Safety record in brief:1 NTSB accident (substantial damage, Aug 2013)5 ADs may apply9 service difficulty reports
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The flight crew's failure to execute a go-around during a non-stabilized approach, which resulted in a runway overrun.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN13LA462)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2026-03-05 | Autopilot Main Servo | Mar 31, 2026 | Airframe (EMB-505)Certain serial numbers: EMB-505 50500004–50500012; EMB-505 50500014; EMB-505 50500016–50500665; EMB-505 50500667–50500779 |
| 2022-05-12 | Elevator Structure; 5540, Rudder Structure; and 5751, Ailerons | Apr 13, 2022 | Airframe (EMB-505) |
| 2021-24-21 | Operations | Jan 25, 2022 | Airframe (EMB-505)Only with: EMB-500 with PW617F-E or PW617F1-E engines installed, or EMB-505 with PW535E engines installed. |
| 2016-22-02 | Equipment/ Furnishing | Dec 1, 2016 | Airframe (EMB-505)Serial numbers per Embraer S.A. SB No. 500-25-0016 and SB No. 505-25-0020, dated December 8, 2015. Only with: Applies to passenger seats installed at manufacture; seats replaced during routine maintenance are not affected. |
| 2014-19-01 | Landing Gear | Oct 22, 2014 | Airframe (EMB-505)Only with: Equipped with brake assembly P/N DAP00097-01 or P/N DAP00097-02. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
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.
From FAA Service Difficulty Reports; matched by N-number and serial number.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…
From FAA Service Difficulty Reports; matched by N-number and serial number.AIR TURN BACK DUE TO PTRIM NML FAIL CAS MESSAGE AFTER MANUAL PITCH TRIM ACTIVATION RESULTED IN NO TRIM INPUT NEAR THE INITIAL LEVEL-OFF ALTITUDE. BACKUP MODE PITCH TRIM WAS USED FOR THE REMAINDER OF THE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT AT KMDW. REPLACED #1 FCE IAW EMB 505 AMM 27-03-01. OPS…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE #2 FCE FAILED DURING ENGINE RUNS. UNIT WAS SWAPPED AND FAULT FOLLOWED UNIT. REPLACED #2 FCE IAW PHENOM 300 AMM 27-03-01.
From FAA Service Difficulty Reports; matched by N-number and serial number.CREW RECEIVED SWPS FAULT, FLAP FAIL AND PTRIM BKP FAIL CAS IN FLIGHT. EXECUTED NO FLAP LANDING. REPLACED FCE #1 IAW PHENOM AMM 27-03-01. ALL FOLLOW-ON CHECK PASSED AND NO FURTHER CAS MESSAGES PRESENT.
From FAA Service Difficulty Reports; matched by N-number and serial number.ABNORMAL SOUND COMING FROM UNDER RH COCKPIT SEAT. ELEVATOR CONTROL FEELS LIKE SOMETHING IS DRAGGING WHEN ACTUATED BY THE CONTROL YOKE. REPLACED ELEVATOR SERVO ACTUATOR. REPLACED ELEVATOR SERVO MOUNT. ACCOMPLISHED ELEVATOR MOVEMENT. ACCOMPLISHED ELEVATOR SERVO OPS CHECK—NO FURTHER DEFECTS FOUND.…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING DESCENT, SPOILER FAIL CAS MESSAGE. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 FCE, IAW PHENOM 300 AMM 27-03-01-400-801. PERFORMED ALL ASSOCIATED RIGGING AND OPERATIONS CHECKS, PER TASK 37-03-01-400-801. ALL OPERATIONS CHECKS GOOD. P/N 462900-1017; S/N 1168.
From FAA Service Difficulty Reports; matched by N-number and serial number.DIVERTED DUE TO "BLEED 2 LEAK" CAS MESSAGE. COMPLETED QRH PROCEDURE AND CAS MESSAGE CLEAR. DURING DECENT CAS MESSAGE CAME BACK. COMPLETED QRH PROCEDURES TO SECOND END POINT AND CAS MESSAGE CLEARED AND REMAINED OFF FOR REMAINDER OF FLIGHT. CREW DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT.…
From FAA Service Difficulty Reports; matched by N-number and serial number.ON DESCENT CREW RECEIVED HYD HIGH TEMP CASS MSG. EXECUTED CHECKLIST & RESULTED IN LOSS OF HYD SYS. DECLARED EMER. UPON LANDING, UTILIZED EMER BRAKES & BLEW BOTH MAIN TIRES ON RUNWAY. FOUND LOOSE CONNECTOR P0589 AT HYD TEMP SWITCH. THE CONNECTOR WAS ADJUSTED & ALL FUNCTIONAL CHECKS WERE SATISFACTORY.
From FAA Service Difficulty Reports; matched by N-number and serial number.