# N317QS: 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: 680-0160
- Year built: 2007
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 14, 2007
- Certificate issued: August 14, 2020
- Expires: August 31, 2027
- Mode S code: A36241
- Owner type: Corporation
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=317QS
- Page: https://openairdocs.org/aircraft/N317QS

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 N317QS.

## FAA accident and incident reports

None matched to N317QS.

## Service difficulty reports (30)

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 DXTA2026041507632](https://openairdocs.org/sdr/DXTA2026041507632), Apr 12, 2026: G SWITCH. TRIPPED. WITH MAIN BATTERIES OFF AND ALSO DISCONNECTED (EMERGENCY LIGHTS ALSO OFF), 3 CABIN LIGHTS INLINE WITH THE EMERGENCY LIGHTING SYSTEM (LEFT FORWARD TABLE AND LEFT
- [SDR DXTA2025091104899](https://openairdocs.org/sdr/DXTA2025091104899), Sep 9, 2025: BATTERY PACK. INOPERATIVE. ON EMERGENECY LIGHTS TEST THE FOLLOWING LIGHTS ARE NOT ILLUMINATING: SEAT LIGHT OVER SEAT 8 RT SIDE WING INSPECTION LIGHT & RT FWD EMERGENCY LIGHT ABOVE WING AL
- [SDR JGVR2025051504](https://openairdocs.org/sdr/JGVR2025051504), May 15, 2025: HINGE BRACKET. CORRODED. UPPER RUDDER HINGE BRACKET, CORROSION, THAT REQUIRED THE REPLACEMENT OF THE UPPER RUDDER HINGE BRACKET PN: 6931050-64
- [SDR JGVR20250402005](https://openairdocs.org/sdr/JGVR20250402005), May 14, 2025: SKIN. CORRODED. REPAIRED CORRODED AREAS OF THE UPPER INBOARD WING SKINS LOCATED UNDER AND ADJACENT TO THE LH AND RH WING AFT DRAG ANGLES (WING-TO-FUSELAGE FAIRING STRUCTURE), B
- [SDR 2025F00106](https://openairdocs.org/sdr/2025F00106), Apr 29, 2025: ANGLE. CORRODED. RH MLG WHEEL WELL AFT SPAR LOWER CLIP INBD OF WS 37.00 IS HEAVILY CORRODED NEAR 2 HI-LOK'S. MECHANICALLY REMOVED CORROSION LOCATED IN RH MLG WHEEL WELL, AFT SPA
- [SDR JGVR20250416003](https://openairdocs.org/sdr/JGVR20250416003), Apr 16, 2025: SUPPORT BEAM. CORRODED. MECHANICALLY REMOVED AREA OF CORROSION ROUND CARRY THRU HYDRAULIC FITTING LOCATED IN RH MLG WHEEL WELL FORWARD END OF WS 37.00 BEAM SUPPORT ON INBOARD SIDE, PER
- [SDR JGVR20250416002](https://openairdocs.org/sdr/JGVR20250416002), Apr 16, 2025: SKIN. CORRODED. BLENDED 3 AREAS OF CORROSION ON THE LOWER FUSELAGE SKIN AROUND LH FWD FUSELAGE CHIN FAIRING, R&R LH FORWARD CHIN FAIRING FOR ACCESS, PERFORMED NDT AND REPORTED 
- [SDR JGVR20250416001](https://openairdocs.org/sdr/JGVR20250416001), Apr 16, 2025: STRUCTURE. CORRODED. MECHANICALLY REMOVED 11 AREAS OF CORROSION FROM E-EXIT DOOR STRUCTURE NEAR CONTOUR RING, PERFORMED NDT AND REPORTED FOR DISPOSITION. REPAIRED CORROSION BLENDS B
- [SDR DXTA2025021402364](https://openairdocs.org/sdr/DXTA2025021402364), Feb 13, 2025: HANDLE. LACK OF LUBE. MAIN DOOR LOCK: WHEN CLOSING THE MAIN CABIN DOOR THE PUSH BUTTON IN THE HANDLE WOULD NOT POP OUT WHEN THE HANDLE WAS IN THE CLOSED POSITION AND THE DOOR WOULD N
- [SDR DXTA2024122301614](https://openairdocs.org/sdr/DXTA2024122301614), Dec 19, 2024: SPRING. DAMAGED. MAIN DOOR: WHEN LOCKING PLANE UP FOR THE NIGHT WHEN WE LIFTED THE UNLOCK BAR TO CLOSE THE AIRSTAIRS WE HEARD A LOUD BANG AND THE DOOR WOULD NOT MOVE. WE REALIZE
- [SDR JGVR20240306001](https://openairdocs.org/sdr/JGVR20240306001), Mar 6, 2024: SKIN. CORRODED. BLENDED CORRODED AREAS UNDER THE NUTPLATES COMMON TO THE LH & RH WING FLAP PANELS 523AB AND 623AB, PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED 
- [SDR DXTA2023120810283](https://openairdocs.org/sdr/DXTA2023120810283), Dec 8, 2023: UNKNOWN. UNKNOWN. EMERGENCY EXIT SIGN ON THE AFT RIGHT FACING UPPER DIVIDER MIRROR IS OUT. ALL EMERGENCY LIGHTS TESTED OKAY DURING PREFLIGHT INSPECTION AND FAILED IN FLIGHT. IAW 
- [SDR DXTA2023092095950](https://openairdocs.org/sdr/DXTA2023092095950), Sep 19, 2023: UNKNOWN. UNKNOWN. SHADE IN THE EMERGENCY EXIT DOOR/HATCH IS FAILED IN THE CLOSED POSITION. REMOVED EMERGENCY DOOR AND GAINED ACCESS TO THE WINDOW SHADE. TROUBLESHOT THE WINDOW SH
- [SDR 2023F00270](https://openairdocs.org/sdr/2023F00270), Sep 11, 2023: SPAR. CORRODED. R/H MLG WHEEL WELL FUEL AND HYDRAULIC LINE THRU PLATE HAS SURFACE CORROSION. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR S-680-ATA57/03RD REPAIR OF WING ST
- [SDR DXTA2023080792420](https://openairdocs.org/sdr/DXTA2023080792420), Aug 7, 2023: UNKNOWN. UNKNOWN. UPON TESTING THE EMER LIGHTS ON POWER UP, THE MAIN EXIT LIGHT OVER THE MAIN CABIN DOOR DID NOT ILLUMINATE. VERIFIED DISCREPANCY, ATTEMPTED TO CHARGE #1 BATTERY 
- [SDR 2023FA0000120](https://openairdocs.org/sdr/2023FA0000120), Mar 9, 2023: SPAR. CORRODED. FOUND DURING BASE CHECK RIGHT MAIN WHEEL WELL AFT SPAR HAS LEVEL 2 CORROSION IN 2 LOCATIONS WILL REQUIRE CLEAN AND BLEND
- [SDR DXTA2022052562610](https://openairdocs.org/sdr/DXTA2022052562610), May 24, 2022: SPRING. DAMAGED. MAIN DOOR CABLE: UPON RAISING CABIN DOOR THE FORWARD CABLE RELEASED AND THE DOOR WENT DOWN HARD. CABLE IS STILL ATTACHED AT BOTH ENDS BUT LOOSE. THE REAR CABLE 
- [SDR JGVR20200506001](https://openairdocs.org/sdr/JGVR20200506001), May 6, 2020: SPAR CAP. CORRODED. REMOVED FOUR HI-LOK FASTENERS FOR ACCESS AND BLENDED CORRODED AREA ON THE UPPER SURFACE OF THE LOWER WING SPAR CAP LOCATED IN THE LEFT HAND MAIN LANDING GEAR WH
- [SDR JGVR20190522002](https://openairdocs.org/sdr/JGVR20190522002), May 22, 2019: SKIN. CORRODED. REPAIRED NUMEROUS AREAS ON LOWER FUSELAGE SKIN, DOUBLERS, AND STRINGERS OF THE DROP AISLE AREA BETWEEN FS 157 AND FS 426 BY BLENDING OUT CORROSION, PERFORMING N
- [SDR JGVR20190522001](https://openairdocs.org/sdr/JGVR20190522001), May 22, 2019: DOUBLER. GOUGED. REPAIRED TWO GOUGED AREAS OF THE INTERIOR FUSELAGE DOUBLER NEAR THE ESCAPE HATCH AT FS 399.75 AND FS 403 BY BLENDING/SMOOTHING THE GOUGED AREAS PERFORMING NDT, 
- [SDR JGVR20181102002](https://openairdocs.org/sdr/JGVR20181102002), Nov 2, 2018: SKIN. CORRODED. THE LT WING SKIN WAS CORRODED. BLENDED CORRODED AREAS ON THE UPPER WING SKIN.
- [SDR JGVR20181031001](https://openairdocs.org/sdr/JGVR20181031001), Oct 31, 2018: SKIN. CORRODED. FOUND EMERGENCY EXIT DOOR CORRODED AROUND THE CONTOUR RINGS AND DOOR SKIN. REPLACED THE CONTOUR RINGS WITH NEW PARTS AND REPAIRED THE DOOR SKIN BY BLENDING AND 
- [SDR 2018FA0000010](https://openairdocs.org/sdr/2018FA0000010), Jan 10, 2018: SPAR. CORRODED. DURING GENERAL VISUAL INSPECTION OF THE LEFT MAIN WHEEL WELL INSPECTION, FOUND CORROSION ON THE AFT LOWER WING SPAR ASSEMBLY.
- [SDR DXTA2014051305770](https://openairdocs.org/sdr/DXTA2014051305770), May 12, 2014: SWITCH. FAILED. AFTER TAKEOFF, GEAR WOULD NOT RETRACT. WOW MISCOMPARE CAS MESSAGE CAME ON FOR THE REST OF THE FLIGHT. FOUND NOSE GEAR WOW SWITCH LOOSE, ADJUSTED & TIGHTENED SWI
- [SDR DXTA2014041105726](https://openairdocs.org/sdr/DXTA2014041105726), Apr 10, 2014: VALVE. MALFUNCTIONED. AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT COME UP. THE PIN NEVER RELEASED & THE GEAR LIGHTS REMAINED GREEN. AMBER WOW INCOMPARABLE CAS MESSAGE CAME ON & REMAINED
- [SDR DXTA2014040705719](https://openairdocs.org/sdr/DXTA2014040705719), Apr 6, 2014: SQUAT SWITCH. DAMAGED. AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. ABOUT TWO MINUTES LATER, RECEIVED AN AMBER WOW INCOMPARABLE CAS MESSAGE. BEFORE LANDING T
- [SDR DXTA2011092604736](https://openairdocs.org/sdr/DXTA2011092604736), Sep 25, 2011: DISPLAY. MALFUNCTIONED. CO-PILOTS PFD WOULD NOT DISPLAY ANY FLIGHT INFORMATION. IT WOULD ONLY DISPLAY RED X. YOU COULD GET THE FLIGHT INFORMATION IF YOU REVERTED THE DISPLAY TO DU 3. C
- [SDR DXTA2010110804297](https://openairdocs.org/sdr/DXTA2010110804297), Nov 5, 2010: BRAKE ASSY. WEAK. LEFT OUTER WHEEL BRAKE INDICATOR AT LIMITS. LT BRAKE MUSHY. REMOVED NR 1 BRAKE ASSY, INSTALLED O/H BRAKE ASSY. BLED BRAKES. REINSTALLED WHEEL ASSY AND TORQUED. 
- [SDR DXTA2010072004164](https://openairdocs.org/sdr/DXTA2010072004164), Jul 19, 2010: COFFEEMAKER. ODOR. 15 MIN INTO FLIGHT CREW NOTICED BURNING ODOR COMING FROM COFFEE & WATER POTS. TURNED POWER OFF TO POTS & ODOR CEASED. OPERATED BOTH TANKS FOR 30 MINUTES WITH NO
- [SDR DXTA2010041204064](https://openairdocs.org/sdr/DXTA2010041204064), Apr 10, 2010: COUPLING. UNSECURE. ON CLIMBOUT, "CABIN ALT" LIGHT ILLUMINATED. ACFT WAS 25,000 FT.; PAX O2 MASKS WERE DEPLOYED. CABIN ALT MAINTAINED 9,500' UNTIL DESCENT BELOW 10K'. DURING THE IN

## Service difficulty reports on N317QS not matched to an aircraft (3)

They name N317QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA200500882](https://openairdocs.org/sdr/DXTA200500882), Aug 4, 2005: BRAKE. INTERMITTENT. PON - LANDING RIGHT BRAKE PEDAL FOR RIGHT SIDE PILOT WAS SOFT (APPROX 3"- 4" TRAVEL) MUCH FIRMER ON SECOND APPLICATION. SAME SEQUENCE EXPERIENCED DURING TAXI. L
- [SDR DXTA200500662](https://openairdocs.org/sdr/DXTA200500662), Apr 6, 2005: WIRE. BROKEN. UPON GEAR EXTENSION, RIGHT MAIN GEAR INDICATOR LIGHT WOULD NOT ILLUMINATE. EMERGENCY GEAR EXTENSION CHECKLIST WAS ACCOMPLISHED; GEAR EXTENDED MANUALLY. EMERGENC
- [SDR 96ZZZX6178](https://openairdocs.org/sdr/96ZZZX6178), Oct 28, 1996: RUDDER SKIN. CRACKED. A LT RUDDER SKIN CRACK HORIZONTAL, ABOUT 2 INCHES LONG, AND ALONG THE RIB LINE OF THE RUDDER RIB BELOW THE TRIM TAB.

## 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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