OpenAirDocs.org

N372QS

Open the Markdown

2008 Cessna 680 · Pratt & Whitney Canada PW306C

Open in FAA registry

Owner type
Corporation
Serial number
680-0201
Year built
2008
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, normal
Airworthiness date
May 5, 2008
Certificate issued
September 12, 2025
Expires
September 30, 2032
Mode S code
A43CA8
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 N372QSMatched 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 · 2

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Incident 20220910009389ITakeoff: Climb Out · Las Vegas, NV[privacy data omitted] Departed klas rwy 19R on 9/10/2022 at 1351Z. After departure, the crew selected gear up and received an unlock gear cas message. Crew ran the qrh but was unable to clear the cas message. The crew then selected gear down and received an…Sep 10, 2022 · Minor damageIncident 20080730856309ITakeoff · Charleston, SCDuring landing roll out the aircraft struck a deer on the runway. The deer caused damage to one of two taxilights. The right landing gear door and the right flap were also damaged. There were no injuries andthe aircraft sustained minor damage.Jul 30, 2008 · Minor damage

Service difficulty reports · 28

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

SDR DXTA2026060808336Trim System · inoperativeON DEPARTURE WE RECEIVED AP FAIL A CAS MESSAGE. REENGAGED AP AND RECEIVED AP FAIL B CAS MESSAGE ALSO. WE FOUND THE PRIMARY STAB TRIM TO BE INOPERATIVE WITH NO PRIMARY STAB TRIM FAIL CAS MESSAGE. WE USED SECONDARY TRIM AND LANDED WITHOUT ISSUE. REMOVED ELEVATOJun 4, 2026 · N372QS · Cessna 680SOV · Autopilot SystemSDR DXTA2025120205930Brake Sys · malfunctionedAFTER PARKING AND SETTING THE BRAKE THE RIGHT BRAKE CALIPER WAS SMOKING WITH BRAKES SET AND RELEASED. PERFORMED GVI OF BOTH RT MLG BRAKES AND WHEEL ASSEMBLIES WITH NO LEAKS OR DEFECTS NOTED. SET BRAKES AND LET SIT FOR 30 MINUTES WITH NO DEFECTS AND PUMPED BRDec 1, 2025 · N372QS · Cessna 680SOV · Landing Gear Brake SystemSDR DXTA2025111005614Cable · out of adjustMAIN DOOR DOES NOT GO DOWN ALL THE WAY. IT STAYS UP ABOUT AN INCH AND WHEN THE PASSENGERS STEP ON IT, IT DROPS THAT INCH UNTIL THE ARMS ARE FULLY EXTENDED. CABLE TENSION NEED TO BE ADJUSTED ACCOMPLISHED THE CABLE TENSION , INSPECTED FOUND CABLE TO MUCH TENSIONov 7, 2025 · N372QS · Cessna 680SOV · Passenger/Crew Doors
See all 28 reports
Reports on N372QS not matched to an aircraft · 13

They name N372QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR DXTA200701875Uplock Switch · malfunctionedRT MAIN GEAR UPLOCK FAILED. HAD A GEAR UNLOCK LIGHT ON WITH A HYDRAULIC PTRS ON LIGHT. RAN THE HYDRAULIC PRES ON CK LIST AND WHEN WE PULLED THE GEAR CONTROL (CB) AS DIRECTED THE RT MAIN GEAR EXTENDED. THE GEAR HANDLE WAS THEN PLACED IN THE GEAR DOWN POS. RESEJan 23, 2007 · N372QS · Cessna 560CESSNA · Landing Gear Retraction/Extension SystemSDR DXTA200601781Throttle · out of rigLT ENGINE SHUT ITSELF DOWN FOLLOWING SPEED BRAKE TEST. THROTTLE WAS AT IDLE. FOUND LT ENGINE IDLE SET TOO LOW AND THROTTLE LINKAGE OUT OF RIG. RIGGED LT ENGINE THROTTLE LINKAGE AND ADJUSTED LOW IDLE. OPS CHECKS GOOD IAW MM 71-00-00.Dec 6, 2006 · N372QS · Cessna 560CESSNA · Power LeverSDR DXTA200601398Fcu · out of adjustLT ENGINE WOULD NOT MAKE TAKEOFF POWER SHORTLY AFTER LIFTOFF. DURING SPEED BRAKE CHECK, ENGINE SHUT DOWN WHEN THROTTLE PULLED BACK TO IDLE. PERFORMED ENGINE BLEED AIR LEAK CHECK, NO LEAKS NOTED. ADJUSTED FUEL CONTROL/ FLOW DIVIDER INTERCONNECT ROD IAW THE MM May 18, 2006 · N372QS · Cessna 560CESSNA · Fuel Control/Turbine Engines

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