# N372QS: 2008 Cessna 680

- Status: Valid registration
- Airframe: [Cessna 680](https://openairdocs.org/model/cessna-680) (registry code 2076811, 9 seats)
- Engine: [Pratt & Whitney Canada PW306C](https://openairdocs.org/engine/pratt-whitney-canada-pw306c) (registry code 52169)
- Data sheets: [TCDS T00012WI](https://openairdocs.org/tcds/T00012WI) (Textron Aviation Inc.), [TCDS E35NE](https://openairdocs.org/tcds/E35NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 680-0201
- Year built: 2008
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, normal
- Airworthiness date: May 5, 2008
- Certificate issued: September 12, 2025
- Expires: September 30, 2032
- Mode S code: A43CA8
- Owner type: Corporation
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=372QS
- Page: https://openairdocs.org/aircraft/N372QS

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 11 in force

### Matched by airframe (Cessna 680)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2018-07-13](https://openairdocs.org/ad/2018-07-13): Landing Gear · Textron 510, 680 and 680A. Effective May 15, 2018
- [AD 2017-06-13](https://openairdocs.org/ad/2017-06-13): Fuselage · Textron 680. Effective May 2, 2017
- [AD 2012-07-04](https://openairdocs.org/ad/2012-07-04): Electrical Power · Cessna 680. Effective May 15, 2012
- [AD 2007-26-16](https://openairdocs.org/ad/2007-26-16): Aft fairing wire bundle assembly · Cessna 680. Effective Jan 18, 2008
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 2005-08-03](https://openairdocs.org/ad/2005-08-03): Cockpit display units · Cessna 680. Effective Apr 29, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998
- [AD 78-05-06](https://openairdocs.org/ad/78-05-06): Flexible Fuel Cells · Cessna 180, 182, 185 and 98 more. Effective Jun 30, 1978

### Matched by engine (Pratt & Whitney Canada PW306C)

None in force.

## Information bulletins (advisory) (2 in force)

- [SAIB NM-10-45](https://openairdocs.org/saib/NM-10-45): Landing Gear: Nose/Tail Landing Gear Attach Section. Issued Aug 11, 2010
- [SAIB NM-10-12](https://openairdocs.org/saib/NM-10-12): Navigation: Flight Management System. Issued Jan 7, 2010

## NTSB investigations

None matched to N372QS.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20220910009389I](https://openairdocs.org/incident/20220910009389I), Sep 10, 2022: Cessna 680 (N372QS), Las Vegas, NV, Minor damage. [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…
- [Incident 20080730856309I](https://openairdocs.org/incident/20080730856309I), Jul 30, 2008: Cessna 680CE (N372QS), Charleston, SC, Minor damage. During 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…

## Service difficulty reports (28)

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

- [SDR DXTA2026060808336](https://openairdocs.org/sdr/DXTA2026060808336), Jun 4, 2026: TRIM SYSTEM. INOPERATIVE. ON 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 P
- [SDR DXTA2025120205930](https://openairdocs.org/sdr/DXTA2025120205930), Dec 1, 2025: BRAKE SYS. MALFUNCTIONED. AFTER 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 W
- [SDR DXTA2025111005614](https://openairdocs.org/sdr/DXTA2025111005614), Nov 7, 2025: CABLE. OUT OF ADJUST. MAIN 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. CABL
- [SDR 2025F00219](https://openairdocs.org/sdr/2025F00219), Sep 11, 2025: SKIN. GOUGED. MECHANICALLY BLENDED HIGH SPOTS ON A GOUGE ON THE RH WING LEADING EDGE APPROXIMATELY 3.25 INCHES OTBD OF THE START OF THE LEADING EDGE. POLISHED AND RETURNED AR
- [SDR DXTA2025082904755](https://openairdocs.org/sdr/DXTA2025082904755), Aug 28, 2025: PUSHROD. OUT OF ADJUST. UPON OPENING DOOR WE HEARD A LOUD GRINDING/BINDING NOISE ON DOOR DOWNWARD DESCENT, DOOR IS DIFFICULT TO LOCK DOWN AND REQUIRES EXCESSIVE FORCE TO LIFT HANDLE OV
- [SDR DXTA2025080104399](https://openairdocs.org/sdr/DXTA2025080104399), Jul 29, 2025: THROTTLE. UNKNOWN. WHILE IN A DESCENT FROM FL 410 TO FL 340 ZERO, WITH THE THRUST LEVERS AT IDLE, THERE WAS A VIBRATION FROM THE RIGHT ENGINE AND THE ENGINE SHUTDOWN R CYAN MESSAG
- [SDR DXTA2025060203674](https://openairdocs.org/sdr/DXTA2025060203674), May 28, 2025: COMPRESSOR. STALLED. REPEAT WRITE UP. BEGAN DESCENT FROM 43,000FT. THROTTLE WAS AT OR NEAR IDLE. AT 43,000FT WE FELT A COMPRESSOR STALL WHILE OBSERVING A RIGHT ENGINE ROLL BACK FOLL
- [SDR DXTA2025050203276](https://openairdocs.org/sdr/DXTA2025050203276), Apr 29, 2025: CONTROL VALVE. FAULTED. RIGHT ENGINE ENGINE COMPRESSOR STALL: AT APPROX. 42000FT IN THE DECENT, A COMPRESSOR STALL WAS FELT FOR ABOUT 5-10 SECONDS, AIRCRAFT VIBRATION WAS FELT AND LOUD
- [SDR DXTA2025010901874](https://openairdocs.org/sdr/DXTA2025010901874), Jan 7, 2025: HANDLE. DETACHED. MAIN ENTRY DOOR INTERIOR GRAB HANDLE CAME OFF WHILE CLOSING DOOR. ATTACHING HARDWARE IS BROKEN OFF ALONG WITH PART OF THE STEP STRUCTURE AND IS INSIDE THE DOOR 
- [SDR JGVR20230416001](https://openairdocs.org/sdr/JGVR20230416001), Apr 16, 2024: SPAR CAP. CORRODED. R&R FASTENERS, BLENDED CORRODED AREAS OF THE AFT WING SPAR LOWER CAP LOCATED IN THE LH MAIN LANDING GEAR WHEEL WELL, PERFORMED NDT, REPORTED FOR RESULTS REPAIR 
- [SDR DXTA2024010810555](https://openairdocs.org/sdr/DXTA2024010810555), Jan 8, 2024: UNKNOWN. UNKNOWN. THE MAIN CABIN DOOR HAND RAIL REQUIRES EXCESSIVE FORCE TO LOCK THE STEPS IN PLACE. ONCE LOCKED IN PLACE, HAND RAIL AGAIN NEEDS EXCESSIVE FORCE TO BE ABLE TO RAI
- [SDR DXTA2022091270120](https://openairdocs.org/sdr/DXTA2022091270120), Sep 10, 2023: UNKNOWN. UNKNOWN. UPON TAKE OFF, RETRACTED MLG, ALL 3 RETRACTED, THE MLG UNLOCK LIGHT DID NOT EXTINGUSH. COMPELETED UNLOCK QRH CHECKLIST, NLG DID NOT EXTEND. COMPLETED MLG WILL N
- [SDR DXTA2022071165740](https://openairdocs.org/sdr/DXTA2022071165740), Jul 11, 2022: LINE. LEAKING. A FEW SECONDS AFTER ROTATION AND LANDING GEAR RETRACTION WE RECEIVED A ?HYDRAULIC VOLUME LOW? AND ?HYDRAULIC PRESSURE LOW L-R? AMBER EICAS MESSAGES AND A RED LA
- [SDR DXTA2021100549950](https://openairdocs.org/sdr/DXTA2021100549950), Oct 4, 2021: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: CABIN INTERIOR EMERGENCY LIGHT OVER WORK TABLE DOES NOT ILLUMINATE DURING EMERGENCY LIGHT CHECK. THE LIGHT DOES ILLUMINATE WITH MAIN DC POWER
- [SDR DXTA2021072945990](https://openairdocs.org/sdr/DXTA2021072945990), Jul 28, 2021: SPRING. LOW TENSION. MAIN CABIN DOOR NOT PROPERLY COUNTER WEIGHTED. DOOR FALLS ALL THE WAY OPEN WHEN NOT COMPLETELY CLOSED. DOOR IS HARD TO BRING UP TO CLOSE FROM INSIDE CABIN. // S
- [SDR DXTA2021070644610](https://openairdocs.org/sdr/DXTA2021070644610), Jul 2, 2021: COUNTERWEIGHT. OUT OF ADJUST. MAIN DOOR: MAIN CABIN DOOR COUNTERWEIGHT NEEDS ADJUSTMENT. DOOR WILL NOT STAY CRACKED AND FALLS 1 QUARTER TRAVEL. PREFORMED OPS CHECK WITH NO DEFECTS NOTED AND 
- [SDR JGVR20210212002](https://openairdocs.org/sdr/JGVR20210212002), Feb 12, 2021: SPAR. CORRODED. 4 AREAS OF VERIFIED CORROSION ON LH AFT SPAR IN MLG WELL. BLENDED 4 AREA OF CORROSION IN LH GEAR WELL, AFT LOWER SPAR. NDT VERIFIED CORROSION REMOVAL AND REMAIN
- [SDR JGVR202102001](https://openairdocs.org/sdr/JGVR202102001), Feb 12, 2021: SPAR. CORRODED. 7 AREAS OF VERIFIED CORROSION ON RH AFT SPAR IN MLG WELL. BLENDED 7 AREA OF CORROSION IN RH GEAR WELL, AFT LOWER SPAR. NDT VERIFIED CORROSION REMOVAL AND REMAIN
- [SDR DXTA2020111504356](https://openairdocs.org/sdr/DXTA2020111504356), Nov 15, 2020: CHARGER. FAILED. EMERGENCY LIGHTING CONSISTING OF AFT OVER WING LIGHT, EXIT SIGN ON BULKHEAD SEAT NINE, EXIT SIGN OVERLAP, SEAT LAV OVERHEAD LIGHT ALL INOPERABLE WITH THE EMERGE
- [SDR EBVR20200915001](https://openairdocs.org/sdr/EBVR20200915001), Sep 15, 2020: STRUCTURE. CORRODED. FOUND DURING CABIN INTERNAL ZONAL INSPECTION, FOUND SEVERAL SPOTS OF CORROSION ON STRUCTURE UNDER THE CENTER DROP AISLE PANELS. PERFORMED AQRD REPAIR ERO-966932
- [SDR JGVR20190829001](https://openairdocs.org/sdr/JGVR20190829001), Aug 29, 2019: CONTROL VALVE. LOOSE. CABIN AND COCKPIT TEMPERATURE CONTROL VALVE INTERNAL AND EXTERNAL COMPONENTS ARE VERY LOOSE AND MOVING DURING VALVE OPERATION. FOUND WHILE PERFORMING TASK 21-61
- [SDR DXTA2019050702358](https://openairdocs.org/sdr/DXTA2019050702358), May 6, 2019: POWER SUPPLY. MALFUNCTIONED. MAU 1 FAIL AMBER CAS ILLUMINATED - MAU 1 FAIL AMBER CAS MESSAGE ILLUMINATED IN FLIGHT A FL400 DURING CRUISE. ****CORRECTIVE ACTION**** REPLACED POWER SUPPLY MOD
- [SDR JGVR201609220001](https://openairdocs.org/sdr/JGVR201609220001), Sep 22, 2016: HINGE. CORRODED. CORROSION DISCOVERED ON AFT BAGGAGE DOOR HINGES. REMOVED CORROSION VIA MECHANICAL MEANS. RECOMMEND REDUCING THE INSPECTION INTERVAL OR USING AN IMPROVED PRIMER 
- [SDR DXTA2010031504031](https://openairdocs.org/sdr/DXTA2010031504031), Mar 13, 2010: BRAKE ASSY. WEAK. BRAKES WEAKER THAN NORMAL AT HIGH SPEEDS. SEEMS MAX BRAKING NOT AVAILBLE WHEN APPLYING MAX BRAKE PEDAL PRESSURE. BRAKING ACTION NORMAL AT TAXI SPEEDS. INSPECTED
- [SDR DXTA2009010303457](https://openairdocs.org/sdr/DXTA2009010303457), Jan 3, 2009: SEAL. WORN. AFTER DEPARTURE GEAR HANDLE PLACED IN UP POSITION. NOSE GEAR RETRACTED NORMALLY " LIGHT OUT ". UNLOCK RED LIGHT REMAINED ILLUMINATED AS MAIN LT AND RT GEAR CYCL
- [SDR DXTA2009010503457](https://openairdocs.org/sdr/DXTA2009010503457), Jan 3, 2009: LANDING GEAR. MALFUNCTIONED. GEAR HANDLE PLACED IN UP POSITION, MAIN LT AND RT GEAR CYCLED UP AND DOWN APPRX 3 TIMES.
- [SDR DXTA2008121503403](https://openairdocs.org/sdr/DXTA2008121503403), Dec 15, 2008: AUTOPILOT SYS. UNKNOWN. AFTER DEPARTING, THE AP FAIL B MESSAGE FLICKERED THEN ILLUMINATED SOLID. TROUBLESHOT AUTOPILOT SYS USING DIAGNOSTIC MX SYS. NO FAULTS FOUND SYSTEM CHECKS GOOD I
- [SDR DXTA2008121603403](https://openairdocs.org/sdr/DXTA2008121603403), Dec 15, 2008: AUTOPILOT SYS. MALFUNCTIONED. AFTER DEPARTING CMH THE AP FAIL B MSG FLICKERED THEN ILLUMINATED SOLID.

## Service difficulty 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 DXTA200701875](https://openairdocs.org/sdr/DXTA200701875), Jan 23, 2007: UPLOCK SWITCH. MALFUNCTIONED. RT 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
- [SDR DXTA200601781](https://openairdocs.org/sdr/DXTA200601781), Dec 6, 2006: THROTTLE. OUT OF RIG. LT 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 
- [SDR DXTA200601398](https://openairdocs.org/sdr/DXTA200601398), May 18, 2006: FCU. OUT OF ADJUST. LT ENGINE WOULD NOT MAKE TAKEOFF POWER SHORTLY AFTER LIFTOFF. DURING SPEED BRAKE CHECK, ENGINE SHUT DOWN WHEN THROTTLE PULLED BACK TO IDLE. PERFORMED ENGINE BLE
- [SDR DXTA200601327](https://openairdocs.org/sdr/DXTA200601327), Apr 1, 2006: WARNING MESSAGE. UNKNOWN. WHILE ON APPROACH TO LAND NOTICED TWO ANNUNCIATORS, POWER BRAKE LOW PRES AND ANTI SKID INOP. BRAKE FAILURE. RAN CHECKLIST AND LANDED WITHOUT BRAKES. ON POST FLI
- [SDR DXTA200601212](https://openairdocs.org/sdr/DXTA200601212), Jan 24, 2006: FAN. FAILED. SMOKE IN COCKPIT FROM RT EYEBALL VENT. TURNED OFF DEFOG FAN PER CHECKLIST, SMOKE DISSIPATED. REPLACED CABIN DEFOG BLOWER WITH OVERHAULED P/N 5703-4, S/N 0809 IN
- [SDR DXTA200601205](https://openairdocs.org/sdr/DXTA200601205), Jan 18, 2006: FUEL CONTROL. OUT OF RIG. NR 1 ENGINE FLAMEOUT AFTER START, REPEATED START AND AGAIN FLAMEOUT AFTER ABOUT 1 MIN. RAN ENGINE FOUND NR 1 ENGINE FAILED SLAM CHECK, RE-RIGGED FUEL CONTROL ON
- [SDR DXTA200501072](https://openairdocs.org/sdr/DXTA200501072), Nov 10, 2005: ENGINE. SHUTDOWN. LEFT ENGINE SHUTS DOWN WHEN THROTTLE MOVED FROM CRUISE TO IDLE SETTING. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200501063](https://openairdocs.org/sdr/DXTA200501063), Nov 5, 2005: MODULE. BURNED. POWERED UP AIRCRAFT FOR PREFLIGHT. FMS SCREEN STAYS BLACK AND SMOKE WAS COMING OUT FROM UNDER FMS. FOUND FMS GNS-XL. CONTACTED EMPIRE. REMOVED AND REPLACED GNS-
- [SDR DXTA200500526](https://openairdocs.org/sdr/DXTA200500526), Jan 10, 2005: FIRE LOOP. CHAFED. LEFT FIRE WARNING LIGHT ILLUMINATED ON TAXI IN. INSPECTED COCKPIT INDICATION LIGHTS AND COULD NOT FIND ANY FAULTS. INSPECTED L/H ENGINE FIRE LOOP & FOUND 2 CLAM
- [SDR DXTA200400443](https://openairdocs.org/sdr/DXTA200400443), Nov 10, 2004: OIL FILTER. MALFUNCTIONED. LEFT ENGINE EXCEEDED 95LB OIL PRESSURE WHEN COMPUTED TAKEOFF POWER SET ON TAKEOFF. REMOVED OIL FILTER AND INSTALLED NEW OIL FILTER. PERFORMED OPERATIONAL CHECK,
- [SDR CWQ2004F00011](https://openairdocs.org/sdr/CWQ2004F00011), Nov 7, 2003: BOLT. BROKEN. DURING PHASE 1-4 INSP, FOUND RT FLAP ACTUATOR TO HAVE THE CYLINDER TO ATTACH BASE BOLT HEAD SHEARED OFF. THE HEAD OF THE BOLT WAS STILL ATTACHED TO THE SAFTEY W
- [SDR DXTA200300066](https://openairdocs.org/sdr/DXTA200300066), Jul 14, 2003: BULB. INOPERATIVE. RT MAIN LANDING GEAR INDICATOR LIGHT IS INOPERATIVE, BLEW THE GEAR DOWN PER THE CHECKLIST. THREE GREEN LIGHTS NOW APPEAR ON AND TEST CORRECTLY AFTER LANDING. - 
- [SDR 20001205SH008](https://openairdocs.org/sdr/20001205SH008), Nov 16, 2000: SKIN. CORRODED. UPON INSPECTION OF RIGHT WING DE-ICE BOOT, DETERMINED THE AERODYNAMIC FILLER UNDER THE BOOT HAD DEBONDED FROM THE LEADING EDGE. AFTER REMOVAL OF THE DE-ICE BOOT

## STCs that may be installed (OpenAirDocs) (50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Cessna 680)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST12344IB](https://openairdocs.org/stc/ST12344IB): Replacement of the Halon Type 1211 portable fire extinguisher with Halotron BrX portable fire extinguisher with Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST12082WI](https://openairdocs.org/stc/ST12082WI): Upgrade of AirCell High Speed Internet System to Gogo Business Aviation C1 System. Duncan Aviation Inc
- [STC ST11984SE](https://openairdocs.org/stc/ST11984SE): Installation of Starlink Aviation System. AeroMech Incorporated
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST01141DE](https://openairdocs.org/stc/ST01141DE): Installation of the LifePort Medical Interior. LifePort LLC
- [STC ST04736NY](https://openairdocs.org/stc/ST04736NY): True Blue TS28 Emergency Battery Power Supply Replacement. Aerospace Design and Compliance LLC
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST04477CH](https://openairdocs.org/stc/ST04477CH): Installation of a Honeywell RDR-7000 Weather Radar System in accordance with AeroTec STC Master Data List, Doc. # ATEC-077-241-1200, Revision F, dated June 4. 2021, or later FAA-approved revisions. AeroTEC Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04573NY](https://openairdocs.org/stc/ST04573NY): AVIATOR 300 Installation. Amtech Aeronautical Limited
- [STC ST01941WI](https://openairdocs.org/stc/ST01941WI): Installation of Gogo Business Aviation AVANCE L5 Broadband System. Duncan Aviation Inc
- [STC ST01403WI-D](https://openairdocs.org/stc/ST01403WI-D): Installation of alternate part number DU-1080 Display Unit. Honeywell International Inc
- [STC ST01410WI-D](https://openairdocs.org/stc/ST01410WI-D): Installation of alternate part number NI-900 Network Interface Module. Honeywell International Inc
- [STC ST01440WI-D](https://openairdocs.org/stc/ST01440WI-D): Installation of alternate part number EPIC MC-850-2 Multi-Function Control Display Unit. Honeywell International Inc
- [STC ST01448WI-D](https://openairdocs.org/stc/ST01448WI-D): Installation of EPIC Phase 4.1 Software. Honeywell International Inc
- [STC ST01482WI-D](https://openairdocs.org/stc/ST01482WI-D): Installation of EPIC Phase 4.2 Software, alternate part number AGM-200 AFGS and alternate part number TR-865B CMF VDR. Honeywell International Inc
- [STC ST01530WI-D](https://openairdocs.org/stc/ST01530WI-D): Installation of EPIC NIC/PROC, AIOP, AND CMC modules and Pentium M software. Honeywell International Inc
- [STC ST01027DE](https://openairdocs.org/stc/ST01027DE): Installation of MarathonNorco Aerospace Inc Nickel Cadmium battery in place of existing Nickel Cadmium main aircraft battery/batteries. MarathonNorco Aerospace Inc
- [STC ST01859WI](https://openairdocs.org/stc/ST01859WI): Installation of Gogo Business Aviation's Gogo Biz 4G Air-to-Ground System. Textron Aviation Inc Wichita Citation Service Center
- [STC ST01840WI](https://openairdocs.org/stc/ST01840WI): Installation of winglets, wing structural reinforcement, and related system changes. Winglet Technology LLC
- [STC ST00934DE](https://openairdocs.org/stc/ST00934DE): Installation of Becker Avionics BXT6553 transponder. Peregrine
- [STC ST02240LA-D](https://openairdocs.org/stc/ST02240LA-D): Installation of a Patient Loading and Utility System (PLUS). LifePort LLC
- [STC ST02286LA](https://openairdocs.org/stc/ST02286LA): Installation of a Patient Loading and Utility System (PLUS). LifePort LLC
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST00347BO](https://openairdocs.org/stc/ST00347BO): Modification to upgrade a BendixKing CAS 67A TCAS II system to CAS 67B TCAS II Change 7.1. Pro Star Aviation, LLC
- [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc
- [STC ST04366AT](https://openairdocs.org/stc/ST04366AT): This STC is a replacement of the original equipment nickel cadmium main batteries manufactured by Saft or Marathon with Concorde valve regulated lead acid main batteries. Concorde Battery Corporation
- [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS
- [STC ST01399WI](https://openairdocs.org/stc/ST01399WI): Installation of Honeywell DL-950 Data Loader. Textron Aviation Inc
- [STC ST02127LA](https://openairdocs.org/stc/ST02127LA): Installation of a Crane Aerospace & Electronics Tire Sensor Assembly. ELDEC Corporation
- [STC ST00717DE](https://openairdocs.org/stc/ST00717DE): Installation of a camera portal as a provision to accommodate a future camera. Sierra Nevada Corporation
- [STC ST01655WI-D](https://openairdocs.org/stc/ST01655WI-D): Installation of a Tenfine Chinese Flight Inspection System. Duncan Aviation Inc
- [STC ST00715DE-D](https://openairdocs.org/stc/ST00715DE-D): Installation of Nose Boom Provisions, Pylons and Antennas. Sierra Nevada Corporation
- [STC ST00718DE](https://openairdocs.org/stc/ST00718DE): Interior installation of, operator seats, equipment racks, power distribution panel, signal junction boxes, inoperative cockpit video display, cabin Inter-Communication System (ICS), ballast boxes and provisions to mount antennas, and baggage compartment installation of, power inverters, alternating current/direct current junction boxes, and a lead-acid mission battery in accordance with Sierra Nevada Corporation Drawing List, Report No. MDL- 0142-25-9309 Revision A, dated June 15, 2011, FAA approved July 25, 2011, or later FAA approved revision. Sierra Nevada Corporation
- [STC ST00720DE](https://openairdocs.org/stc/ST00720DE): Installation of sensors and provisions for future capability to monitor aircraft control surface deflections, existing pilot control input signals, and other aircraft systems in accordance with Sierra Nevada Corporation Drawing List, Report Number MDL-0142-25-9315, Revision B, dated February 24, 2011, FAA approved July 25, 2011, or later FAA approved revision. Sierra Nevada Corporation
- [STC ST00719DE](https://openairdocs.org/stc/ST00719DE): Installation of structural fittings in the wing as provisions to accommodate future external stores in accordance with Sierra Nevada Corporation Drawing List, Report No MDL-0142-25-9316, Revision A, dated February 15, 2011, FAA approved March 29, 2011, or later FAA approved revision. Sierra Nevada Corporation
- [STC ST01608WI-D](https://openairdocs.org/stc/ST01608WI-D): Installation of Aircell High Speed Internet System with Wireless LAN System. Duncan Aviation Inc
- [STC ST02240LA](https://openairdocs.org/stc/ST02240LA): Installation of a Patient Loading and Utility System (PLUS). Lifeport, Inc
- [STC ST02146NY](https://openairdocs.org/stc/ST02146NY): Installation of EMS Technologies Ltd. Cabin Network Xcelerator (CNX). EMS Technologies Canada Ltd
- [STC ST02248NY](https://openairdocs.org/stc/ST02248NY): Installation of EMS HSD-64, HSD-128, HSD-HCM, and HSD-X. EMS Technologies Canada Ltd
- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc
- [STC ST00263BO](https://openairdocs.org/stc/ST00263BO): Installation of Pratt & Whitney Engine Services, Inc. Data Transmission Unit (DTU). Pratt & Whitney Engine Services Inc
- [STC ST02893AT](https://openairdocs.org/stc/ST02893AT): Installation of a Boom Beam Taxi/Landing Light System. Whelen Aerospace Technologies

## Related

- Other Cessna 680 aircraft: https://openairdocs.org/model/cessna-680/aircraft.md
- The Pratt & Whitney Canada PW306C engine: https://openairdocs.org/engine/pratt-whitney-canada-pw306c.md

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