# N320QS: 2007 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: 680-0169
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 2, 2007
- Certificate issued: February 12, 2021
- Expires: February 29, 2028
- Mode S code: A36FBF
- Owner type: Corporation
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=320QS
- Page: https://openairdocs.org/aircraft/N320QS

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB WPR09LA036](https://openairdocs.org/ntsb/WPR09LA036), Nov 12, 2008: Cessna 680 (N320QS), Los Angeles, CA, substantial damage. Probable cause: Failure of the ground service vehicle driver to maintain adequate clearance/distance from the taxiing airplane.

## FAA accident and incident reports (1)

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.

- [Accident 20081111851949A](https://openairdocs.org/incident/20081111851949A), Nov 11, 2008: Cessna 680SOV (N320QS), Los Angeles, CA, Substantial damage. (-23) Pilot was cleared to taxi to the landmark aviation ramp and when he turned right to enter the ramp area a truck operated by an employee of abx air, a…

## Service difficulty reports (44)

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 DXTA2026061808462](https://openairdocs.org/sdr/DXTA2026061808462), Jun 15, 2026: BATTERY. FAULTY. SEVERAL OVERHEAD INTERIOR EMERGENCY LIGHTS AND HALF OF THE EXTERIOR EMERGENCY LIGHTS FAILED TO ILLUMINATE DURING PREFLIGHT CHECKS. REPEAT WRITE-UP. REMOVED FAIL
- [SDR JGVR20251117002](https://openairdocs.org/sdr/JGVR20251117002), Nov 17, 2025: SKIN. CORRODED. REPAIRED CORRODED AREAS OF THE INNER SURFACES OF THE BAGGAGE COMPARTMENT SKINS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPA
- [SDR JGVR20251117001](https://openairdocs.org/sdr/JGVR20251117001), Nov 17, 2025: SKIN. CORRODED. MECHANICALLY REMOVED CORROSION LOCATED ON THE LT LOWER WING SKIN AT WS.294 PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED TREATED AND PRIMED REPAIR 
- [SDR JGVR20251113002](https://openairdocs.org/sdr/JGVR20251113002), Nov 13, 2025: SKIN. CORRODED. FOUND CORROSION ON THE UPPER INBOARD WING SKINS LOCATED ALONG AND UNDER THE DRAG ANGLES (FUSELAGE TO WING FARING ATTACH STRUCTURE), REMOVED THE DRAG ANGLES, BLE
- [SDR JGVR20251112002](https://openairdocs.org/sdr/JGVR20251112002), Nov 12, 2025: SKIN. CORRODED. BLENDED CORRODED AREAS LOCATED ON THE NUTPLATE-SIDE OF THE FUSELAGE STRUCTURE WHERE THE SPADE DOOR (MAIN ENTRY DOOR LOWER FAIRING DOOR) ATTACHES TO THE AIRCRAFT
- [SDR JGVR20251112001](https://openairdocs.org/sdr/JGVR20251112001), Nov 12, 2025: SKIN. CORRODED. FOUND 5 AREAS OF CORROSION ON THE UPPER SURFACE OF THE LH UPPER WING SKIN AND 2 AREAS ON THE UPPER SURFACE OF THE RH UPPER WING SKIN, MECHANICALLY BLENDED CORRO
- [SDR JGVR20251111002](https://openairdocs.org/sdr/JGVR20251111002), Nov 11, 2025: TAIL CONE. CORRODED. REPAIRED CORRODED AREA LOWER TAILCONE SKINS AT THE AIRCRAFT DATA PLATE BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING
- [SDR JGVR20251111001](https://openairdocs.org/sdr/JGVR20251111001), Nov 11, 2025: SKIN. CORRODED. REPAIRED CORRODED AREA ON THE LOWER WING SKIN IN THE RH LANDING GEAR WELL, BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTAL
- [SDR JGVR20251110003](https://openairdocs.org/sdr/JGVR20251110003), Nov 10, 2025: SKIN. CORRODED. MECHANICALLY REMOVED CORROSION LOCATED ON RH VERTICAL STABILIZER SKIN, JUST FORWARD OF ACCESS PANEL 341BR PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION, CLE
- [SDR JGVR20251110002](https://openairdocs.org/sdr/JGVR20251110002), Nov 10, 2025: SKIN. CORRODED. BLENDED 7 AREAS OF CORROSION PLUS 1 ADDITIONAL AREA LOCATED ON RH UPPER WING SKIN AT WS 294 TO THE WING TIP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. 
- [SDR JGVR20251110001](https://openairdocs.org/sdr/JGVR20251110001), Nov 10, 2025: SKIN. CORRODED. MECHANICALLY BLENDED 1 AREA OF CORROSION LOCATED ON E-EXIT EXTERIOR SKIN LOCATED ON INNER EDGE PERIMETER OF CONTOUR RINGS, LOWER AREA OF E-EXIT PERFORMED NDT AN
- [SDR JGVR20250910002](https://openairdocs.org/sdr/JGVR20250910002), Sep 10, 2025: SKIN. CORRODED. MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED ON FUSELAGE SKIN AT THE RH NOSE DOOR AFT LATCH AREA, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRE
- [SDR JGVR20250910001](https://openairdocs.org/sdr/JGVR20250910001), Sep 10, 2025: ANGLE. CORRODED. MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED IN LH MLG WHEEL WELL AFT SPAR LOWER CLIP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED CORROSION
- [SDR 2024F00254](https://openairdocs.org/sdr/2024F00254), Oct 17, 2024: FAIRING. DAMAGED. DURING INSPECTION 80 HOLES WERE OVERSIZED DURING HI-LOCK REMOVAL ON THE BELLY FAIRING. 40 OVERSIZED HOLES AT LWS 37 AND 40 OVERSIZED HOLES AT RWS 37. REPAIR WAS
- [SDR 2024FA0000761](https://openairdocs.org/sdr/2024FA0000761), Oct 9, 2024: CASE. GOUGED. N320QS (680-0169) RH ENGINE CASE GOUGE.
- [SDR 2024F00248](https://openairdocs.org/sdr/2024F00248), Oct 9, 2024: DOUBLER. CORRODED. THE LH AND RH WING FUEL PANELS HAVE CORROSION PRESENT IN MULTIPLE AREAS.
- [SDR DXTA2023101397900](https://openairdocs.org/sdr/DXTA2023101397900), Oct 12, 2023: POSITION SWITCH. DAMAGED. DESCENDING THROUGH 7000 FEET THE CABIN DOOR OPEN AMBER MESSAGE ILLUMINATED. UPON LANDING THE SIGHT GAUGES SHOWED THE HASH MARKS THAT'S THE PINS WERE IN PLACE. V
- [SDR JGVR20230901001](https://openairdocs.org/sdr/JGVR20230901001), Sep 1, 2023: UNKNOWN. UNKNOWN. BLENDED TWO AREAS OF CORROSION ON THE UPPER SURFACE OF THE UPPER INBOARD WING SKIN AT THE TRAILING EDGE OF THE LH WING AND TWO ADDITIONAL AREAS ON THE FORWARD E
- [SDR JGVR20230831002](https://openairdocs.org/sdr/JGVR20230831002), Aug 31, 2023: UNKNOWN. UNKNOWN. MECHANICALLY BLENDED CORROSION AROUND RH WING AFT SPAR #8 SPOILER/SPEED BRAKE RETURN AND PRESSURE FITTINGS. R&R THE BULKHEAD FITTINGS FOR ACCESS. PERFORMED NDT,
- [SDR JGVR20230831001](https://openairdocs.org/sdr/JGVR20230831001), Aug 31, 2023: UNKNOWN. UNKNOWN. MECHANICALLY BLENDED CORRODED AREAS OF THE AFT SPAR LOWER CAP AND SPAR FACE LOCATED IN THE LH MAIN LANDING GEAR WHEEL, PERFORMED NDT AND REPORTED RESULTS FOR RE
- [SDR JGVR20230810002](https://openairdocs.org/sdr/JGVR20230810002), Aug 10, 2023: UNKNOWN. UNKNOWN. BLENDED 2 AREAS OF CORROSION ON THE EXTERIOR OF THE FUSELAGE SKIN LOCATED JUST AFT OF THE EMERGENCY EXIT DOOR OPENING, PERFORMED NDT AND REPORTED FOR REPAIR DIS
- [SDR JGVR20230810001](https://openairdocs.org/sdr/JGVR20230810001), Aug 10, 2023: UNKNOWN. UNKNOWN. BLENDED 5 AREAS OF CORROSION ON THE EXTERIOR SKIN OF THE EMERGENCY EXIT DOOR, PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIME
- [SDR DXTA2022100671670](https://openairdocs.org/sdr/DXTA2022100671670), Oct 5, 2022: SPRING. BROKEN. MAIN DOOR CABLE: MAIN DOOR FORWARD CABLE DOES NOT WORK. REMOVED AND REPLACED MAIN CABIN DOOR FWD AND AFT LUBRICATED SPRINGS AND FWD SUPPORT STRUT ASSY WITH A CU
- [SDR DXTA2022050561270](https://openairdocs.org/sdr/DXTA2022050561270), May 4, 2022: SPRING. DAMAGED. MAIN DOOR: UNABLE TO OPEN MAIN CABIN DOOR FROM INSIDE USING NORMAL METHOD. AFTER FLIGHT/ SHUTDOWN (VERIFIED UNPRESSURIZED) UNABLE TO PRESS IN RED PUSH BUTTON ON
- [SDR DXTA2021102250710](https://openairdocs.org/sdr/DXTA2021102250710), Oct 21, 2021: NONE. NONE. MAIN DOOR: WHEN THE MAIN CABIN DOOR IS OPEN, IT DOES NOT FULLY EXTEND THE EXTENSION GUIDE RODS. THERE IS A LITTLE BOUNCE AS PEOPLE BOARD AND DEPLANE FROM THE DO
- [SDR JGVR20210428001](https://openairdocs.org/sdr/JGVR20210428001), Apr 28, 2021: RIB. CORRODED. MECHANICALLY REMOVED 13 AREAS OF CORROSION IN LH MLG, OUTBD RIB AT WS 67.25 INBD ROW OF FASTENERS. FOUND CORROSION BLENDS TO BE BEYOND C680 SRM 51-70-02 LIMITAT
- [SDR JGVR20210413001](https://openairdocs.org/sdr/JGVR20210413001), Apr 13, 2021: DOOR FRAME. CORRODED. 10+ AREAS OF VERIFIED CORROSION AROUND PERIMETER OF EMERGENCY EXIT DOOR. MECHANICALLY REMOVED 10 AREAS OF CORROSION ON OUTER SKIN OF E-EXIT. PERFORMED AN EDDY C
- [SDR DXTA2020110104330](https://openairdocs.org/sdr/DXTA2020110104330), Nov 1, 2020: CONTROL UNIT. DEFECTIVE. AT APPROXIMATELY 150' AGL THE PRIMARY TRIM FAIL LIGHT CAME ON AND THE TRIM STARTED TO RUN AWAY NOSE UP. I PRESSED THE AP/TRIM/NWS DISC BUTTON WHICH STOPPED THE 
- [SDR JGVR20201027002](https://openairdocs.org/sdr/JGVR20201027002), Oct 27, 2020: SPAR. CORRODED. MECHANICALLY REMOVED CORROSION FROM AFT SPAR, LOWER FORWARD SPAR CAP ANGLE LOCATED IN RT WHEEL WELL AT WS35. PERFORMED NDT AND REPORTED RESULTS FOR REPAIR DISPO
- [SDR EBVR20191022001](https://openairdocs.org/sdr/EBVR20191022001), Oct 22, 2019: SKIN. CORRODED. DURING INSPECTION FOUND CORROSION UNDER FLOORBOARD PANEL 162AC. COMPLIED WITH AQRD ERO-962576 FUSELAGE REPAIR, REVISION IR, DATED OCTOBER 26, 2019. AND 8110-3 D
- [SDR DXTA2019061432496](https://openairdocs.org/sdr/DXTA2019061432496), Jun 13, 2019: DISPLAY. MALFUNCTIONED. CAPTAIN MCDU BLANK/WENT BLANK - IN FLIGHT ON ARRIVAL WITH APU ON, THE #1 MCDU WENT BLANK AND WE NOTICED WHAT APPEARED TO BE AN ACCOCIATED HOT ELECTRICAL SMELL. 
- [SDR JGVR20190419001](https://openairdocs.org/sdr/JGVR20190419001), Apr 19, 2019: SPAR. CORRODED. MECHANICALLY BLENDED AREA OF CORROSION ON AFT SPAR IN LH GEAR WELL, POLISHED, AND PERFORMED NDT FOR REPAIR DISPOSITION. TREATED, TOPCOATED AND REPLACED FASTENER
- [SDR DXTA2019011801925](https://openairdocs.org/sdr/DXTA2019011801925), Jan 17, 2019: ECS. ODOR. CABIN ODOR OIL SMELL - PUNGENT OILY SMELL NOTICED IN COCKPIT/CABIN AT LOW POWER SETTINGS/SPEEDS AT LOW ALTITUDES DURING DESCENT. APU WAS NOT RUNNING.**WAITING F
- [SDR DXTA2018011100466](https://openairdocs.org/sdr/DXTA2018011100466), Jan 11, 2018: OIL SYSTEM. OVERSERVICED. INFLIGHT AT FL430 PASSENGERS NOTED A STRONG ODOR OF BURNING RUBBER/HOT OIL. NOTED A HOT/BURNING ODOR FROM THE GALLEY AREA. FOUND APU OIL OVERSERVICED DURING A G
- [SDR DXTA2018010400427](https://openairdocs.org/sdr/DXTA2018010400427), Dec 31, 2017: SWITCH. FAILED. ON DEPARTURE, HAD TO CYCLE THE GEAR 3 - 4 TIMES BEFORE FINALLY LOCKING INTO PLACE. REMOVED THE NOSE GEAR SQUAT SWITCH AND ACTUATING CAM. INSTALLED NEW SWITCH AN
- [SDR DXTAT2PL6D005MNZR](https://openairdocs.org/sdr/DXTAT2PL6D005MNZR), Dec 29, 2017: CAM. DEFECTIVE. ON DEPARTURE, THE LANDING GEAR WOULD NOT RETRACT. ICE AND SLUSH ON THE GEAR ARE PROBABLY THE REASON. REMOVED THE NOSE GEAR SQUAT SWITCH ACTUATING CAM. INSTALLED
- [SDR DXTA201801010001](https://openairdocs.org/sdr/DXTA201801010001), Dec 29, 2017: UNKNOWN. MALFUNCTIONED. ON DEPARTURE THE LANDING GEAR WOULD NOT RETRACT. ICE AND SLUSH ON THE GEAR ARE PROBABLY THE REASON.
- [SDR JGVR20171220001](https://openairdocs.org/sdr/JGVR20171220001), Dec 20, 2017: SPAR CAP. CORRODED. FOUND CORROSION AROUND TWO LOCK FASTENERS LOCATED IN THE RT WING LOWER SPAR CAP NEAR RWS 49.50. REMOVED AFFECTED LOCK FASTENERS, PERFORMED BLEND AND TREAT REPAI
- [SDR 2017F00047](https://openairdocs.org/sdr/2017F00047), Feb 17, 2017: FITTING. CORRODED. AFT WING SPAR BULKHEAD FITTING CORRODED.
- [SDR DXTA2016091306301](https://openairdocs.org/sdr/DXTA2016091306301), Sep 13, 2016: UPLOCK SWITCH. OUT OF RIG. IN FLIGHT LEVEL 41,000, HEARD AND FELT A THUNK NOISE FROM THE FRONT OF THE PLANE. THE RED LANDING GEAR UNLOCK LIGHT ILLUMINATED BUT THERE WERE NO UNUSUAL RUMBLE
- [SDR DXTA2014052005776](https://openairdocs.org/sdr/DXTA2014052005776), May 19, 2014: POWER SUPPLY. FAILED. DURING CRUISE AT FL410, FIRST MONITOR WARNING FAIL CAS MESSAGE, FOLLOWED BY MONITOR WARNING FAIL RT IN DESCENT. ALSO MAU 1 & 2 FAIL, GPS 2 INACTIVE, TAWS FAILUR
- [SDR DXTA2014031705691](https://openairdocs.org/sdr/DXTA2014031705691), Mar 16, 2014: POWER SUPPLY. FAILED. BOTH MAU1 & MAU2 FAILED. REPLACED MAU 1 & 2 POWER SUPPLIES & NIC PROCESSOR IAW MM 34-17-00. LOADED SOFTWARE & OPS CHECKED WITH NO FAULTS NOTED.
- [SDR DXTA2014031705689](https://openairdocs.org/sdr/DXTA2014031705689), Mar 15, 2014: STARTER GEN. FAILED. DURING CRUISE AT FLIGHT LEVEL 410, RECEIVED AN AMBER DC GENERATOR OFF LIGHT & AN AMBER DC EMERGENCY BUSS LIGHT, CAS MESSAGE. LOST THE NR 1 DISPLAY UNIT, THE NR 
- [SDR CWQD201101](https://openairdocs.org/sdr/CWQD201101), Jan 26, 2011: PUMP. LEAKING. DURING UNSCHEDULED MX, THE RT ENGINE HYD PUMP WAS REPLACED DUE TO INTERNAL LEAKAGE.

## Service difficulty reports on N320QS not matched to an aircraft (9)

They name N320QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200601530](https://openairdocs.org/sdr/DXTA200601530), Jul 30, 2006: WIRE. CHAFED. ON TAKEOFF, WHEN GEAR HANDLE WAS PLACED IN THE UP POSITION, THE GEAR CONTROL CIRCUIT BREAKER POPPED, GEAR WOULD NOT RETRACT. 200KTS WAS NOT EXCEEDED. FOUND WIRE
- [SDR DXTA200601465](https://openairdocs.org/sdr/DXTA200601465), Jun 29, 2006: THROTTLE. OUT OF RIG. ENGINES STARTED NORMALLY, DURING SPEED BRAKE RETRACTION TEST THE LEFT ENGINE FLAMED OUT, TAXIED BACK TO FBO. RERIGGED LT ENGINE THROTTLE IAW CE560 MM 76-11-00. 
- [SDR DXTA200500868](https://openairdocs.org/sdr/DXTA200500868), Jul 27, 2005: PIN. BROKEN. ANIT-SKID INOP LIGHT ILLUMINATED IN FLIGHT AS GEAR RETRACTED, EMERGENCY BRAKES USED ON LANDING. FOUND ONE BROKEN PIN, THE CONNECTOR CORRODED ON THE BITE BOX. RE
- [SDR DXTA200500637](https://openairdocs.org/sdr/DXTA200500637), Mar 19, 2005: ANTI-SKID SYS. DEFECTIVE. WHEN GEAR WAS SELECTED DOWN THE POWER BRAKE LOW PRESS AND ANTI SKID INOP LIGHT CAME ON AND REMAINED ON. DURING BRAKE OPERATION PEDALS WERE SOFT BUT BRAKING WAS 
- [SDR DXTA200400385](https://openairdocs.org/sdr/DXTA200400385), Sep 8, 2004: CONTROL HANDLE. STUCK. DURING FLIGHT THE FLAPS DEPLOYED AT 7 DEGREES AND FLAP CONTROL LEVER IS STUCK IN POSITION. ADJUSTED FLAP PRESELECT LEVER AND OPERATIONAL CHECK GOOD, PERFORMED W
- [SDR DXTA200400363](https://openairdocs.org/sdr/DXTA200400363), Aug 17, 2004: DIODE. FAILED. THE LEFT THRUST REVERSER DEPLOYED IN FLIGHT. REMOVED AND REPLACED DIODES NR 169 AND 171, ALSO REMOVED AND REPLACED LEFT T/R SELECTOR VALVE. LEFT T/R OPS AND LEA
- [SDR DXTA200400221](https://openairdocs.org/sdr/DXTA200400221), Jan 19, 2004: WIRE. LOOSE. DURING TAXIING OUT FOR TAKEOFF, PASSENGER NOTICED BURNING ELECTRICAL ODOR IN CABIN. CREW MEMBER VERIFIED THE ELECTRICAL ODOR COMING FROM THE CEILING NEAR THE RE
- [SDR DXTA200300136](https://openairdocs.org/sdr/DXTA200300136), Oct 13, 2003: FLOW DIVIDER. OUT OF RIG. DURING GROUND CHECK BY CREW LT ENGINE FLAMED OUT WHEN POWER BROUGHT BACK TO IDLE. FOUND RIGGING ON FUEL FLOW DIVIDER SLIGHTLY OUT. ADJUSTED RIGGING ON FUEL FLOW
- [SDR DXTA200300128](https://openairdocs.org/sdr/DXTA200300128), Sep 28, 2003: HEAT EXCHANGER. DIRTY. DURING ENROUTE FROM PHL TO ACK, NOTICED A BURNING ELECTRICAL ODOR FOLLOWED BY THE EMERGENCY PRESSURIZATION LIGHT. ACCOMPLISHED AIR TURN BACK TO PHL CLEANED LINT

## 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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