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N392QS

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2016 Embraer Executive EMB-505 · Pratt & Whitney Canada PW535E

Open in FAA registry

Owner type
Co-owned
Serial number
50500349
Year built
2016
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, commuter
Airworthiness date
May 25, 2016
Certificate issued
August 10, 2026
Expires
August 31, 2033
Mode S code
A48BA6
Embraer Executive EMB-505Airframe model · 8 seats · 2 engines · 531 registeredTCDS A60CEAirframe · Embraer Executive EMB-505TCDS E00053ENEngine · Pratt & Whitney Canada PW535E

From the FAA registry file of October 24, 2026.

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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.

2011In forceSuperseded2026
See all 18 ADs

Information bulletins that may apply · 2

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N392QSMatched 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 N392QSMatched 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
Reports on N392QS not matched to an aircraft · 1

They name N392QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

Incident 19980118002089IGulstm 560 · Omaha, NENarrative: N392QS, a CE-560, was on an aircraft repositioning flight from minneapolis, MN, to aspen, co at 37,000 feet when the hydraulic pressure light came on. The aircraft landed at Omaha, NE. Cessna mechanics found a sticky hydraulic pressure switch…Jan 18, 1998

Service difficulty reports · 10

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR DXTA2025092905093Battery Pack · faultedALL EMER LIGHTS AND SIGNS FLASH WHEN IN FLIGHT AND ON GROUND. REPEAT WRITE UP CORRECTIVE ACTION: FOLLOWED EMB CONTACT CENTER RECOMMENDATION AND C/W SL505-33-0005-REV.05 DURING STEP 9 OF FIM 33-50-00-810-802-A FOUND AN ERROR IN THE MANUAL. CONFIRMED WITH EMB THSep 25, 2025 · N392QS · Emb EMB505 · Emergency LightingSDR DXTA2025092205015Battery Pack · dischargedON LIGHT TEST DURING PREFLIGHT ALL EMER LIGHTS JUST BLINK CONTINUOUSLY. AFTER BATTERY EXERCISE TASK CARD PROCEDURE WAS PERFORMED, NO DEFECTS WERE FOUND IN THE EMERGENCY BATTERIES. RE-CHARGED BATTERIES IAW TASK CARD TC-FLT-33-1001 REV 2 AND RESTORED TO ORIGISep 19, 2025 · N392QS · Emb EMB505 · Emergency LightingSDR DXTA2024042211563Switch · failedPASSENGER DOOR SHOWS RED ON STATUS PAGE. CANNOT VERIFY DOOR IS LATCHED. UPPER RIGHT WINDOW ONLY HAS PARTIAL GREEN INDICATION. REMOVED MED AIR STAIRS. CLEANED ALL GREEN HAGS WITH ISOPROPYL ALCOHOL AS NEEDED. VERIFIED ALL GREEN FLAGS ARE VISIBLE. WHILE STAIRS WApr 21, 2024 · N392QS · Emb EMB505 · Door Warning SystemSDR DXTA2023081492990Battery · defectiveEMER LIGHTS ARE ILLUMINATED WITH SWITCH IN THE ARM POSITION. REMOVED #1 EMERGENCY BATTERY 7450LS-00 SN 005266 DUE TO FAILING FUNCTIONAL CHECK INSTALLED NEW BATTERY PN 7450LS-00 SN 006958 IA W EMB-505S AMM 33-52-01-400-8010-A CHARGED AND OPS CHECKED GOOD. REAug 13, 2023 · N392QS · Emb EMB505 · Emergency LightingSDR DXTA2022070565130Battery · inoperativeEMER LT NOT ARM YELLOW CAS: EMER LIGHT NOT ARM CAS MESSAGE IS DISPLAYED AND WONT CLEAR WITH THE SWITCH IN THE ARM POSITION. " CORRECTIVE ACTION" REMOVED AND REPLACED #2 EMERGENCY BATTERY PN 6450LS-00 SN 001640 AND INSTALLED NEW CONDITION EMERGENCY BATTERY REF Jul 1, 2022 · N392QS · Emb EMB505 · Emergency LightingSDR DXTA2022061964140Ahrs · defectiveVENTRAL RUD FAIL WHITE CAS: CLIMBING THROUGH FL350 BOTH PFDS DISPLAYED HDG MISCOMPARE. SOON AFTER YAW DAMP FAIL CAS MESSAGE DISPLAYED. AP FAIL CAS COME ON SECONDS LATER. VENTRAL RUD FAIL CAS CAME ON MOMENTS AFTER. SLIGHT DUTCH ROLL WAS EXPERIENCED WHILE AT HIGJun 19, 2022 · N392QS · Emb EMB505 · Rudder Control SystemSDR DXTA2021082547630Light · burned outCABIN EMERG LIGHT: EMERGENCY LIGHT NUMBER 6 (BY THE LAV DOOR) INOP. REMOVED FAULTY EMERGENCY LIGHT NUMBER 6 IAW AMM CHAPTER 33-52-11. 08/24/21. INSTALLED A NEW LED ESCAPE PATH MARKING LIGHT ASSEMBLY NR 6 IAW AMM 33-52-11. OPS CHECK IS GOOD.Aug 24, 2021 · N392QS · Emb EMB505 · Emergency LightingSDR DXTA2021072645710Pdu · defectiveFLAP FAIL YELLOW CAS: FLAP FAIL CAS MESSAGE. FLAP FAIL MESSAGE APPEARED WHEN THE FLAP WERE MOVING FROM POSITION 2 TO 4. FLAPS ARE STUCK BETWEEN POSITION 2 AND 4. // SIGNOFF // POWERED AIRCRAFT AND CHECKED CAS. NO RELATED CAS NOTED. PERFORMED FLAP OPS CHECKS APJul 23, 2021 · N392QS · Emb EMB505 · Trailing Edge Flap Control SystemSDR 2021F00178Battery · no testDURING SCHEDULED FUNCTIONAL CHECK, THE FORWARD EMERGENCY LIGHTS BATTERY FAILED FUNCTIONAL TEST. THE BATTERY ASSEMBLY WAS REPLACED WITH A NEW UNIT (P/N 7450LS-00) AND FUNCTIONAL TEST WAS PERFORMED WITH SATISFACTORY RESULTS.Jun 28, 2021 · N392QS · Emb EMB505 · Emergency LightingSDR 2020FA0000408Balance Weight · corrodedDURING 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 PARTSep 16, 2020 · N392QS · Emb EMB505 · Elevator Structure
Reports on N392QS not matched to an aircraft · 7

They name N392QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR DXTA2010052704105Petcock · looseANTI-SKID BRAKE SYSTEM GRABS INTERMITTENTLY. FOUND LT BRAKE MANUAL BLEEDER LOOSE. TIGHTENED BLEEDER AND C/W ANTISKID SYS BRAKE BLEED AS REQUIRED C/W TAXI CHECK TAXI CHECK GOOD. IAW MM 32-42-00.May 26, 2010 · N392QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA2009021703510Handle · looseON FINAL THE FLAP HANDLE WOULD NOT GO PAST 15 DEG FLAPS. FOUND FLAP HANDLE TO BE LOOSE AND TIGHTENED ALL THE WAY DOWN ON ITS POST NOT ALLOWING ENOUGH MOVEMENT FOR THE SPRING PIN TO DISENGAGE FROM THE 15 DEGREE DETENT MOVING TOWARDS 35 DEGREES. ADJUSTED FLAP Feb 16, 2009 · N392QS · Cessna 560CESSNA · Trailing Edge Flap Control SystemSDR DXTA200702168Display · inoperativeDURING TAKEOFF, RMU NR 2 & THE NR 2 PFD BOTH WENT BLANK. AFTER A COUPLE SECONDS THE PFD WENT TO A RED X AND THEN ABOUT 10 SECONDS LATER A NORMAL DISPLAY CAME BACK ON. THE RMU TOOK ABOUT ONE MINUTE TO COME BACK ON & HAVE A NORMAL DISPLAY. FOUND NR 2 PFD INCORREMay 1, 2007 · N392QS · Cessna 560CESSNA · Central Display

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