG AND OPS CHECK GOOD. FLAP FAIL CAS CLEARED. WORK COMPLETED IAW EMB505 AMM 27-03-01, 27-50-00 AND 27-40-00.

AP FAIL CAS FOLLOWED BY SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL, AND SPOILER FAULT CAS ILLUMINATED WHILE CRUISING AT FL450. CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. DURING DESCENT, THE SPEED TAPE DISPLAYED A CONTINUOUS MAX SPEED CAUTION UNTIL 3000 FT DESPITE LOWER SPEEDS, AND THE FLAPS AND PITCH INDICATOR SHOWED YELLOW X’S. REPLACED FCE 1 IAW PHENOM 300 AMM 27-03-01. RIGGED UNIT AND OPS CHECKS OF FLAPS, PITCH TRIM, AND PRESSURIZATION SYSTEMS SATISFACTORY WITH NO DEFECTS FOUND.

PTRIM BACKUP FAIL CAS ILLUMINATED IN FLIGHT. REPLACED FCE #1 IAW PHENOM 300 AMM 27-03-01.

GND SPLR FAIL CAS ILLUMINATED ON TOUCHDOWN. REPLACED FCE 2. RIGGING AND OPS CHECK GOOD. ALL WORK COMPLETED IAW EMBRAER PHENOM 300 AMM 27-03-01.

FCE 1 REPLACED DUE TO MULTIPLE INCIDENTS OF SPURIOUS FLIGHT CONTROL CAS MESSAGES. WORK COMPLETED IAW EMB-505 AMM 27-03-01. COMPLETED RIGGING PROCEDURE OF THE FLAP SYSTEM. ALL OPS CHECKS GOOD.

PITCH TRIM BACKUP FAIL CAS DURING TRIM CHECK WHEN SELECTING NOSE DOWN. REPLACED #1 FCE IAW EMB 505 AMM 27-03-01. OPS CHECK GOOD WITH NO DEFECTS FOUND.

DIVERTED DUE TO GEN 1 OFF BUS CAS APPROXIMATELY 2.5 HOURS INTO A FLIGHT FROM KSFO TO KPHL. CREW FOLLOWED QRH, DESCENDED TO FL310, AND STARTED THE APU. AT APPROXIMATELY 3 HOURS INTO THE FLIGHT, ADDITIONAL ALERTS WERE RECEIVED: ENGINE 1 EXCEEDANCE AND ENGINE 1 LOW OIL PRESSURE. THE CREW REDUCED ENGINE 1 POWER TO IDLE PER QRH INSTRUCTIONS. THE AIRCRAFT LANDED SAFELY AT KSTL. REPLACED GEN 1 IAW EMB-545/550 AMM 24-31-01.

CREW RECEIVED FLAP FAIL CAS AFTER SELECTING FLAPS 1 FROM 0 IN FLIGHT BEFORE LANDING. REPLACED THE FCE #1 IAW EMB 505 AMM 27-03-01. PERFORMED FLAP RIGGING PROCEDURE AND ALL REQUIRED OPS CHECKS.

DIVERTED DUE TO A TRIPPED CB LABELED "OVRHD" ON THE COCKPIT LIGHTS SECTION OF THE RH CB PANEL AND AN ELECTRICAL BURNING SMELL REPORTEDLY COMING FROM BENEATH THE PILOT'S SEAT. CREW FOLLOWED THE QRH, WHICH APPEARED TO ISOLATE THE ISSUE. AIRCRAFT LANDED WITHOUT INCIDENT AT KCLT. TECHNICIAN INSPECTED THE BACKSIDE OF THE RH CB PANEL AND FOUND NO SIGNS OF SHORTED WIRES. AFTER POWERING UP THE AIRCRAFT AND RESETTING THE "OVRHD" CB, TECHNICIAN OPERATED BOTH OVERHEAD LIGHTING DIMMER SWITCHES THROUGH ALL POSITIONS AND LEFT THE LIGHTS ON FULL BRIGHT FOR 15 MINUTES. THE CB DID NOT TRIP AGAIN. FAULT COULD NOT BE DUPLICATED; NO DEFECTS NOTED IAW AMM 24-60-01.

DURING CLIMB OUT FROM KSJC, THE SIC NOTICED A SMOKE SMELL AND VISIBLE LIGHT SMOKE. CREW TURNED OFF ENGINE BLEEDS WHICH REDUCED THE QUANTITY OF SMOKE. THE CREW DID NOT DON OXYGEN MASKS DUE TO THE SHORT FLIGHT DURATION. AIRCRAFT LANDED WITHOUT INCIDENT AT KNUQ. TROUBLESHOOTING TRACED THE ISSUE TO A SEIZED AIR CYCLE MACHINE. REPLACED THE AIR CYCLE MACHINE WITH A REPAIRED UNIT IAW AMM 21-52-13. OPS CHECK AND LEAK CHECKS GOOD.

PTRIM NML FAIL CAS WITH X OVER TRIM INDICATION FOLLOWING STAB TRIM MOVEMENT ANOMALY AFTER DE-ICE PROCEDURE. TRIM INITIALLY MOVED TO 0.0 DURING DE-ICE AND RETURNED TO T/O POSITION AFTERWARD, TRIGGERING THE CAS MESSAGE. CREW PERFORMED AN ELECTRICAL RESET, BUT THE FAULT DID NOT CLEAR. REPLACED FCE #2 IAW EMB 505 AMM 2-60-00. PERFORMED RIGGING OF THE MULTIFUNCTION SPOILER SYSTEM IAW 27-50-00 AND VERIFIED RIGGING WAS WITHIN LIMITS. CONDUCTED OPS CHECKS OF FLAPS, MULTIFUNCTION SPOILERS, AND PITCH TRIM; ALL CHECKS GOOD WITH NO CAS MESSAGES RELATED TO FCE #2 PRESENT.

CREW RECEIVED GND SPOILER FAIL CAS MESSAGE DURING DESCENT. ATC INSTRUCTED THE CREW TO REDUCE SPEED TO 190 KNOTS; THE CREW ATTEMPTED TO DEPLOY SPEED BRAKES AT APPROXIMATELY 225 KNOTS. A GND SPOILER FAIL CAS MESSAGE APPEARED, AND THE SPOILER BOX INDICATED A FAILURE. REPLACED FCE #2 IAW AMM 27-03-01-400-801. PERFORMED SPOILER RIGGING IAW AMM 27-60-00/800-801. OPS CHECK GOOD WITH NO DEFECTS FOUND.

DURING CLIMB THE #2 ENGINE ROLLED BACK APPROXIMATELY 0.2-0.3 EPR. POWER RESTORED WITHIN 2-3 SECONDS WITHOUT ANY CAS MESSAGES OR UNUSUAL PARAMETERS NOTED. APPROXIMATELY 2 MINUTES LATER, #2 ENGINE ROLLED BACK AGAIN BY 0.2-0.3 EPR AND RESTORED WITHIN 2-3 SECONDS, FOLLOWED BY A CYAN R FADEC FAULT MESSAGE. THE CAS MESSAGE CLEARED FROM THE EICAS APPROXIMATELY 10 MINUTES LATER. NO FURTHER ABNORMAL POWER INDICATIONS OR CAS MESSAGES OCCURRED DURING THE REMAINDER OF THE FLIGHT. SWAPPED THE EEC FROM #1 ENGINE TO THE #2 ENGINE AND VICE VERSA IAW RR EMM 73-21-01 AND BD-700 XRS AMM 71-00-00. PERFORMED 5 ENGINE RUNS OF 5 MINUTES EACH WITH 15-MINUTE SHUTDOWNS BETWEEN RUNS. OPS CHECK GOOD WITH NO DEFECTS NOTED.

ON TAXI OUT, CREW RECEIVED PITCH TRIM BACKUP FAIL CAS. CREW PERFORMED MULTIPLE SOFT RESETS USING CIRCUIT BREAKERS WITH NO SUCCESS. AFTER RETURNING TO THE FBO, A FULL ELECTRICAL RESET WAS PERFORMED, BUT THE BACKUP PITCH TRIM FAIL CAS MESSAGE REMAINED. REPLACED FCE1 IAW AMM 27-03-01. OPS CHECK GOOD WITH NO DEFECTS FOUND.

PILOT’S WINDSHIELD STARTED TO ARC AND THEN SHATTERED WHILE ON DESCENT INTO KTME. AIRCRAFT LANDED WITHOUT INCIDENT. POST-FLIGHT INSPECTION REVEALED THE PILOT’S WINDSHIELD WAS MELTED AT THE ARCING AREA. REPLACED THE LH WINDSHIELD IAW G450 AMM 56-11-01. REPLACED THE LEFT WINDSHIELD HEAT CONTROLLER IAW G450 AMM 30-41-01. LEAK CHECKS AND OPS CHECKS GOOD.

PITCH TRIM BACKUP FAIL CAS MESSAGE DURING SYSTEM TEST. REPLACED FCE1 IAW AMM 27-03-01. RIGGING AND OPS CHECK GOOD.

AIRCRAFT EXPERIENCED BRAKE FAILURE WHILE HOLDING SHORT OF RUNWAY 26R, WITH BRAKE FAIL CAS MESSAGE ILLUMINATING AND THE AIRCRAFT BEGINNING TO ROLL. CREW MANEUVERED THE AIRCRAFT AWAY FROM THE HOLD SHORT LINE AND ONTO THE RAMP TO REMAIN CLEAR OF THE TAXIWAY. THE PARKING BRAKE WAS USED TO STOP THE AIRCRAFT ABRUPTLY, PREVENTING REENTRY INTO THE ACTIVE TAXIWAY. HYDRAULIC SYSTEM AND EMERGENCY BRAKE ACCUMULATOR PRESSURE WERE NORMAL, WITH THE HYDRAULIC RESERVOIR PROPERLY CHECKED AND WITHIN LIMITS. TROUBLESHOOTING LED TO A FAULTING BRAKE CONTROL MODULE (BCM). REPLACED BCM IAW PH300 AMM 32-41-07. PERFORMED HYDRAULIC SYSTEM BLEEDING IAW 29-10-00 AND BRAKE FUNCTION CHECK IAW 32-41-00. BRAKE FUNCTIONAL TEST WAS SATISFACTORY.

REPLACED FCE #1 DUE TO PITCH TRIM BACKUP FAIL CAS POSTED DURING FLIGHT. WORK COMPLETED IAW EMB 505 AMM 27-03-01. OPS CHECK GOOD. RIG CHECKS GOOD. NO DEFECTS FOUND.

DIVERTED DUE TO GEN 2 BUS OFF CAS AND RELATED MESSAGES WHILE CLIMBING THROUGH FL430. THE SIC RAN THE CHECKLIST AND ATTEMPTED TO RESET THE GENERATOR, BUT THE ISSUE PERSISTED. THE CREW DESCENDED TO FL310, DECLARED AN EMERGENCY, AND DIVERTED TO KRDU. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND #2 GENERATOR SHAFT SHEARED. REPLACED #2 GENERATOR WITH CUSTOMER-SUPPLIED NEW GENERATOR IAW EMB-550 AMM 24-31-01. OPS CHECK GOOD

DIVERTED DUE TO CPCS LOW AIRFLOW DURING CRUISE TO KRME. CABIN ALTITUDE INITIALLY AT 6,500'. CREW FOLLOWED AFM PROCEDURES, TURNING ON WING ANTI-ICE, WHICH CLEARED THE CAUTION. AFTER CONTACTING MAINTENANCE, CREW SWITCHED TO MANUAL CONTROL AND TURNED ANTI-ICE OFF, CAUSING RAPID CABIN ALTITUDE CLIMB TO 10,000'. EMERGENCY DESCENT INITIATED, CREW DONNED OXYGEN MASKS, AND CABIN ALTITUDE STABILIZED AT 15,000' AGL. AIRCRAFT DIVERTED TO KTEB AND LANDED SAFELY. REPLACED CABIN PRESSURE CONTROLLER IAW G450 AMM 21-31-01. PERFORMED SYSTEM AND PRESSURIZATION CONTROL CHECKS IAW G450 MM 21-31-00; OPS CHECK SATISFACTORY.