N310QS

ATA 3240

Part: TRANSDUCER — DEFECTIVE (WHEEL SPEED) · airframe 9,793 hrs · 7,641 cycles

BRK FAIL YELLOW CAS: BRK FAIL YELLOW CAS ILLUMINATED STARTING TAXI ROLL. USED PARKING BRAKE TO STOP AIRCRAFT. CORRECTIVE ACTION: REPLACED R/H WHEEL SPEED TRANSDUCER. OPS CHECK GOOD. IAW EMB PHENOM 300 AMM 32-41-06-000-801-A.

ATA 2700

Part: SPOILER SYS — FAULTED · airframe 9,660 hrs · 7,539 cycles

HORIZONTAL STAB CONTROL: WE WERE AT FL400, 2 YELLOW AND 1 WHITE CAS MESSAGES POPPED UP ON THE PFD (GND SPLR FAIL, PTRIM NML FAIL, AND SPOILER FAULT). WE CONSULTED THE QRH, LANDED AT DESTINATION SAFELY. CORRECTIVE ACTION; AS INSTRUCTED BY MCC, SWAPPED FCE1 & FCE2 IAW EMB505 AMM 27-03-01 AND PERFORMED ALL REQUIRED ELECTRICAL RIGGINGS ON FLAP/SPOILERS SYSTEM IAW EMB505 AMM 27-50-00 & 27-60-00. FOUND SYSTEM WORKING NORMALLY WITH NO CAS MESSAGES POSTED.

ATA 3350

Part: BATTERY — FAULTED (ZONE 200) · airframe 9,453 hrs · 7,396 cycles

DURING FLIGHT CABIN LIGHTS WOULD FLICKER WITH EMER LT ARMED DUPLICATED DISREPANCY. FOUND EMERGENCY LIGHT SWITCH LOOSE MOUINTING. GANED ACCESS TO BACK OF SWITCH ON LIGHT SWITCH PANEL AND RE-SECURED EMERGENCY LIGHT SWTCH. WORK. PERFORMED IAW EMB-505AMM 33-01-01. AFTER RESECURING SWITCH. FOUND AFT BATTERY LIGHT BATTERY PACK CAUSING LIGHTS TO COME ON AND ARM POSITON. REMOVED AND REPLACED N0.2 EMERGENCY LIGHT BATTERY PACKS WITH NEW UNITS OPS CHECK AND RE-CHARGE IAW EMB-505 33-52-0 1. OPS CHECK GOOD

ATA 3350

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 8,782 hrs · 6,883 cycles

CABIN EMERG LIGHT: DURING CRUISE FLIGHT CABIN EMERGENCY LIGHTING FLICKERING. REMOVED FAULTY EMERGENCY LIGHT POWER UNIT SIN 005715 AND REPLACED IT WITH TESTED EMERGENCY LIGHT POWER UNIT AND PERFORMED SATISFACTORY OPERATIONAL TEST. ALL MAINTENANCE PERFORMED IAW PHENOM 300 AMM 33-52-01. NO FURTHER DEFECTS NOTED AT THIS TIME.

ATA 3350

Part: LIGHT — UNKNOWN (CABIN) · airframe 8,782 hrs · 6,883 cycles

CABIN EMERG LIGHT: DURING CRUISE FLIGHT CABIN EMERGENCY LIGHTING FLICKERING.

ATA 3230

Part: VALVE — FAULTED (UNKNOWN) · airframe 8,663 hrs · 6,795 cycles

UPON MLG EXTEND, LEVER DISAGREE MESSAGE ILLUM WITH BOTH MAINS GREEN & NOSE RED. NLG WOULD NOT EXTEND. RAN CKLST. CYCLED MLG LEVER UP & DOWN, NO CONDITION CHANGE. PULLED FREE-FALL HANDLE. RECEIVED 3 GREEN. LANDED & TAXIED WITHOUT INCIDENT. PERFORMED CHECK OF EXTEN & RETRACT SYS. FOUND THE LG CMD C/B TRIPPED. AFTER PRESSED IN, & CYCLING MLG, C/B TRIPPED. TROUBLESHOT, A FAULTY MLG CONTROL LEVER IAW WD 32-61-50-1. R & R MLG CONTROL LEVER IAW AMM 32-31-01. R & R MLG SELECTOR VALVE LAW AMM 32-31-04, PERFORMED MLG EXTEND & RETRACT SYS CHECKS IAW AMM 32-31-00, & EMER EXTEND TEST IAW AMM 32-35-00, NO FAULTS. BLED MAIN HYD SYS IAW AMM 29-10-00 & PERFORMED BRAKE & EMER PARKING BRAKE SYS BLEEDING LAW AMM 12-13-00.

ATA 3350

Part: BATTERY PACK — DEFECTIVE · airframe 6,681 hrs · 5,237 cycles

EMERG EXIT SIGN/LIGHT: LIGHTS FLICKER IN THE ARMED POSITION.///SIGN-OFF///REMOVED AND REPLACED EMERGENCY BATTERY PACKS. IAW PHENOM AMM 33-52-010400. OPS CHECK GOOD.

ATA 2730

Part: BEARING — CORRODED (ELEVATORS) · airframe 5,828 hrs · 4,595 cycles

DISCREPANCY: WHILE DOING CONTROL CHECK NOTICED THE CONTROLS FELT COARSE AND HAD RESISTANCE. THEY DID NOT FEEL SMOOTH. THE CONTROLS STAY ON THE LAST POSITION AND DO NOT RETURN TO NEUTRAL POSITION. CORRECTIVE ACTION: ISOLATED LT AND RT ELEVATORS AT UPPER BELL CRANK ROD AND FOUND ELEVATORS TO HAVE ROUGH OPERATION. REMOVED LT AND RT ELEVATORS SURFACES IN ACCORDANCE WITH AND PERFORMED GVIS OF MECHANISM, NOTED LEFT AND RIGHT TORQUE TUBE SUPPORT BEARINGS PART NUMBER KP21BSFS428 CORRODED AND LT TORQUE TUBE PART NUMBER 505-11003-005 WITH DENT ON BEARING MOUNTING SURFACE. REPLACED LEFT AND RIGHT TORQUE TUBE SUPPORT BEARINGS PART NUMBER KP21BSFS428 AND LT TORQUE TUBE PART NUMBER 505-11003-005 WITH NEW PARTS, RE-INSTALLED LT AN RT ELEVATORS AND BELL CRANK RODS. PERFORMED GVI OF THE PILOT AND COPILOT YOKES ASSEMBLIES AND NOTED BEARINGS PART NUMBER MS27645-4A WORN ON BOTH YOKES’ SPECIAL JOINTS ASSEMBLIES, REPLACED PILOT AND COPILOT BEARINGS PART NUMBER MS27645-4A WITH NEW PARTS. PERFORMED ELEVATORS FUNCTIONAL CHECK AND ALL OPERATIONS ARE NORMAL AND SMOOTH AT THIS TIME. ALL WORK PERFORMED, IAW PHENOM 300 AMM 27-31-01, 27-31-04, 25-11-01, 27-01-03, 27-31-00 AND 20-10-06. THIS REPORT COMPLIES WITH FAA 14 CFR PART 135 OPERATOR'S GMM REQUIREMENTS.

ATA 5270

Part: SWITCH — FAULTY (PAX DOOR) · airframe 4,382 hrs · 3,448 cycles

DOOR EMER OPEN RED CAS ILLUMINATED-IN FLIGHT DESCENDING TO FL 290 DOOR PAX OPEN RED CAS MESSAGE ILLUMINATED. EMERGENCY DECLARED CHECKLIST COMPLETED LAND AS SOON AS POSSIBLE AS PER CHECKLIST. REPLACED MED DOOR SWITCH AND J0057 CONNECTOR PLUG. OPS CHECKED GOOD. REMOVED 505-25962-401 SWITCH, 330-00185-78 CONNECTOR.