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N361QS

Open the Markdown

2008 Cessna 680 · Pratt & Whitney Canada PW306C

Open in FAA registry

Owner type
Corporation
Serial number
680-0235
Year built
2008
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
October 27, 2008
Certificate issued
January 4, 2021
Expires
January 31, 2028
Mode S code
A41172
Cessna 680Airframe model · 9 seats · 2 engines · 253 registeredTCDS T00012WIAirframe · Cessna 680TCDS E35NEEngine · Pratt & Whitney Canada PW306C

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 11

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1978In forceSuperseded2026

Information bulletins that may apply · 2

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N361QSMatched 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 Cessna 680 aircraft

FAA incident reports

No FAA accident or incident reports matched to N361QSMatched 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 Cessna 680 aircraft

Service difficulty reports · 51

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

SDR DXTA2026093009937Spring · brokenWHEN CLOSING THE MAIN ENTRY DOOR, THERE WAS A LOUD POP AND THE FORWARD CLOSING ASSIST CABLE BECAME SLACK. INSPECTED MED FOUND BROKEN FWD COUNTERBALANCE SPRING AND BROKEN MED OVER CENTER PUSHROD. REMOVED AND REPLACED MED FWD FAILED COUNTERBALANCE SPRING, AND Sep 28, 2026 · N361QS · Cessna 680SOV · Passenger/Crew DoorsSDR 2026F00110Landing · corrodedFOUND SIGNS OF CORROSION UNDER 9 NUTPLATES UNDER PANEL 154BC. MECHANICALLY REMOVED 9 AREAS OF CORROSION LOCATED WHERE 8 NUTPLATES WERE PREVIOUSLY REMOVED INSIDE FUSELAGE BAY 154BC IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSMay 18, 2026 · N361QS · Cessna 680A · Fuselage Miscellaneous StructureSDR 2026F00109Landing · corrodedBUBBLING PRIMER AND WHITE POWDER AROUND AND UNDER 26 NUTPLATES UNDER PANEL 154AC. MECHANICALLY REMOVED CORROSION LOCATED WHERE 26 NUTPLATES WERE PREVIOUSLY REMOVED IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW CESSNA 680 SRM 51-7May 18, 2026 · N361QS · Cessna 680A · Fuselage Miscellaneous Structure
See all 51 reports
Reports on N361QS not matched to an aircraft · 15

They name N361QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR DXTA200702369Pressure Switch · malfunctionedON FINAL APPROACH THE BRAKE LOW PRESSURE AND ANTI SKID INOP LIGHT ANNUNCIATORS ILLUMINATED FOR ABOUT 10 SECONDS AND THEN EXTINGUISHED. DURING TAXI THE LIGHTS ILLUMINATED AGAIN AND BOTH THE CAPTAIN AND F/O BRAKES BECOME EXTREMELY MUSHY. AFTER ABOUT 10 SECONDSJul 31, 2007 · N361QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200702212Master Cylinder · leakingCO-PILOTS BRAKES ARE SPONGY WITH EXCESSIVE TRAVEL BEFORE BECOMING EFFECTIVE. INSPECTED LT AND RT CO-PILOT BRAKE MASTER CYLINDERS FOUND LEAKING. REMOVED AND REPLACED LT AND RT BRAKE MASTER CYLINDERS WITH A OVERHAULED UNITS AND SECURED; BLED BRAKE SYST. AS REQMay 22, 2007 · N361QS · Cessna 560CESSNA · Master Cylinder/Brake ValveSDR DXTA200702203Brake Assy · weakBOTH CO-PILOTS BRAKES ARE SPONGY, THE PEDALS TRAVEL ABOUT 1/4 WAY DOWN BEFORE THE BRAKES APPLY. PERFORMED BRAKE BLEEDING PROCEDURE. OPS CHECK NORMAL AT THIS TIME, WORK PERFORMED IAW CE-560 MM CHAP 32-42-00.May 17, 2007 · N361QS · Cessna 560CESSNA · Landing Gear Brake System

STCs that may be installed · 50

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 50 STCs