N436QS

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 4,275 hrs · 3,317 cycles

CABIN EMERGENCY LIGHTS FLASHING INFLIGHT. REMOVED FAILED FWD BATTERY PACK & INSTALLED REPAIRED UNIT IAW AMM 33-52-01. REMOVED FAILED AFT BATTERY PACK & INSTALLED REPAIRED UNIT IAW AMM 33-52-01. OPS CHECKED GOOD IAW AMM 33-52-00.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 3,811 hrs · 2,930 cycles

NLG LANDING GEAR RETRACTION: ON DEPARTURE AFTER GEAR RETRACTION THE LG LEVER DISAG CAS CAME ON. QRH COMPLETED BUT DID NOT FIX PROBLEM. NOSE GEAR DID NOT RETRACT. APPROACH AND LANDING WERE NORMAL. USE SECOND PHOTO WITH RED NOSE GEAR INDICATION.

Part: BRAKE — DEFECTIVE (UNKNOWN) · airframe 3,811 hrs · 2,930 cycles

RIGHT MLG BRAKE: WHILE TAXIING TO RUNWAY THE RIGHT BRAKE STARTED LOCKING UP WHEN DEPRESSING THE BRAKE PEDAL, NO MATTER HOW GENTLY. IT SENT EXTREME SHUDDERS THROUGHOUT THE PLANE. IT WAS ESPECIALLY NOTICEABLE AS WE LINED UP ON THE RUNWAY AS WE HAD TO USE RIGHT BRAKE TO LINE UP. WE TAXIIED OFF RUNWAY AND PROCEEDED VERY SLOWLY BACK TO FBO.//CORRECTIVE ACTION//PERFORMED INITIAL INSPECTION OF RH MAIN WHEEL AND BRAKE. NO OBVIOUS DEFECTS NOTED. UPON INSPECTION, NOTED RH BRAKE HAD 3-4MM REMAINING, SUGGESTED TO MCC WE SHOULD REPLACE RH BRAKE AT THIS TIME AND PERFORM BRAKE BLEEDING PROCEDURE. REMOVED REPLACED RH FAULTY BRAKE ASSEMBLY WITH OH BRAKE ASSEMBLY. OPS CHECK GOOD. REF EMBRAER PHENOM 300 AMM 32-45-21/400 REMOVED BRAKE - PN: DAP0009 /-04 / SN: 50311141 INSTALLED BRAKE - PN: DAP00097-04 / SN. 5033VC CONDITION: OVERHAULED

Part: BRAKE SYS — INOPERATIVE (MLG) · airframe 3,338 hrs · 2,579 cycles

UPON POWERING UP THE ENGINES FOR TAKEOFF WITH THE BREAKS HELD FOR A STATIC TAKEOFF, YELLOW BRK FAIL CAS MESSAGE CAME ON AND THE BREAKS NO LONGER WORKED AT ALL. REMOVED AND INSTALLED REPAIRED WHEEL SPEED TRANSDUCER IAW AMM 32-41-06-400-801-A. OPS CHECK GOOD IAW AMM 32-41-06-710-801-A. REMOVED AND INSTALLED TESTED BRAKE CONTROL MODULE IAW AMM 32-41-07-400-801-A. PERFORMED FUNCTIONAL CHECK OF THE BRAKE SYSTEM IAW AMM 32-41-00-720-801-A/500. ALL CHECKS GOOD. ORIG SUB DATE: 12/29/2022

Part: NONE — DEFECTIVE (ZONE 100) · airframe 3,004 hrs · 2,310 cycles

CABIN EMERG LIGHT: ALL EMERGENCY LIGHTS CONTINUOUSLY FLICKER WITH SWITCH SELECTED TO ARMED AND ON POSITIONS. VIDEO ATTACHED. POWERD UP AIRCRAFT AND FOUND LIGHTS NOT FLICKING WITH SWITCH SELECTED TO ARMES. PERFORMED EMB 505 FIM TASK 33-50-00-810-802-A INCORRECT FUNCTIONING OF EMERGENCY LIGHTS", OPS CHECK GOOD BUT NOTED LIGHTS TURNS ON WITH SWITCH SELECTED TO ARM WITH POWER APPLIED (GPU AND BATTERIES) REF FIM TASK BLOCK 5 (STEP 6). REMOVED AND REPLACED COCKPIT EMERGENCY LIGHTS BATTERY SUPPLY AND PERFORMED EMERGENCY LIGHTS FUNCTIONAL CHECK REF EMB 505 AMM 33-52-01. OPS CHECK GOOD AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 892 hrs · 681 cycles

THE EMERGENCY LIGHTS BEGAN BLINKING WHILE IN THE ARM AND ON POSITIONS. CORRECTIVE ACTION: INSTALLED REPAIRED FWD EMERGENCY BATTERY AND MODIFIED AFT EMERGENCY BATTER, IAW AMM 33-52-00. PERFORMED SATISFACTORY OPERATIONS CHECK, IAW AMM 33-52-00-710 501A AND 33-52-01-710-801A.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 12,785 hrs · 6,288 cycles

FLOORBOARD PUNCTURED IN THE TOP SKIN OF FLOOR.

Part: HINGE FITTING — CORRODED (RUDDER) · corrosion level 2 · airframe 12,785 hrs · 6,288 cycles

VERTICAL FIN, RUDDER HINGE, LOWER FITTING IS PITTED.

Part: HINGE FITTING — CORRODED (RUDDER) · corrosion level 2 · airframe 12,785 hrs · 6,288 cycles

VERTICAL FIN, RUDDER HINGE, CENTER FITTING IS PITTED

Part: HINGE FITTING — CORRODED (RUDDER) · corrosion level 2 · airframe 12,785 hrs · 6,288 cycles

VERTICAL FIN, RUDDER HINGE, UPPER FITTING IS CORRODED.

Part: FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 12,785 hrs · 6,288 cycles

LEFT AND RIGHT HORIZ STAB PIVOT BUSHINGS AND LUGS CORRODED.

Part: HINGE FITTING — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 12,785 hrs · 6,288 cycles

LT ELEVATOR HINGE LINE NR 4 CORRODED.

Part: HINGE FITTING — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 12,785 hrs · 6,228 cycles

RT ELEVATOR HINGE LINE NR 4 CORRODED.

Part: HINGE FITTING — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 12,785 hrs · 6,288 cycles

LEFT ELEVATOR HINGE LINE NR 2 ON HORIZONTAL STAB HAS CORROSION BOTH FITTINGS.

Part: HINGE FITTING — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 12,785 hrs · 6,288 cycles

RIGHT ELEVATOR HINGE LINE NR 2 HAS CORROSION.

Part: HINGE FITTING — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 12,785 hrs · 6,288 cycles

LEFT ELEVATOR HINGE LINE NR 3 CORRODED.

Part: HINGE FITTING — CORRODED (RT ELEVATOR) · corrosion level 3 · airframe 12,785 hrs · 6,288 cycles

RIGHT NR 4 ELEVATOR HINGE HAS PITTED CORROSION, TOP AND BOTTON CONTACT SURFACES.

Part: HINGE FITTING — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 12,785 hrs · 6,288 cycles

RIGHT ELEVATOR HINGE LINE NR 3 CORRODED.

Part: HINGE — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 12,785 hrs · 6,288 cycles

LEFT ELEVATOR HINGE CORRODED.

Part: HINGE FITTING — CORRODED (RT ELEVATOR) · corrosion level 3 · airframe 12,785 hrs · 6,288 cycles

RIGHT ELEVATOR HINGE LINE NR 1 ON HORIZONTAL STAB HAS PITTED CORROSION AND ELONGATION IN BOTTOM FITTING.

Part: TORQUE TUBE — CORRODED (RUDDER) · corrosion level 3 · airframe 12,785 hrs · 6,288 cycles

RUDDER TORQUE TUBE IS PITTED BEYOND THE ALLOWABLE DAMAGE LIMITS

Part: FITTING — GOUGED (LT ENGINE) · airframe 12,122 hrs · 5,956 cycles

LEFT ENGINE AFT MOUNT FITTING HAS GOUGES AND SCRATCHES ON THE AFT VIBRATION ISOLATOR FITTING ON THE FORWARD FACE IN SEVERAL LOCATIONS.

Part: APU — ODOR · airframe 10,055 hrs · 4,902 cycles

AIR CONDITIONING SYSTEM PRODUCED A DIRTY SOCK ODOR. REMOVED LEFT AND RIGHT WATER SEPARATOR COALESCER BAG AND INSTALLED NEW. COMPLIED WITH CMP 215005 AIR CONDITIONING SYSTEM OPS TEST WITH NO DEFECTS NOTED. THERE IS STILL AN ODOR PRESENT ONLY WHEN THE APU IS RUNNING THE A/C PACKS. ISOLATED LEFT AND RIGHT PACK WITH NO DIFFERENCE. STARTED LEFT AND RIGHT ENGINES AND OPERATED BOTH PACKS FOR 30 MINUTES AND ODOR DISAPPEARED. SELECTED APU AS AIR SOURCE AND ODOR IMMEDIATLY RETURNED. CHECKED BOTH PACKS FOR PROPER OPERATION WITH NO DEFECTS FOUND. REMOVED APU AND INSTALLED A REPAIRED UNIT. COMPLIED WITH CMP MSG3 490052 OPS TEST. OPS AND LEAK CHECKED GOOD. CHECKED BOTH PACKS FOR PROPER OPERATION WITH NO DEFECTS FOUND.

Part: COALESCER BAG — ODOR (LEFT) · airframe 9,476 hrs · 4,621 cycles

DURING CLIMB, NOTICED A VERY STRONG EXHAUST ODOR THROUGHOUT THE ENTIRE CABIN. THE ODOR TEMPORARILY FADED BUT REAPPEARED ABOUT 10 MINUTES INTO THE FLIGHT AND REMAINED. DONNED MASKS AND DROPPED PAX MASKS AND RETURNED TO DEPARTURE. AFTER LANDING THE ODOR WAS STILL VERY STRONG. NO SMOKE WAS OBSERVED ANYWHERE IN THE CABIN. 20 MINUTES AFTER COMPLETE SHUTDOWN OF ENGINES AND APU, AND WITH THE MAIN CABIN DOOR AND BAGGAGE DOOR OPEN TO VENTILATE THE CABIN, COULD STILL DETECT A VERY STRONG ODOR COMING FROM THE AFT LAVATORY AREA. R & R RT AND LT WATER SEPARATOR COALESCER BAGS IAW GIV MSG3 CMP 217078 AND 217077. R & R AFT TOILET DUE TO GAS INDUCTION INTO THE SYS. RAN APU WITH BLEED AIR ON FOR 20 MINUTES, CYCLED THROUGH ALL TEMPERATURE RANGES. NO SMOKE OR EXHAUST ODOR IS EVIDENT.

Part: COALESCER BAG — ODOR (CABIN) · airframe 8,254 hrs · 4,021 cycles

STRONG EXHAUST & FUEL ODOR PREVALENT IN CABIN UPON DESCENT. ODOR WAS VERY STRONG AND WAS FIRST NOTICED ON DESCENT THROUGHOUT APPROXIMATELY 10,000FT. R & R WATER SEPARATOR BAGS . PERFORMED OPS AND LEAK CHECKS WITH NO DEFECTS OR ODORS NOTED. ALL WORK DONE IAW CMP 'S.

Part: OVEN — ODOR (GALLEY) · airframe 7,891 hrs · 3,846 cycles

ABOUT 30 MINUTES INTO FLIGHT, THE F/A TURNED THE OVEN ON TO WARM SOME BREAD. WITHIN A FEW MINUTES SHE NOTICED THE AREA HAD AN ELECTRICAL BURNING ODOR AND AN ODOR OTHER THAN BURNED FOOD. SHE ALSO STATED SHE NOTICED SMOKE INSIDE THE OVEN DOOR WINDOW. THE OVEN WAS TURNED OFF AND THE CIRCUIT BREAKER WAS PULLED TO DEACTIVATE THE SYS AND THERE WERE NO FURTHER ISSUES.

Part: SAFETY VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 7,758 hrs · 3,787 cycles

DURING CLIMB, CABIN PRESURIZATION BECAME ERRATIC AND UNCONTROLABLE. CREW DESCENDED IMEDIATELY. CABIN LOW WARNING ILLUMINATED. OPEN.

Part: THROTTLE CABLE — BROKEN (LT ENGINE) · airframe 7,721 hrs · 3,767 cycles

CREW REPORTED LT THROTTLE IS LOOSE AND INOPERATIVE. MX FOUND LT THROTTLE CABLE BROKEN UNDER FLOOR IN AFT LAV JUST FWD OF WHERE CABLE TURNS UPWARD AT AFT LAV AFT WALL. CABLE APPARENTLY HAD BEEN FRAYING ON STRUCTURE PRIOR TO BREAKING.

Part: WIRE HARNESS — FAILED (STEER BY WIRE)

STEER BY WIRE FAILURE ON LANDING ROLLOUT.

Part: SERVO VALVE — FAILED (NLG STEERING)

NOSE STEERING FAILED ON LANDING.

Part: MANIFOLD — FAILED (STEER BY WIRE)

STEER BY WIRE FAILED ON LANDING.

Part: STEERING SYS — OUT OF ADJUST (NLG) · airframe 4,390 hrs · 2,148 cycles

STEERING LAGS WHEN TURNED TO LT WITH TILLER OR RUDDER PEDALS. PERFORMED ADJUSTMENT CHECK IAW GIV MM 32-05-00.

Part: STEERING SYS — MALFUNCTIONED (NLG)

STEERING LAGS WHEN TURNED TO LT WITH TILLER OR RUDDER PEDALS. PERFORMED ADJUSTMENT CHECK IAW MM 32-05-00.