N418QS

ATA 2810

Part: PRESSURE SWITCH — DEFECTIVE (FUEL PUMP) · airframe 7,200 hrs · 5,662 cycles

FUEL 2 FEED FAULT, APPEARED WHEN CLIMBING THROUGH FL400. NO OTHER MESSAGES APPEARED. WHEN PULLING UP THE FUEL SCHEMATIC WE SAW THAT JET PUMP INDICATOR HAD A YELLOW X OVER IT AND WAS BEING FED BY THE ELECTRIC FUEL PUMP. REPLACED PRESSURE SWITCH. OPS CHECK GOOD. IAW AMM 28-45-01.

ATA 3350

Part: BATTERY — FAULTED (ZONE 200) · airframe 7,086 hrs · 5,580 cycles

WITH THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION THE CABIN EMERGENCY LIGHTING BLINKS ON AND OFF. REMOVED AND REPLACED FORWARD AND AFT BATTERIES WITH REPAIRED UNITS AND COMPILED WITH DEPLETE AND FULL CHARGE PROCEDURE IAW AMM 33-52-01, OPS CHECK GOOD

ATA 5297

Part: WIRE — DAMAGED (ZONE 800) · airframe 6,838 hrs · 5,380 cycles

DOOR PAX CAS ILLUMINATED THREE TIMES IN FLIGHT. FIRST FOR ABOUT 20 SECONDS EXTINGUISHED BEFORE LEVELING OFF AND BEING ABLE TO ACCOMPLISH QRH. ILLUMINATED 2 MORE TIMES FOR ABOUT 5 SECONDS. NO ILLUMINATION BELOW 15,000 FEET. CORRECTIVE ACTION: REPAIRED WIRE. OPS CHECK GOOD. IAW EMB50 SWPM 20-41-20

ATA 2750

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 6,598 hrs · 5,188 cycles

FLAP FAIL YELLOW CAS: IN CRUISE FLIGHT AT FL 430 RECEIVED FLAP FAIL YELLOW CAS MESSAGE AS WELL AS SWPS FAULT AND PTRIM BKP FAIL CAS ASSOCIATES WITH FCE FAILURE. FLAP INDICATION HAD YELLOW X OVER IT AS WELL AS DID THE PITCH TRIM INDICATIONS. PITCH TRIM WORKED NORMALLY CORRECTIVE ACTION: ARRIVED AT AIRPLANE AND SECURED. REQUESTED GPU FROM TINE SERVICE DEPARTMENT AND WAITED FOR IT. FORMATTED SD CARD AND POWERED UP AIRPLANE. LET IT STABILIZE, AND DOWNLOADED CMC DATA AND SENT IT TO EMBRAER CONTACT CENTER AND AWAITED RESULTS AND RECOMMENDATIONS. MONITORED AIRPLANE FOR SEVERAL MINUTES TO SEE IF CAS MESSAGES APPEARED, NONE NOTED. ON THE RECOMMENDATION OF EMBRAER CONTACT CENTER, PERFORMED WIRE CHECKS REF FIM TASK 27-36-00-810-816-A, AND TASK 27-03-00-810-811-A. NO DEFECTS NOTED. REMOVED ACCESS PANELS 241AZ, 241CZ, AND 241DZ TO FACILITATE ACCESS TO #1 FCE BOX. REMOVED STATIC INVERTER #3 TO FACILITATE ACCESS TO #1 FCE. REMOVED #1 FCE P/N 462900-1017, S/N 0505, AND REPLACED WITH TESTED FCE P/N 462900-1017, S/N 1071. REINSTALLED #3 STATIC INVERTER, REINSTALLED ACCESS PANELS 241AZ, 241CZ, AND 241DZ IAW EMBRAER PHENOM 300 AMM 27-03-01. REFER TO PARKER HANNIFIN CORPORATION 8130# 203054479 FOR DETAILS. PERFORMED FLAP SYSTEM RIGGING IAW PHENOM 300 AMM TASK 27-50-00-820-801-A, NO DEFECTS NOTED. PERFORMED FLAP SYSTEM OPERATIONAL CHECK 5 TIMES IAW PHENOM 300 AMM TASK 27-50-00-710-801-A, OPS CHECK GOOD AND NO DEFECTS NOTED. PERFORMED PITCH TRIM OPERATIONAL CHECK S TIMES IAW PHENOM 300 AMM TASK 27-40-00-710-801-A, OPS CHECK GOOD AND NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECKS OF THE PRESSURIZATION SYSTEM IAW PHENOM 300 AMM TASKS 21-31-00-710-801-A, 21-31-00-710-B02-A AND 21-31-00-710-803-A. ALL OPS CHECKS GOOD AND NO DEFECTS NOTED. ORIGINAL SUBMISSION DATE: 5/2/2025.

ATA 5100

Part: STRUCTURE — NO DISCREPANCY · airframe 6,460 hrs · 5,076 cycles

DAMAGE INSPECTION: AIRCRAFT OVER SPEED CROSSING A LINE OF WEATHER AT FLIGHT LEVEL 450 DESCENDING TO FLIGHT LEVEL 430 WE ENCOUNTERED MODERATE TURBULENCE IN CLEAR AIR. AIRPLANE ACCELERATED RAPIDLY AND OVERSPEED APPROXIMATELY 10 KTS AND WE RECEIVED ONE HIGH-SPEED ORAL WARNING. AIRPLANE WAS IN THE CLEAN CONFIGURATION AND OVER SPEED CONDITION LASTED FOR ABOUT 2 TO 3 SECONDS. CORRECTIVE ACTION; PERFORMED A SATISFACTORY PHASE-1 INSPECTION WITH NO DEFECTS NOTED AT THIS TIME. WORK PERFORMED IAW EMB PHENOM 300 AMM 5-50-04, 31,31,00

ATA 5210

Part: SPRING — BROKEN (DOOR HANDLE) · airframe 6,128 hrs · 4,827 cycles

MAIN DOOR HANDLE: EXTERIOR MAIN ENTRANCE DOOR HANDLE DOES NOT STOW WHEN DOOR IS CLOSED AND LATCHED USING EITHER THE INTERIOR OR EXTERIOR HANDLE. CORRECTIVE ACTION; FOUND THAT THE SPRING INSIDE THE DOOR HANDLE TO BE BROKEN. REPLACED WITH A NEW SPRING. REATTACHED THE DOOR AND REINSTALLED THE PANELS, PERFORMED OPERATIONAL CHECK OF THE DOOR AND THE DOOR HANDLE STOWS. OPERATIONAL CHECK GOOD, WORK PERFORMED IAW EMB 505 AMM 52-11-24,

ATA 3350

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 5,175 hrs · 4,097 cycles

EMERGENCY LIGHTS BLINKING FOR THE LAST 35 MIN OF FLIGHT IN TO SDL. COMPLIED WITH FIM TASK 33-50-00-810-802-A. FOUND WITH ELECTRICAL CONNECTOR P1360 DISCONNECTED, EMERGENCY LIGHTS DO NOT COME ON IN ARM POSITION. PER FIM TASK, REPLACEMENT OF THE EMERGENCY LIGHT BATTERY 2 IS REQUIRED. BATTERY PLACED ON ORDER BY CUSTOMER. PERFORMED WORK IAW EMBRAER 505 FIM CH. 33-50-00-810-802-A. (JH-12/18/23) REMOVED AND REPLACED AFT EMERGENCY BATTERY WITH "NEW" IAW PHENOM 300 MM 33-52-01-400-801-A. ALL FOLLOW ON CHECKS PASS WITH NO DEFECTS NOTED.

ATA 2210

Part: UNKNOWN — DEFECTIVE (FCE 2) · airframe 4,947 hrs · 3,904 cycles

AUTOPILOT SYSTEM: FLIGHT CONTROL ELECTRONIC FAILURE -FCE2 FAILURE TO INCLUDE GND SPLR FAIL, PTRIM NML FAIL, SPOILER FAULT //SIGNOFF// ARRIVED AT THE AIRCRAFT AND APPLIED POWER WITH A GPU REF EMBSOS AFM. TECHS NOTED NO ACTIVE FAULTS AT THIS TIME. PERFORMED OPERATIONAL CHECK OF THE HORIZONTAL PITCH TRIM SYSTEM IAW EM8505 MM 27-40-00 WITH NO DEFECTS NOTED. PERFORMED THE OPERATIONAL CHECK OF THE MULTIFUNCTION SPOILER SYSTEM IAW EMBSOS MM 27-60-00 WITH NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF THE FLAP SYSTEM !AW EMB505 MM 27-50-00 WITH NO DEFECTS NOTED. DOWNLOADED THE PREVIOUS CMC CAS ENG FILES AND SENT TO CONTACT CENTER FOR FURTHER REVIEW. CONTACT CENTER RECOMMENDED TECHS COMPLY WITH FIM 27-03-00-810-812. TECHS COMPLIED WITH FIM 27-03-00-810-812 WITH NO DEFECTS NOTED. REMOVED POWER FROM THE AIRCRAFT. GAINED ACCESS TO THE FCE 2 AS REQUIRED. PERFORMED GVI OF FCE 2 SECURITY, CANNON PLUGS, AND ASSOCIATED WIRING WITH NO DEFECTS NOTED, CONTACTED MCC WITH FINDINGS. DUE TO NO HISTORY MCC ELECTS TO REPLACE THE FCE 2 AND CONTINUE TO MONITOR. AWAITED REPLACEMENT FCE. RECEIVED REPAIRED FCE AND ALL PAPERWORK MATCHES. REMOVED FAULTY FCE 2 PN: 462900-1017 SN: 1229 AND INSTALLED REPAIRED FCE 2 PN: 462900-1017 SN: 0112 REF EM8505 MM 27-03-01. PERFORMED RIGGING PROCEDURE OF THE MULTIFUNCTION SPOILER SYSTEM IAW EMBSOS MM 27-60-00, PERFORMED THE OPERATIONAL CHECK OF THE MULTIFUNCTION SPOILER SYSTEM 5 TIMES REF EMBSOS MM 27-60-00 WITH NO DEFECTS NOTED, PERFORMED THE OPERATIONAL CHECK OF THE PITCH TRIM OPERATIONAL CHECK 5 TIMES REF EMBSOS MM 27-40-00 WITH NO DEFECTS NOTED. PERFORMED OPERATIONAL MANUAL PRESS CONTROL MODE OPERATIONAL CHECK REF EMB505 21-31-00 WITH NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF THE AUTOMATIC PRESSURIZATION CONTROL MODE REF EMB505 21-31-00 WITH NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY CABIN DECOMPRESSION REF EMB505 21-31-00 WITH NO DEFECTS NOTED. REMOVED POWER FROM THE AIRCRAFT. CLOSED ALL ACCESS AS REQUIRED.

ATA 3350

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHTS) · airframe 3,473 hrs · 2,736 cycles

CABIN EMERG LIGHT: CABIN EMERGANCY LIGHTING FLICKERED ON AND OFF, IN FLIGH. POWERED UP AIRCRAFT AND TURNED EMERGENCY LIGHTS ON, EMERGENCY LIGHTS BEGAN TO FUCKER, GAINED ACCESS TO THE FWD AND AFT EMERGENCY BATTERY PACKS, REMOVED THE FWD EMERGENCY BATTERY P/N: 6450LS·OO, S/N: 000818, INSTALLED A NEW EMERGENCY BATTERY IN THE FWD POSITION P/N1 74SOLS·OO, S/N: 006142, REMOVED THE AFT EMERGENCY BATTERY P/N: 64SOLS-OO, 5/N: 001904. INSTALLED A NEW EMERGENCY BATTERY IN THE AFT POSITION P/NI 7450LS-OO, S/N: 006340, PERFORMED EMERGENCY BATTERY OPERATIONAL TEST, OPERATIONAL TEST IS GOOD AT THIS TIME, PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST, OPERATIONAL TEST IS GOOD AT THIS TIME, RECHARGED THE EMERGENCY LIGHT BATTERIES FOR 90 MINUTES, EMERGENCY LIGHTS DID NOT FLICKER AFTER NEW EMERGENCY BATTERIES WERE RECHARGED, CLOSED UP FWD AND AFT ACCESS, PHENOM 300 AMM 33·52-01 AND 33-52·00,

ATA 2150

Part: MODULE — LEAKING (COMPRESSOR DRIVE) · airframe 1,939 hrs · 1,523 cycles

CLIMBING THROUGH FL260 ALL OF SUDDEN A VERY STRONG ELECTRICAL BURNING SMELL. FO CONFIRMED, AS WELL AS, THE PASSENGER. DECLARED EMERGENCY AND PERFORMED CHECKLIST. DIVERTED INTO LOCAL AIRPORT AND AS WE DESCENDED SMELL DISSIPATED. ON BASE TO FINAL AFTER GEAR AND FLAPS EXTENDED ANOTHER VERY STRONG BURNING SMELL RETURNED, BUT THIS WAS MORE OF AN OILY RUBBER BURNING SMELL. NO SMOKE PRESENT BUT WE ELECTED TO STOP THE AIRCRAFT ON THE RUNWAY AND EVACUATE. EVAC CHECKLIST WAS COMPLETED. FIRE DEPARTMENT COULD NOT FIND ANY HOT SPOTS AND PLANE WAS TOWED TO FBO. CORRECTIVE ACTION: INSPECTED A/C WIRING, CONNECTOR AND COMPONENTS IN COCKPIT AND AFT EQUIPMENT AREA. INSPECTED BAGGAGE AREA WIRING, COMPONENTS AND CONNECTORS. FOUND COMPRESSOR DRIVE MODULE LEAKING OIL. REMOVED AND REPLACED COMPRESSOR DRIVE MODULE AND RECEIVER DRYER ASSEMBLY, PER PHENOM 300 AMM 21-52-01, 21-52-07. PERFORMED FUNCTIONAL CHECK PER PHENOM 300 AMM 21-52-00. OPERATIONS CHECKS GOOD.

ATA 5540

Part: BALANCE WEIGHT — CORRODED (LT ELEVATOR) · airframe 1,774 hrs · 1,391 cycles

DURING ACCOMPLISHMENT OF SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING LEFT ELEVATOR ADJUSTABLE MASS BALANCE WEIGHTS BELOW TOLERANCE: PART NUMBER PE915109-L33 (6 EACH) AS FOLLOWS 5=83G,82G (MINIMUM 84G) AND HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH) 1=1093G (MINIMUM 1086G). ALL WEIGHTS HAVE BEEN REPLACED WITH A NEW MASS WEIGHTS AND THE ELEVATOR BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED.THE ELEVATOR WAS RE-IDENTIFIED TO PART NUMBER 505-11082-601, AS PER SERVICE BULLETIN INSTRUCTIONS. WE ALSO NOTED THE FOLLOWING RIGHT ELEVATOR ADJUSTABLE MASS BALANCE WEIGHTS BELOW TOLERANCE: PART NUMBER PE915109-L33 (7 EACH) AS FOLLOWS 3=83G, 2=82G, 81G, 80G (MINIMUM 84G) AND HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH) 1=1093G (MINIMUM 1095G). ALL WEIGHTS HAVE BEEN REPLACED WITH A NEW MASS WEIGHTS AND THE ELEVATOR BALANCING WAS PERFORMED WITH NO FURTHER DEFECTS NOTED. THE ELEVATOR WAS RE-IDENTIFIED TO PART NUMBER 505-11082-602, AS PER SERVICE BULLETIN INSTRUCTIONS. THIS REPORT COMPLIES WITH FAA 14 CFR PART 135 OPERATOR’S GMM REQUIREMENTS