# N341QS: Cessna 680

- Status: Valid registration
- Airframe: [Cessna 680](https://openairdocs.org/model/cessna-680) (registry code 2076811, 9 seats)
- Data sheets: [TCDS T00012WI](https://openairdocs.org/tcds/T00012WI) (Textron Aviation Inc.) (OpenAirDocs)
- Serial number: 680-0225
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: August 25, 2020
- Expires: August 31, 2027
- Mode S code: A3C274
- Owner type: Corporation
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=341QS
- Page: https://openairdocs.org/aircraft/N341QS

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

## 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 N341QS.

## 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 20260302001059I](https://openairdocs.org/incident/20260302001059I), Mar 2, 2026: Cessna 680 (N341QS), Broomfield, CO, Minor damage. Bird strike with dent on the left-wing outer edge near the red nav lights.
- [Incident 20120810019479I](https://openairdocs.org/incident/20120810019479I), Aug 10, 2012: Cessna 680 (N341QS), Newburg, NY, Substantial damage. Aircraft took off from greensboro, NC (kgso) and was enroute to bridgeport, CT (kbdr) when it diverted into Newburg, NY (kswf) due to a vibration from an…

## Service difficulty reports (59, newest 50)

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 DXTA2026010506406](https://openairdocs.org/sdr/DXTA2026010506406), Jan 2, 2026: WING. GROUND DAMAGE. JUST AS WE GOT TO THE AIRPORT AND BEFORE WE GOT TO THE PLANE A EXECUJET VAN STRUCK THE LEFT WING OF N341QS AT 8:56. THE DAMAGE TO THE WING SEEMS MINIMAL BUT THE
- [SDR DXTA2025120806024](https://openairdocs.org/sdr/DXTA2025120806024), Dec 7, 2025: POWER SUPPLY. INOPERATIVE. DURING PREFLIGHT FOUND ALL BUT TWO EMERGENCY LIGHTS INOPERATIVE. THE ONLY TWO THAT WORK ARE THE CABIN FLOOR FWD LT & EXTERIOR LIGHT BY THE CABIN DOOR. REMOVED N
- [SDR 2025FA0000724](https://openairdocs.org/sdr/2025FA0000724), Oct 18, 2025: SPAR CAP. CORRODED. CORROSION FOUND IN RT WHEEL WELL ON LOWER AFT SPAR CAP. ACCOMPLISHED FORM 8100-9, FIELD REPAIR FR-680-0225-15874 FIELD REPAIR-CORROSION, RT WING REAR SPAR CAP L
- [SDR DXTA2025051403445](https://openairdocs.org/sdr/DXTA2025051403445), May 11, 2025: DOOR. MALFUNCTIONED. PRIMARY CABIN DOOR WOULD NOT OPEN AFTER LANDING. RED BUTTON WOULD NOT DEPRESS TO OPEN THE DOOR. ATTEMPTED TO HAVE GROUND CREW OPEN THE DOOR FROM THE OUTSIDE. TH
- [SDR DXTA2025041403069](https://openairdocs.org/sdr/DXTA2025041403069), Apr 12, 2025: CABIN PRESSURE. MALFUNCTIONED. OVERWEIGHT LANDING: LANDED AT APPROXIMATELY 28,100 POUNDS DUE TO PRESSURIZATION EMERGENCY WITH PASSENGERS. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING INSPECTION 
- [SDR DXTA2025041403068](https://openairdocs.org/sdr/DXTA2025041403068), Apr 12, 2025: COUPLING. OUT OF POSITION. CABIN PRESSURIZATION CONTROL: DURING CLIMBOUT, WE NOTICED A FLUTTERING/POPPING NOISE FROM ABOUT 1000 MSL TO ABOUT 2000 MSL. IT STOPPED. THEN WE NOTICED THAT THE
- [SDR DXTA2025040102859](https://openairdocs.org/sdr/DXTA2025040102859), Mar 29, 2025: CONTROL VALVE. LEAKING. AFTER A NORMAL LANDING IN HOU, A LINEMAN NOTICED OUR RIGHT MLG TRUCK SMOKING WITH A VERY DISTINCT CRACKLING SOUND (ALMOST THE SOUND OF A WOOD LOG BURNING IN A F
- [SDR 2025FA0000214](https://openairdocs.org/sdr/2025FA0000214), Mar 27, 2025: SPAR. CORRODED. DURING WING AFT SPAR INSPECTION, FOUND CORROSION AROUND HYDRAULIC FITTINGS ON LH AFT SPAR. DURING BLENDING OF LH WING SPAR FOUND CORROSION UNDER ADDITIONAL FEED
- [SDR 2025FA0000213](https://openairdocs.org/sdr/2025FA0000213), Mar 27, 2025: SPAR. CORRODED. DURING LH AND RH WING AFT SPAR INSPECTION FOUND CORROSION AROUND SPEED BRAKE HYDRAULIC FITTING AND SP HYDRAULIC FITTING ON RH WING. PERFORMED REPAIR TO RH WING 
- [SDR 2025FA0000183](https://openairdocs.org/sdr/2025FA0000183), Mar 13, 2025: SPAR WEB. CORRODED. LH WING AFT SPAR WEB CORROSION.
- [SDR 2025FA0000182](https://openairdocs.org/sdr/2025FA0000182), Mar 13, 2025: CLOSEOUT PANEL. CORRODED. MED LOWER CLOSEOUT PANEL CORROSION AND GOUGING.
- [SDR 2025FA0000120](https://openairdocs.org/sdr/2025FA0000120), Feb 19, 2025: TAIL CONE. CORRODED. TAIL CONE HAS CORROSION SURROUNDING LOWER DATA PLATE.
- [SDR DXTA2024110401000](https://openairdocs.org/sdr/DXTA2024110401000), Oct 30, 2024: SHROUD. DAMAGED. ON TAKEOFF CLIMB OUT, APPROXIMATELY 500 FEET AGL A TURKEY VULTURE IMPACTED THE FRONT LEFT WINDSHIELD CRUSHING THE WINDSHIELD AIR VENT DUCTING. NO STRUCTURAL DAM
- [SDR DXTA2024040211373](https://openairdocs.org/sdr/DXTA2024040211373), Mar 31, 2024: CABLE. LOW TENSION. MAIN DOOR: MAIN CABIN DOOR NOT BALANCED AND OPENS VERY VIOLENTLY. VERY HEAVY/DIFFICULT TO CLOSE. TECH PERFORMED THE COUNTERBALANCE ADJUSTMENT/TECH AND FOUND THE
- [SDR DXTA2024030811126](https://openairdocs.org/sdr/DXTA2024030811126), Mar 6, 2024: SPRING. FAULTY. MAIN DOOR CABLE IS LOOSE INSIDE DOOR. CABLE IS ATTACHED, BUT SLACK. INSPECTED CABIN DOOR AND FOUND AFT DOOR COUNTERBALANCE SPRING BROKEN. REMOVED AND REPLACED C
- [SDR DXTA2024022811004](https://openairdocs.org/sdr/DXTA2024022811004), Feb 25, 2024: SPRING. DAMAGED. MAIN DOOR CABLE: LEFT SIDE MAIN CABIN DOOR COUNTER BALANCE CABLE WILL NOT RETRACT AND UNABLE CLOSE DOOR FROM INSIDE THE AIRCRAFT. REMOVED MAIN ENTRY DOOR STAIRS
- [SDR DXTA2023113010191](https://openairdocs.org/sdr/DXTA2023113010191), Nov 30, 2023: HINGE. DAMAGED. OPENING THE MAIN CABIN DOOR, AFTER LANDING, BITS OF THE MAIN HINGE BROKE OFF. TECHS WERE UNABLE TO REMOVE THE DAMAGED HINGE HALF AS THE HINGE PIN IS FULLY SEIZE
- [SDR 2023FA0000698](https://openairdocs.org/sdr/2023FA0000698), Oct 29, 2023: SPAR CAP. CORRODED. FIELD REPAIR - CORROSION, VERTICAL STABILIZER, AFT SPAR CAP VFS 174.85 - VFS 238.39. REPORT NO. FR-680-0225-12507 DATED OCTOBER 12, 2023 WITH FAA FORM 8100-9.
- [SDR DXTA2023062689410](https://openairdocs.org/sdr/DXTA2023062689410), Jun 26, 2023: UNKNOWN. UNKNOWN. AC GENERATION AND CONTROL: SLIGHT ELECTRICAL SMOKE ODOR BEFORE TAKEOFF , FADED WHEN FACING DOWN RUNWAY. DURING TROUBLESHOOTING OF THE RH WINDSHIELD HEAT INOP CA
- [SDR DXTA2023060587810](https://openairdocs.org/sdr/DXTA2023060587810), Jun 5, 2023: UNKNOWN. UNKNOWN. EMER LIGHTS FAIL PREFLIGHT CHECK. WITH BATTERIES OFF AND EMERGENCY LIGHT SWITCH IN ARM, ZERO EMERGENCY LIGHTS TURN ON. WITH THE EMERGENCY LIGHT SWITCH ON, ALL E
- [SDR DXTA2023052486950](https://openairdocs.org/sdr/DXTA2023052486950), May 23, 2023: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: OVERHEAD CABIN EMERGENCY LIGHTS ON LEFT SIDE, AND MAIN CABIN DOOR EXTERIOR EMERGENCY LIGHT DO NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. VER
- [SDR DXTA2023051285940](https://openairdocs.org/sdr/DXTA2023051285940), May 11, 2023: UNKNOWN. UNKNOWN. EMERGENCY LIGHTING: WITH THE EMERGENCY LIGHTS IN THE ON POSITION OR THE PAX, SAFETY LIGHT SWITCH ON ALL INTERIOR EMERGENCY SIGNS AND PAX SAFETY LIGHTS FORWARD O
- [SDR DXTA2022111573970](https://openairdocs.org/sdr/DXTA2022111573970), Nov 14, 2022: G SWITCH. TRIPPED. EMERGENCY LIGHTING: CABIN EMER LIGHTS ASSOCIATED WITH BATTERY PACK ONE FOR FORWARD PORTION OF CABIN, ILLUMINATED ON THEIR OWN DURING CRUISE. LIGHTS STAYED ON RE
- [SDR DXTA2022102672790](https://openairdocs.org/sdr/DXTA2022102672790), Oct 25, 2022: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTING: CABIN, EXTERIOR, AND LAV EMERGENCY LIGHTS FAIL TO ILLUMINATE DURING PREFLIGHT CHECKS. PERFORMED EMERGENCY LIGHTING POWER SUPPLY BATTERY EXER
- [SDR DXTA2021071345190](https://openairdocs.org/sdr/DXTA2021071345190), Jul 12, 2021: APU. SMOKE. SMOKE AND AND ODOR IN THE CABIN. APU AND BLEED AIR WERE ON, ENGINES OFF. INSPECTED THE APU EXHAUST FINDING NO OIL OR VISUAL ABNORMALITIES. STARTED THE APU IAW T
- [SDR DXTA2021032439900](https://openairdocs.org/sdr/DXTA2021032439900), Mar 23, 2021: WARNING MESSAGE. FALSE ACTIVATION. MAIN DOOR: AMBER CABIN DOOR OPEN CAS MESSAGE WILL NOT CLEAR. WE HAD PLANE PLANE GO DARK. WE OPENED AND CLOSED DOOR 6X TIMES IN A ROW TO RESET, NO LUCK PERFORMED
- [SDR EBVR20200807001](https://openairdocs.org/sdr/EBVR20200807001), Aug 7, 2020: STRUCTURE. CORRODED. CORROSION FOUND AROUND THREE LOCK FASTENERS IN CENTER AFT CABIN FLOOR JUST FWD OF OUTFLOW VALVES, FOUND SEVERAL SPOTS OF CORROSION ON STRUCTURE UNDER THE CENTER
- [SDR DXTA2019031302157](https://openairdocs.org/sdr/DXTA2019031302157), Mar 13, 2019: PRINTED CKT BOARD. FAULTY. ALL LANDING GEAR RETRACTION DID NOT RETRACT-GEAR WOULDNT RETRACT AFTER TAKEOFF. AMBER CAS WOW MIS-COMPARE CAME ON SHORTLY AFTER. **SUPPLEMENTAL INFORMATION - RE
- [SDR DXTA2018071800266](https://openairdocs.org/sdr/DXTA2018071800266), Jul 18, 2018: SPAR CAP. CORRODED. VERTICAL STAB AFT SPAR CAP DAMAGE, CORROSION.
- [SDR DXTA2018053001017](https://openairdocs.org/sdr/DXTA2018053001017), May 30, 2018: UNKNOWN. ODOR. BURNING SMELL IN COCKPIT.
- [SDR 2017F00002](https://openairdocs.org/sdr/2017F00002), Jan 10, 2017: SKIN. DAMAGED. REPAIR OF AFT CABIN LIGHTNING STRIKE DAMAGE, S-680-0225/10RD REV-. DATED DECEMBER 20, 2016 WITH FAA FORM 8100-9.
- [SDR 2017F00001](https://openairdocs.org/sdr/2017F00001), Jan 5, 2017: SKIN. DAMAGED. REPAIR OF AFT CABIN LIGHTNING STRIKE DAMAGE.
- [SDR DXTA2016020206174](https://openairdocs.org/sdr/DXTA2016020206174), Feb 1, 2016: APU. LEAKING. AFTER APU BLEED AIR SELECTED ON, THERE WAS AN ODOR & HAZY SMOKE IN THE COCKPIT & CABIN. WITH ENGS RUNNING & APU BLEED AIR OFF THE ODOR & SMOKE DISSIPATED. REMOV
- [SDR DXTA2015005006014](https://openairdocs.org/sdr/DXTA2015005006014), May 1, 2015: COALESCER BAG. DIRTY. WHEN APU STARTED & BLEED AIR VALVES OPENED, SMOKE BEGAN TO POUR OUT OF VENTS. SMOKE DISSIPATED WHEN APU BLEEDS CLOSED. WHEN ENG STARTED, NO SMOKE WAS OBSERVED. 
- [SDR DXTA2013080505467](https://openairdocs.org/sdr/DXTA2013080505467), Aug 4, 2013: BRAKE. WEAK. CO-PILOT`S LT BRAKE SPONGY. ON LANDING ROLLOUT, BRAKES WERE APPLIED EVENLY AND ACFT VEERED TO RT AND LT PEDAL FELT SPONGY. BLED LT INBD AND OTBD BRAKES IAW MM 3
- [SDR DXTA2013052005397](https://openairdocs.org/sdr/DXTA2013052005397), May 18, 2013: OIL SYSTEM. OVERSERVICED. WITH THE APU ONLY RUNNING, BLEED AIR WAS SELECTED ON. SMOKE IMMEDIATELY STARTED TO POUR INTO BOTH CABIN AND COCKPIT. SHUTDOWN APU WITHIN 15 SECONDS AND A CONSID
- [SDR CWQR20130501032](https://openairdocs.org/sdr/CWQR20130501032), May 1, 2013: NOZZLE. CRACKED. DURING A SCHEDULED INSPECTION OF THE APU COMPARTMENT THE TECH FOUND THE FIRE EXTINGUISHING SYSTEM NOZZLE CRACKED 2.5" AT THE BULKHEAD MOUNTING FLANGE. THIS COND
- [SDR DXTA2013030805309](https://openairdocs.org/sdr/DXTA2013030805309), Mar 7, 2013: SQUAT SWITCH. OUT OF ADJUST. DEPARTED, RECEIVED AN AMBER WOW MISCOMPARE MESSAGE. ON GEAR RETRACTION LANDING GEAR DID NOT RETRACT AND RED UNLOCK LIGHT ILLUMINATED. RETURNED LANDING HANDLE DO
- [SDR DXTA2012112105189](https://openairdocs.org/sdr/DXTA2012112105189), Nov 20, 2012: BULB. INOPERATIVE. LANDING, HAD AN UNSAFE GEAR INDICATION (NO GREEN LIGHT ON LT MAIN) WE HAD GREEN LIGHTS FOR RT MAIN AND NOSE GEAR AND NO RED UNLOCK LIGHT. RAN GEAR WILL NOT EXTE
- [SDR DXTA2012111305182](https://openairdocs.org/sdr/DXTA2012111305182), Nov 12, 2012: COALESCER BAG. ODOR. ON ROTATION THROUGH FIRST POWER REDUCTION ABOUT 2 MINUTES AT HIGH BODY ANGLE, A STRONG OIL BURNING ODOR OCCURRED. WENT AWAY AT THAT TIME. DID NOT HAPPEN ON GROU
- [SDR DXTA2012081305091](https://openairdocs.org/sdr/DXTA2012081305091), Aug 10, 2012: COWLING. BROKEN. 75 PERCENT OF BOTTOM HALF OF RT ENGINE COWLING IS MISSING. PERFORMED AIRCRAFT FOREIGN OBJECT DAMAGE INSPECTION IAW MM 5-50-00. NO FURTHER DAMAGE NOTED. PERFORME
- [SDR DXTA2012081305092](https://openairdocs.org/sdr/DXTA2012081305092), Aug 10, 2012: DOOR. OPEN. ON LT ENGINE, THE THREE SMALL LATCHED ON THE LOWER FRONT OF COWLING WERE FOUND UNLATCHED. ON THE LATCHED ON THE SIDE OF THE COWLING, LATCH 1 (FROM THE FRONT) WA
- [SDR DXTA2012011004843](https://openairdocs.org/sdr/DXTA2012011004843), Jan 10, 2012: FUEL NOZZLE. CLOGGED. AFTER TAKEOFF AT HIGH POWER SETTING AND RELATIVELY LOW AIRSPEED ON CLIMBOUT, A STRONG ODOR OF FUMES CAME INTO COCKPIT AND CABIN FOR ABOUT 10 MINS. THE APU WAS N
- [SDR DXTA2011111404787](https://openairdocs.org/sdr/DXTA2011111404787), Nov 13, 2011: WIRE. CHAFED. IN CRUISE AT FL230 A STRONG ELECTRICAL ODOR WAS DETECTED IN THE FWD CABIN AND COCKPIT. SECURED INTERIOR ELECTRICAL SWITCH AND ODOR DISSIPATED. FOUND THROTTLE QU
- [SDR 2010F00025](https://openairdocs.org/sdr/2010F00025), Feb 4, 2010: WARNING LIGHT. ILLUMINATED. ENGINE CHIP DETECT ILLUMINATED IN FLIGHT, REMAINED ON FOR LAST 20 MINUTES OF FLIGHT.
- [SDR DXTA2009021203501](https://openairdocs.org/sdr/DXTA2009021203501), Feb 11, 2009: SWITCH. INOPERATIVE. AT FL410 FOR 2.5 TO 3 HOURS - AMBER CAS MSG ACM O'TEMP DISPLAYED & WITHIN 5 SEC AMBER EMERGENCY PRESSURIZATION DISPLAYED - PAX SAID SMOKE & FUMES IN CABIN. REQU
- [SDR DXTA200702714](https://openairdocs.org/sdr/DXTA200702714), Dec 25, 2007: ENGINE. POWER LOSS. ON TAKEOFF, UNABLE TO MAKE TAKEOFF, N1OF 95.5 PERCENT UNLESS THE POWER LEVER ON RT ENGINE WAS AT THE FIREWALL STOP. OPS CHECK GOOD ON ENGINE RUN. ALL NUMBERS WI
- [SDR DXTA200702406](https://openairdocs.org/sdr/DXTA200702406), Aug 15, 2007: VALVE. FAILED. BRAKES FAILED ON LANDING. REMOVED AND REPLACED BRAKE BLEED VALVE WITH NEW , PERFORMED FUNCTIONAL CHECKED GOOD. I.A.W. 560 M/M 32-42-04. NO LEAKS NOTED P/N 77B62
- [SDR DXTA200702162](https://openairdocs.org/sdr/DXTA200702162), Apr 29, 2007: ANTI-SKID SYS. MALFUNCTIONED. ANTI-SKID PULSES DURING NORMAL BRAKE USE. RETURNED TO DEPARTURE. [SUP 05-03-07] REMOVED & REPLACED A/S CONTROL BOX IAW CESSNA 560 M/M CHPT 32-42-00.
- [SDR DXTA200702152](https://openairdocs.org/sdr/DXTA200702152), Apr 27, 2007: BRAKE ASSY. WEAK. BRAKES ARE SPONGY AND SLOPPY FEELING DURING LANDING. RT SIDE PULSATED INTERMITTENTLY. [SUP 05-03-07] PERFORMED BRAKE & ANTI-SKID BLEEDING PROCEDURE 3 TIMES ON E

All 59: https://openairdocs.org/aircraft/N341QS/reports.md

## Service difficulty reports on N341QS not matched to an aircraft (2)

They name N341QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR 98ZZZX880](https://openairdocs.org/sdr/98ZZZX880), Feb 10, 1998: LINE ASSY. CHAFE. TWO WING DEICE LINES AND CLAMPS LOCATED AT FUSELAGE AND WING LEADING EDGE, CHAFE FUSELAGE SKIN. SUBMITTER STATED SHRINK WRAP AND THERMOPROTECTION TAPE SHOULD BE
- [SDR 98ZZZX879](https://openairdocs.org/sdr/98ZZZX879), Feb 10, 1998: LINE ASSY. CHAFE. TWO WING DEICE LINES AND CLAMPS LOCATED AT FUSELAGE AND WING LEADING EDGE, CHAFE FUSELAGE SKIN. SUBMITTER STATED SHRINK WRAP AND THERMOPROTECTION TAPE SHOULD BE

## 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

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