N412QS

ATA 5210

Part: HANDLE — BROKEN (ZONE 800) · airframe 6,431 hrs · 5,024 cycles

MAIN DOOR HANDLE: MAIN DOOR HANDLE BROKE OFF CLOSING AND LOCKING DOOR. CORRECTIVE ACTION: PERFORMED REMOVAL OF BROKEN MAIN ENTRY DOOR HANDLE AND INSTALL NEW CUSTOMER SUPPLIED MAIN ENTRY DOOR HANDLE P/N: 505-09870-403 NSN, OPS CHECK GOOD ALL WORK PERFORMED IAW EMB-505 AMM 52-11-24

ATA 3350

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 6,074 hrs · 4,748 cycles

WITH SWITCH IN ARM POSITION CABIN AND EXTERIOR EMERGENCY LIGHTS ARE ILLUMINATED. DURING LAST FLIGHT PASSENGERS HIGHLIGHTED EMERGENCY LIGHTS FLASHED PERIODICALLY DURING THE PERIOD 25 MIN BEFORE LANDING UNTIL WE TURNED THEM OFF FOR ENGINE SHUTDOWN. REPLACED BATTERIES. OPS CHECK GOOD. IAW PHENOM 300 AMM 33-52-01.

ATA 2730

Part: ELECTRONIC UNIT — INTERMITTENT (NR 2) · airframe 6,044 hrs · 4,722 cycles

PTRIM NML FAIL CAS MESSAGE AT FL430. REPLACED INTERMITTENT #2 FCE. OPS CHECK GOOD. WORK PERFORMED IAW AMM 27-03-01, 27-60-00, 21-31-00

ATA 2120

Part: UNKNOWN — ODOR (CABIN) · airframe 54,719 hrs · 4,251 cycles

ON DEPARTURE, WE NOTICED A BURNING OIL SMELL THAT PERMEATED THE CABIN AND DISSIPATED OVERTIME. DURING CRUISE THERE WAS NO SMELL, BUT IT DID COME BACK ON DESCENT DURING ARRIVAL. PERFORMED CLEANING OF THE FWD AND AFT CABIN EVAPORATORS. BLEW DRAIN LINES CLEAR OF DEBRIS AND CLEANED FINS AS NEEDED. WORK PERFORMED IAW AMM 21-52-03.

ATA 3350

Part: BATTERY — DEFECTIVE (ZONE 100) · airframe 5,162 hrs · 4,013 cycles

WHEN SWITCH IS IN ARM POSITION, EMERGENCY LIGHTS FLASH. BEGAN TROUBLESHOOTING & CONNECTED GPU TO ACFT. APPLIED ELECTRICAL POWER & TURNED EMERGENCY LIGHTS ON, ALL LIGHT ILLUMINATED. THEN TURN LIGHTS TO ARM & LIGHTS ILLUMINATED FOR APPROX 3 MINS & BEGAN TO FLICKER. COMPLIED WITH TC-505·33·200403 EMERGENCY LIGHTS BATTERY TOP CHARGE. REV 0. LEFT LIGHTS SWITCH TO ARM WITH POWER APPLIED FOR HALF HOUR, LIGHTS CONTINUED TO FLICKER, LEFT LIGHT SWITCH TO ARM WITH POWER SUPPLIED FOR ANOTHER HOUR & LIGHTS CONTINUED TO FLICKER. REMOVED CONNECTOR TO NR 2 BATTERY & LIGHT STOPPED FLICKERING. SUSPECT NR 2 BATTERY FAILURE, REMOVED NR 2 BATTERY & INSTALLED REPAIRED BATTERY. INSTALLATION & OPS CHECKS GOOD IAW MM 33-52·01.

ATA 3350

Part: BATTERY — DEFECTIVE · airframe 3,613 hrs · 2,822 cycles

THE EMERGENCY LIGHTS REMAIN ILLUMINATED WHEN THE EMER LT SWITCH IS IN THE ARM POSITION UNDER MAIN DC POWER. THE LIGHTS TURN OFF PROPERLY WHEN SELECTING THE SWITCH TO OFF.//CORRECTIVE ACTION// REMOVED AND REPLACED BOTH #1 & #2 EMERGENCY LIGHT BATTERIES. NO FURTHER DEFECTS NOTED. EMB505 MM 33-52-01 BATTERY PN OFF 7450L-00 SN OFF #1 001518 SN OFF #2 001359. INSTALLED PN 7450L-00 SN ON #1 005900 SN ON #2 006017

ATA 2120

Part: UNKNOWN — ODOR (CABIN) · airframe 2,991 hrs · 2,305 cycles

PNEUMATIC DISTRIBUTION: DURING INITIAL CLIMBOUT AND FLAP RETRACTION, A VERY STRONG ODOR WAS DETECTED BY BOTH PILOTS. IT LASTED ABOUT 45 SECONDS WITH NO SMOKE PRESENT. THE SMELL SUBSIDED AS WE RETURNED TO NASSAU. // SIGNOFF // PER EMBRAER CONTACT CENTER CASE # EEJ-04197444 PERFORMED FIM 21-20-00-810-801-A AND NOTED NO DEFECTS. COULD NOT DUPLICATE DISCREPANCY FOR PRECAUTIONARY REASON GAINED ACCESS TO AND CLEANED THE AVIONICS BLOWERS FAN IAW PHENOM 300 AMM 31-41-07 AND NOTED NO DEFECTS.

ATA 5210

Part: BUSHING — LACK OF LUBE (PAX DOOR) · airframe 2,396 hrs · 1,873 cycles

MAIN ENTRANCE DOOR DIFFICULT TO OPEN. SIGN-OFF. INSPECTED MAIN DOOR, NOTED LUBRICATION A LITTLE DRY ON THE ESSENTRIC BUSHING AND LOCK PINS. CLEANED AND LUBED BUSHING/LOCK PINS, AS REQUIRED. DOOR OPERATES SATISFACTORY. ALL WORK DONE PER PHENOM 300 AMM 55-1-23.

ATA 5500

Part: BALANCE WEIGHT — CORRODED (STAB) · airframe 2,376 hrs · 1,857 cycles

DURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (15 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G). ALL WEIGHTS HAS 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 MASS BALANCE WEIGHTS BELOW TOLERANCE: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (13 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PART NUMBER PE915109-L42 (1 EACH BELOW MINIMUM OF 1095G); ALL WEIGHTS HAS 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.