- Owner type
- Co-owned
- Serial number
- 50500279
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- June 22, 2015
- Certificate issued
- August 13, 2026
- Expires
- August 31, 2033
- Mode S code
- A438F1
Embraer Executive EMB-505TCDS A60CEAirframe · Embraer Executive EMB-505TCDS E00053ENEngine · Pratt & Whitney Canada PW535E
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 13
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2011 | 1 |
|---|---|
| 2012 | 1 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2020 | 1 |
| 2022 | 2 |
| 2023 | 4 |
| 2024 | 1 |
| 2025 | 2 |
| 2026 | 2 |
Airframe · Embraer Executive EMB-505
AD 2026-10-18Flight Control SystemAD 2026-03-05Autopilot Main ServoAD 2024-22-06Cabin Equipment/FurnishingsInformation bulletins that may apply · 2
Advisory, not mandatory.
Airframe · Embraer Executive EMB-505
SAIB CE-16-23Navigation; Degraded Attitude and Heading Reference System (AHRS) Performance When Operating in Areas of Unreliable or Unavailable Global Positioning System (GPS) SignalSAIB CE-10-46Navigation; Embraer EMB-505 Terrain Awareness Warning System (TAWS) Instructions in Airplane Flight ManualNTSB investigations
No NTSB investigations matched to N371QSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Embraer Executive EMB-505 aircraft
FAA incident reports
No FAA accident or incident reports matched to N371QSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Embraer Executive EMB-505 aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025040702972Warning Message · false indicationAIR INTAKE ANTI-ICE / DE-ICE: A-I E1 FAIL AND A-I E2 FAIL CAS MESSAGE DISPLAYED DURING THE APPROACH PHASE. WE WERE OPERATING IN INSTRUMENT CONDITIONS AND THE TAT WAS 8C. CYCLING THE ENG1 AND ENG2 SWITCHES OFF AND BACK ON AGAIN CLEARED THE MESSAGE. CORRECTIVE ASDR DXTA2025010301763Battery Pack · inoperativeWHEN STARTING THE ENGINES, THE EMERGENCY LIGHTS COME ON. LOOKS LIKE THE BATTERY PACKS HAVE GONE BAD. REPLACED EMERGENCY BATTERIES. OPS CHECK GOOD. IAW PHENOM 300 AMM 24-61-00, 24-31-00, AND 33-50-00.SDR DXTA2024103100978Battery Pack · failedCABIN EMER LIGHTS FLASHING IN ARMED MODE DURING FLIGHT. CORRECTIVE ACTION; REPLACED #1 & #2 EMERGENCY BATTERY REF. EMB PHENOM AMM 33-52-01 OPS CHECK GOOD .SDR DXTA2023112710152Unknown · unknownCABIN EMERG LIGHT: CABIN EMERG LIGHTS STAY ON IN THE ARMED POSITION.///SIGN-OFF PERFORMED REACTIVATION OF INERTIA SWITCH IN REF TO EMB-505S AMM 33-52-17. OPS CHECK GOOD.SDR DXTA2023100997400Battery · inoperativeIN LEVEL FLIGHT AT ALTITUDE, CABIN EMERGENCY LIGHTS STARTED FLASHING ON & OFF FOR REMAINDER OF THE FLT. ARMED EMER BATTS AND FOUND THE LIGHTS TO FLASH. GAINED ACCESS TO BOTH 1 & 2 EMER BATTS, IT WAS NOTED THAT DURING OPS CHECKS 1 (COCKPIT BATT) WAS FOUND INOPSDR DXTA2023072491560Control Module · failedBRK FAIL YELLOW CAS: AFTER ENGINE START AND TAXI BEGAN OUT OF PARKING RECEIVED YELLOW CAS "BRK FAIL". DISCREPANCY WAS TROUBLESHOT DOWN TO A BRAKE CONTROL MODULE PER EMB505 FIM TASK L2-41-00-810-813·A. GAINED ACCESS, REMOVED AND REPLACED BRAKE CONTROL MODULE. SDR 2022FA0000138None · noneDISCREPANCY: DURING EMBRAER PHENOM 300 BASE CHECKLIST FOUND EMERGENCY LIGHT SWITCH INTERMITTENT IN ON POSITION. CORRECTIVE ACTION: FOUND THE EMERGENCY LIGHT SWITCH TO BE DEFECTIVE, PERFORMED REPLACEMENT OF THE COCKPIT LIGHTING SYSTEM CONTROL PART NUMBER 441-44SDR DXTA2021111051590Battery · inoperativeEMERGENCY LIGHTING: EXTERIOR AND INTERIOR EMERGENCY LIGHTING DOES NOT WORK WHEN ON GROUND POWER OR BATTERY. IN OFF POSITION EMERGENCY LIGHTING NOT ARMED CAS MESSAGE ILLUMINATES, IN ARM POSITION EMERGENCY LIGHT INTERIOR LIGHTS BLINK FOR ONE SECOND, IN THE ON PSDR DXTA2021051141860Fcu · defectiveFLAP FAIL YELLOW CAS: DURING LEVEL FLIGHT AT FL410, THE FOLLOWING MESSAGES WERE DISPLAYED: SWPS FAULT, SPOILER FAULT, FLAP FAIL, AND PTRIM BKP FAIL. REFERED TO AOB 20-05 TO CONFIRM FCE 1 FAILURE. RAN ALL CHECLISTS/QRH ASSOCOTED WITH THE CAS MESSAGES AND LASDR 2020FA0000358Balance Weight · corrodedDURING ACCOMPLISHMENT OF SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE LEFT AILERON MASS BALANCE WEIGHT PART NUMBER PE915109-L31 WAS UNDER THE WEIGHT LIMITS (1761 GRAMS) AS PRESCRIBED BY THE SERVICE BULLETIN (MINIMUM 1787 GRAMS) -21 GRAMSSDR DXTA2019010303283Shutoff Valve · failedBLEED 2 FAIL YELLOW CAS - PASSING THROUGH 15,000 FT IN ICING CONDITIONS AN ACRID SMELL PERMEATED THE CABIN AND THE BLEED 2 FAIL EICAS ILLUMINATED . UPON RESETTING THE BLEED WITH QRC PROCEDURE THE SMELL DISAPPEARED.. AND WING DEICING WAS REESTABLISHED.( CORRESDR DXTA201711300001Starter Gen · failedJUST AFTER STARTING THE TAXI, A STRONG ELECTRICAL BURNING SMELL FILLED THE COCKPIT AND CABIN. TROUBLESHOT BURNING SMELL. CAUSE OF SMELL SUSPECTED TO BE ASSOCIATED STARTER GENERATOR FAILURE. REMOVED AND REPLACED RT ENGINE STARTER GENERATOR. PERFORMED GROUND RUNSDR DXTAT2PL6D005EAU5Sensor · defectiveAT 36000FT. DUCT 2 OVERHEAT. FOLLOWED CHECKLIST. DUCT ONE OVERHEAT SHORTLY AFTER. INSTALLED A NEW NR 1 DUCT TEMPERATURE SENSOR AND NEW ECS TEMPERATURE CONTROLLER IAW MM 21-61-03 AND MM 21-61-01. OPS CHECKS PERFORMED MM 21-61-00-710-801A/500. OPS CHECKE
STCs that may be installed · 47
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 47 STCs
Earlier aircraft with this N-number · 1
This aircraft carried N371QS before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.