- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500161
- Year built
- 2013
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- September 16, 2013
- Certificate issued
- May 18, 2022
- Expires
- May 31, 2029
- Mode S code
- A35E8A
Embraer S A EMB-505TCDS A60CEAirframe · Embraer S A 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 S A 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 S A 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 N316QSMatched 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 S A EMB-505 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025110305492Battery Pack · malfunctionedTAXIING FOR TAKEOFF, ALL EMERGENCY LIGHTS STARTED FLICKERING. WHEN EMERGENCY SWITCH IN THE OFF POSITION, EMERGENCY LIGHTS SOMETIMES ON & SOMETIMES OFF. REMOVED NR 1 EMERGENCY BATTERY DUE TO LIGHTS FLICKER AND INSTALLED A REPAIRED ASSY IAW AMM 33-52-01. ALL CHESDR DXTA2025051103452Elec Connector · looseCABIN EMERG LIGHT: DURING POST-FLIGHT, THE OVERHEAD EMERGENCY LIGHT LOCATED BETWEEN SEAT 3 AND SEAT 4 IS INOPERATIVE. CORRECTIVE ACTION: FOUND THE CONNECTOR TO BE LOOSE ON EMER/COURTESY LIGHT. RECONNECTED CONNECTOR AS REQUIRED. PERFORMED OPS CHECK. OPS CHECK GSDR DXTA2025022502456Door · faultedMAIN ENTRY DOOR NEEDS TO BE EVALUATED; DOOR TENDS TO DROP/SLAM WITHOUT GUIDANCE. REMOVED FOD. OPS CHECK GOOD. IAW EMB-505 AMM CH 52-14-00.SDR DXTA2025012102010Strut · defectiveLG LEVER DISAG RED CAS: REPEAT WRITE UP. ON TAKEOFF, RECIEVED RED "LG LEVER DISAG" CAS WHEN LG LEVER SELECTED UP. CYCLED LG PER QRH AND CONDITION RETURNED. RECIEVED 3-GREEN INDICATION WHEN LG LEVER SELECTED DOWN. LANDED UNEVENTFULLY. CORRECTIVE ACTION: REPSDR DXTA2024022010940Battery · unknownAC GENERATION AND CONTROL: AFTER TAKEOFF, WE GOT CAS EMER LIGHT NOT ARMED AND THE EMER LIGHTS WERE PHYSICALLY ON (THIS SEEMED TO SUPPORT WHAT WE LATER DISCOVERED, AS THEY WERE RESPONDING TO THE ELECTRICAL PROBLEM) WE THEN NOTICED BOTH MAIN BATTERIES WERE NOT SDR DXTA2024010510519Shutoff Valve · defectiveCABIN PRESSURIZATION CONTROL: DURING CLIMB OUT ~12000-14000' WE HAD AN ECS VALVE 2 FAILURE - PULLED UP THE ECS PAGE AND CONFIRMED IT. APPROXIMATELY 17000' IT CLEARED AND THE CABIN PRESSURE BEGAN TO READJUST (DECREASING). AT APPROXIMATELY 22000-23000' WE RECESDR DXTA2023101097610Unknown · unknownWITH THE CABIN DOOR, OPEN, TOP RIGHT BOLT CAME OUT. WASHER FELL INTO THE DOOR COWLING. THIS HAPPENED DURING PASSENGER BOARDING. GAINED ACCESS TO MED INTERIOR AND RETRIEVED THE WASHER AND THE SCREW REINSTALLED THE PREVIOUSLY GAINED ACCESS INSTALLED THE HARDWARESDR DXTA2023060187500Unknown · unknownMAIN ENTRANCE DOOR HANDLE BROKE OFF AT THE BASE WHILE A HUB SERVICE TECH WAS CLOSING THE DOOR. PERFORMED AN OPS CHECK AND TROUBLESHOOTING PLUS VISUAL INSPECTION OF INNER DOOR OPEN AND LOCKING MECHANISM AND LATCH PINS. NO OBVIOUS DEFECTS NOTED AT THIS . COULD SDR DXTA2022080867530None · noneCABIN EMERG LIGHT: EMERGENCY LIGHTS FLICKERING ON/OFF IN FLIGHT.SDR DXTA2022072566700Battery · defectiveCABIN EMERGENCY LIGHTS FLASHING IN ARM POSITION. // SIGNOFF// GAINED ACCESS TO FWD EMERGENCY BATTERY BY REMOVING FLOOR PANEL 223CLF. REMOVED INOP EMERGENCY BATTERY P/N 6450LS-00 S/N 001876 AND INSTALLED NEW CUSTOMER SUPPLIED EMERGENCY BATTERY P/N 7450LS-00 S/NSDR 2020FA0000535Balance Weight · corrodedDURING 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 (11 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PSDR DXTA2014091505881Transducer · inoperativeWHEEL BRAKES PULSE & GRAB UNEVENLY DURING LANDING ROLLOUT, CAUSING SIGNIFICANT DIRECTIONAL CONTROL DIFFICULTY DURING BRAKING. THEREAFTER THE BRAKES PULSE DURING TAXI-IN. IT FEELS LIKE THE RT BRAKE IS GRABBING MORE THAN THE LT. PERFORMED MAIN BRAKE SYS INSPESDR DXTA2013121205595Actuator · faultyWHEN THE GEAR IS SELECTED TO THE DOWN POSITION THE NOSE GEAR REMAINS IN THE UP & LOCKED POSITION UNTIL THE MAIN GEAR IS DOWN & LOCKED THEN THE NOSE GEAR EXTENDS. R & R NLG DOWN LOCK RELEASE ACTUATOR. OPERATIONS CHECKED IAW 300 MM 32-21-03. R & R NLG UP LOCK
Reports on N316QS not matched to an aircraft · 15
They name N316QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2011032104516Pressure Switch · failedNORMAL BRAKE FAILED ON LANDING ROLL. ON SHORT FINAL (100 FT AGL) "POWER BRAKE LOW PRESS" AND "ANTI SKID INOP" ANNUNCIATORS ILLUMINATED, ON LANDING NORMAL BRAKES SLOWED THE AIRCRAFT TO A WALKING SPEED, THEN FAILED COMPLETELY. THE EMERGENCY BRAKE HANDLE WAS USEDSDR DXTA2011010304385Line · leakingOUT OF 4000 FT THE LT ENG FIRE LIGHT CAME ON, PULLED POWER TO IDLE AND LIGHT WENT OUT. LANDED WITH NO OTHER LIGHTS. REMOVED COWLING AND INSPECTED ENGINE FOR HOT STAB. NO DAMAGE NOTED RAN ENG AND FOUND INBD BLEED AIR LINE LEAKING. INSTALLED NEW LINE ASSY ISDR DXTA2010081604191Motor · smokeSMOKE SEEN COMING FROM HELLHOLE, AC NOW INOP, NO SIGN OF CHARRING OR ANY OTHER SIGN OF DAMAGE. ODOR COMING FROM INSIDE MOTOR. REMOVED FREON FROM SYS. REMOVED ACFT PALLET FROM TAIL OF ACFT, WORK COMPLETED IAW MM 21-52-00. REMOVED FAILED FUSE LIMITER. INSTAL
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