Owner type
Co-owned, fractional ownership
Serial number
680A0084
Year built
2017
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
June 5, 2017
Certificate issued
July 29, 2025
Expires
July 31, 2032
Mode S code
A6DD12

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 3

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

2018In forceSuperseded2026
ADs by the year they took effect: 3 ADs
20181
20231
20261

Information bulletins that may apply

Advisory, not mandatory.

No bulletins matched this aircraft’s models

NTSB investigations

No NTSB investigations matched to N541QSMatched 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 Textron 680A aircraft

FAA incident reports

No FAA accident or incident reports matched to N541QSMatched 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 Textron 680A aircraft

Service difficulty reports · 9

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

SDR 2026FA0000691Panel · corrodedCORROSION WAS FOUND IN THE NOSE LANDING GEAR ACTUATOR TUNNEL AROUND A HYDRAULIC LINE STANDOFF. DURING THE REPAIR A HOLE WAS MISLOCATED NEAR THE DEFECT. THE CORROSION WAS REMOVED AND NDT WAS ACCOMPLISHED TO VERIFY REMAINING MATERIAL THICKNESS AND THAT NO CRACKSSep 14, 2026 · N541QS · Cessna 680A · Fuselage Main, StructureSDR DXTA2025070204096Static Wick · brokenDURING TOW OF N541QS THE THIRD STATIC WICK FROM THE WINGTIP OF THE LEFT WING MADE CONTACT WITH THE RIGHT LEADING EDGE OF N959QS AND BROKE OFF. CORRECTIVE ACTION; VISUALLY INSPECTED LEFT WING TRAILING EDGE. THE ONLY DAMAGE APPEARS TO BE A BROKEN STATIC WICK. REJun 30, 2025 · N541QS · Cessna 680A · Pitot/Static SystemSDR 3J7R202302800001Impact Switch · activatedFOUND THE FWD EMERGENCY LIGHTS ON WITH THE SWITCH BEING IN THE "OFF" POSITION.Jul 28, 2023 · N541QS · Cessna 680A · Emergency LightingSDR DXTA2023041083940Window · brokenFIRST OFFICER COCKPIT WINDOW: ON DESCENT COPILOTS SIDE WINDOW CRACKED SIGNIFICANTLY. REMOVED FIRST OFFICER COCKPIT WINDOW REF. CE680A AMM 56-10-05 INSTALLED NEW FIRST OFFICER COCKPIT SIDE WINDOW PER CE-680A MM 56-10-05 STEP 5. STEP 6 THROUGH END NEEDS COMPLEApr 8, 2023 · N541QS · Cessna 680A · Flight Compartment WindowsSDR DXTA2022032158700Warning Message · illuminatedFUEL BST PUMP ON R AMBER CAS: ENROUTE MOVED THE CROSSFEED SWITCH FROM RIGHT TO OFF. CAS MESSAGE FUEL BST PUMP R DISPLAYS IN AMBER AND DIAGRAM SHOWED AMBER BOOST PUMP ON. FOLLOWED CHECKLIST PROCEDURE TO MANUALLY TURN ON RIGHT BOOST PUMP AND CAS MESSAGE TURNEDMar 21, 2022 · N541QS · Cessna 680A · Aircraft Fuel SystemSDR DXTA2022020356110Apu · defectiveAPU SMOKE: SMOKE EVIDENT IN CABIN WITH APU RUNNING, BLEEDS OFF. THOUGHT IT WAS THE VACUUM. TURNED BLEEDS ON AND THICK GRAY SMOKE FILLED CABIN.///SIGN-OFF/// REMOVED AND REPLACED THE APU. IAW CE-680A MM 49-10-00. OPS CHECK GOOD.Feb 2, 2022 · N541QS · Cessna 680A · APU Cowling/ContainmentSDR DXTA2022011755320Battery · abnormalBATTERY OTEMP R RED CAS: RIGHT BATTERY OVERHEAT CAS MSG. HAD AT ABOUT 13K. FLUCTUATED BETWEEN COOL AND 105C. SEATTLED AT 73C. RAN CK LIST. LANDED. CKED BATTERY ONCE ON GROUND. WAS COOL. // SIGNOFF// REMOVED RH SIDE BATTERY AND INSTALLED NJA SUPPLIED OVERHAJan 16, 2022 · N541QS · Cessna 680A · Battery/Charger SystemSDR DXTA2020112104386Proximity Switch · failedMAIN DOOR OPEN AMBER CAS MESSAGE DOOR OPEN. ILLUMINATED WITH DOOR CLOSED AND LOCKED. CHECKLIST FOLLOWED. MESSAGE DID NOT CLEAR AND IS CYCLING ON AND OFF. CORRECTIVE ACTION: REMOVED CABIN DOOR PROXIMITY SWITCHES PIN: S2800-1257 AND S2800-1256. REMOVED CABINov 21, 2020 · N541QS · Cessna 680A · Passenger/Crew DoorsSDR 2020F00375Support Frame · crackedNOSE LANDING GEAR WHEEL WELL FRAME CRACK.Sep 22, 2020 · N541QS · Cessna 680A · Fuselage Main, Structure
Reports on N541QS not matched to an aircraft · 1

They name N541QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

STCs that may be installed · 16

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

See all 16 STCs