# N308QS: 2006 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: 680-0116 - Year built: 2006 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 21, 2006 - Certificate issued: December 6, 2019 - Expires: December 31, 2029 - Mode S code: A33E79 - Owner type: Corporation, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=308QS - Page: https://openairdocs.org/aircraft/N308QS 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 N308QS. ## 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 20181008019629I](https://openairdocs.org/incident/20181008019629I), Oct 8, 2018: Cessna 680 (N308QS), Stratford, CT, Minor damage. [privacy data omitted] From the bradley FSDO(AFG-600), was notified 8 ocober 2018 at 1000. [privacy data omitted] Assisted the chdo(columbus Ohio FSDO) by… - [Incident 20070314003209I](https://openairdocs.org/incident/20070314003209I), Mar 14, 2007: Cessna 680CE (N308QS), Lincoln, NE. (-23) N308QS, CE680, was operated by net jets aviation inc., on a repositioning flight from st. paul, MN to Lincoln, NE. Thirty five miles north east of… ## Reports on N308QS not matched to an aircraft (1) They name N308QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [Incident 20011214037639I](https://openairdocs.org/incident/20011214037639I), Dec 14, 2001: Cessna 560CESSNA (N308QS), Philadelphia, PA. (-23) After landing on runway at phl eja 308 reported loss of brakes and ran off the end of runway 94. No injuries. After a/w and maintenance inspected… ## Service difficulty reports (43) 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 DXTA2026012006591](https://openairdocs.org/sdr/DXTA2026012006591), Jan 19, 2026: BATTERY PACK. FAULTY. RIGHT FORWARD EXTERIOR EMERGENCY LIGHT DOES NOT COME ON DURING EMERGENCY LIGHT TEST. REMOVED NR 3 BATTERY. INSTALLED CUSTOMER SUPPLIED NEW EMER BATTERY. OPS CHE - [SDR DXTA2026011606557](https://openairdocs.org/sdr/DXTA2026011606557), Jan 15, 2026: LIGHT. INOPERATIVE. DURING EMERGENCY LIGHT PREFLIGHT CHECK THE FORWARD OVER WING LIGHT, SEAT 8 LIGHT, AND AFT WALL EXIT SIGN LIGHT DID NOT ILLUMINATE. WE POWERED UP THE AIRPLANE TO - [SDR DXTA2025053003669](https://openairdocs.org/sdr/DXTA2025053003669), May 28, 2025: G SWITCH. TRIPPED. UPON SHUTDOWN EMER LIGHTS WOULD NOT EXTINGUISH. RESET PILOT/CP 5G SWITCH AND ATTEMPTED POWER CYCLE RESET WITH NEGATIVE RESULT. CORRECTIVE ACTION: CONFIRMED THE - [SDR DXTA2025052303593](https://openairdocs.org/sdr/DXTA2025052303593), May 22, 2025: ACTUATOR. TIGHT. DURING CLIMBOUT PASSING 32000 WE GOT A VERY NOTICABLE THUD IN THE COCKPIT FLOOR, A "BUMP IN THE NIGHT". IT COULD BE FELT AND HEARD. IT HAPPENED 3 MORE TIMES AND - [SDR DXTA2025031702721](https://openairdocs.org/sdr/DXTA2025031702721), Mar 16, 2025: BATTERY. DEFECTIVE. BATTERY O'TEMP L RED CAS: AT APPROXIMATELY 4000 FEET ON CLIMB OUT RED MASTER, WARNING, LIGHT, ORAL ALERT, AND BATTERY OVER TEMP LEFT CAS MESSAGE ILLUMINATED. AC - [SDR JGVR20250214001](https://openairdocs.org/sdr/JGVR20250214001), Feb 14, 2025: DOOR. CORRODED. BLENDED MULTIPLE AREAS OF CORROSION ON THE EMERGENCY EXIT DOOR P/N 6911251-4, REMOVED CONTOUR RING FOR ACCESS AND BLENDED ADDITIONAL AREAS OF CORROSION PERFORME - [SDR JGVR20250123001](https://openairdocs.org/sdr/JGVR20250123001), Jan 23, 2025: SPAR. CORRODED. MECHANICALLY REMOVED 3 AREAS OF CORROSION LOCATED IN LH MLG WHEEL WELL, AFT WING SPAR LOWER CLIP INBOARD OF BAY 730DL PERFORMED NDT AND REPORTED FOR REPAIR DISP - [SDR JGVR20250117001](https://openairdocs.org/sdr/JGVR20250117001), Jan 17, 2025: SKIN. CORRODED. MECHANICALLY BLENDED 3 AREAS OF CORROSION UNDER RH LOWER WING SKIN, AFT SIDE, INBD OF FLAP PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, - [SDR DXTA2024111401130](https://openairdocs.org/sdr/DXTA2024111401130), Nov 12, 2024: PRESSURE SWITCH. FAULTED. FUEL PRESSURE LOW L AMBER CAS: AFTER TAKEOFF ABOUT 300 FT AGL WE RECEIVED THE FUEL PRESSURE LOW L CAS MESSAGE. RAN THE QRH MESSAGE DID NOT CLEAR. ON FINAL BACK - [SDR 2024F00201](https://openairdocs.org/sdr/2024F00201), Aug 24, 2024: SPAR CAP. CORRODED. CORROSION WAS FOUND ON THE 6922435-4 REAR SPAR CAP, LOWER FORWARD ANGLE-RH, NEAR RWS 41. ACCOMPLISHED FIELD REPAIR: FR-680-0116-1466 REV -, FIELD REPAIR-CORROSI - [SDR EBVR450D121923001](https://openairdocs.org/sdr/EBVR450D121923001), Dec 19, 2023: ATTACH FITTING. CORRODED. FRETTING CORROSION ON AFT HORIZONTAL ATTACH FITTINGS, ON THE HORIZONTAL STAB AND VERTICAL STAB. TEXTRON ENGINEERING PER MINOR RECOMMENDED REPAIR MEMO DQ40986M1 - [SDR DXTA2023012378980](https://openairdocs.org/sdr/DXTA2023012378980), Jan 21, 2023: FUSE. BLOWN. CABIN EMERGENCY LIGHTS INOP. EXIT SIGN OVER MAIN CABIN DOOR INOPERATIVE. EXIT SIGNS LT AND RT OF MAIN CABIN DOOR INOPERAITVE. EMERGENCY LIGHT OVER GALLEY INOPER - [SDR DXTA2023011778680](https://openairdocs.org/sdr/DXTA2023011778680), Jan 16, 2023: APU. DEFECTIVE. AFTER STARTING APU, AND AFTER TURNING BLEEDS ON CABIN, AND FLIGHT DECK STARTED TO FILL WITH A THICK HAZE FROM THE INTERIOR OUTLETS. APU REMOVED AND REPLACED IAW - [SDR 3J7R2023011200001](https://openairdocs.org/sdr/3J7R2023011200001), Jan 11, 2023: POWER SUPPLY. BLOWN. THE FORWARD EMERGENCY LIGHTS IN THE CABIN AT THE CABIN DOOR ARE INOP, AT LEAST THREE SIGNS ARE OUT. THESE INCLUDE THE EXIT SIGN IN THE OVERHEAD AND THE EXIT SIG - [SDR DXTA2022122376910](https://openairdocs.org/sdr/DXTA2022122376910), Dec 23, 2022: BATTERY PACK. DEFECTIVE. WHEN THE PASSENGER SAFETY PUSH SWITCH WAS TURNED ON DURING DESCENT, NONE OF THE EMERGENCY LIGHTS ILLUMINATED. WITH THE EMERGENCY LIGHTS SWITCH IN THE ARM POSITI - [SDR DXTA2021122854310](https://openairdocs.org/sdr/DXTA2021122854310), Dec 27, 2021: UNKNOWN. UNKNOWN. CABIN EMERG LIGHT: CABIN EMERGENCY LIGHTS INOP. WOULD NOT COME ON DURING PREFLIGHT, LIGHTS WORK ON NORMAL BATTERY POWER. (PRE-FLIGHT) // SIGNOFF // COMPLIED WIT - [SDR JGVR20210429001](https://openairdocs.org/sdr/JGVR20210429001), Apr 29, 2021: SPAR. CORRODED. BENDED CORRODED ARE AROUND THE LH WING MIDDLE SPAR AFT SIDE AROUND THE BRAKE LINE BULKHEAD FITTING, PERFORMED ULTRASONIC THICKNESS INSPECTION AND REPORTED FOR R - [SDR DXTA030120213881](https://openairdocs.org/sdr/DXTA030120213881), Feb 28, 2021: PCB. DEFECTIVE. WING ANTI-ICE COLD L AMBER CAS: AT FL220 IN ICING CONDITIONS, WING ANTI-ICE COLD L&R AMBER MSG ILLUMINATED. DUE TO ATC CONDITIONS AND COMM ISSUES, WE DECLARED A - [SDR 2020FA0000558](https://openairdocs.org/sdr/2020FA0000558), Dec 20, 2020: SPAR CAP. CORRODED. VERTICAL STABILIZER AFT SPAR CAP DAMAGE (CORROSION). ENGINEERING MEMO DQ28088M1 DATED DECEMBER 7, 2020. - [SDR DXTA2020111504357](https://openairdocs.org/sdr/DXTA2020111504357), Nov 15, 2020: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS ON RIGHT SIDE INOPERABLE. 2 RIGHT SIDE EXTERIOR OVER WING, RIGHT SIDE SHARK LIGHT, INTERIOR LAV OVERHEAD AND EXIT LIGHTS, AFT FLOOR LIGHTING, R - [SDR DXTA2020092804144](https://openairdocs.org/sdr/DXTA2020092804144), Sep 28, 2020: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN SWITCH IS PLACED TO ARM WITH BATTERIES OFF. FOUND DURING PREFLIGHT. R & R THE NR 1 EMERGENCY BATTERY, CHARGED BATTERY WI - [SDR DXTA2020011303322](https://openairdocs.org/sdr/DXTA2020011303322), Jan 9, 2020: ACTUATOR. MALFUNCTIONED. RIGHT MLG LANDING GEAR RETRACTION DID NOT RETRACT - RIGHT MAIN DID NOT RETRACT. THE NOSE AND LEFT MAIN RETRACTED NORMALLY. THE RED UNLOCK LIGHT WENT OUT WITH TH - [SDR DXTA2019123093266](https://openairdocs.org/sdr/DXTA2019123093266), Dec 29, 2019: CONVERTER. DIRTY. CABIN ODOR OIL SMELL - AT 45000 SLIGHT ORDER AND A LOT OF HAZE IN CABIN. DROPPED OX MASK, RAN CHECK LIST . SELECTED L PRESSURE SOURCE , CABIN CLEARED. REMOVED O - [SDR DXTA2019071502611](https://openairdocs.org/sdr/DXTA2019071502611), Jul 12, 2019: ENGINE. MALFUNCTIONED. REPEAT WRITE UP. DECENDING FROM FL410, POWER WAS REDUCED TO IDLE. AIRCRAFT BEGN TO SHUDDER AND RIGHT ENGINE SHUTDOWN CAS MESSAGE DISPLAYED. RIGHT ENGINE UNCOMMA - [SDR DXTA2019061402501](https://openairdocs.org/sdr/DXTA2019061402501), Jun 14, 2019: BLEED VALVE. ABNORMAL. AT FLIGHT LEVEL 43000 WE WERE CLEARED TO DECENT TO 35000. AS WE REDUCED THRUST LEVERS TO IDLE, FELT A RUMBLE, CYAN RIGHT ENGINE SHUTDOWN CAS MESSAGE. RIGHT ENGI - [SDR DXTA2019052302430](https://openairdocs.org/sdr/DXTA2019052302430), May 23, 2019: SOLENOID. ABNORMAL. SHORTLY AFTER INITIATING DESCENT FROM FL430, AND EVENTUALLY AT FLIGHT IDLE, EXPERIENCED TWO SHORT BURSTS OF ENGINE VIBRATION, AND NOTICED THAT THE CYAN ENGINE S - [SDR DXTA2019F00018](https://openairdocs.org/sdr/DXTA2019F00018), Feb 22, 2019: SPAR CAP. DAMAGED. RT WING FORWARD SPAR CAP ANGLE REPAIR. ACCOMPLISHED IAW AQRD ENGINEERING ORDER ERO-102798 DATED 01/15/2019. - [SDR JGVR20180316002](https://openairdocs.org/sdr/JGVR20180316002), Mar 16, 2018: STRUCTURE. CORRODED. CORRODED AREAS ON THE UPPER AND LOWER SURFACES OF THE EMERGENCY EXIT DOOR ALONG THE CONTOUR RINGS. BLENDED THE CORROSION. PERFORMED EDDY CURRENT INSPECTION FOR - [SDR JGVR20180316001](https://openairdocs.org/sdr/JGVR20180316001), Mar 16, 2018: SKIN. CORRODED. REPAIRED TWO CORRODED AREAS ON THE UPPER LT WING SKIN AT WS 37 NEAR THE DRAG ANGLE. - [SDR DXTA20170406156](https://openairdocs.org/sdr/DXTA20170406156), Apr 6, 2017: SKIN. DEBONDED. REPAIR OF NOSE SKIN DISBONDS AROUND ACCESS DOOR OPENINGS. REPAIRED. - [SDR DXTA2014060905797](https://openairdocs.org/sdr/DXTA2014060905797), Jun 6, 2014: BEARING. FAILED. WHEN STOPPING THE ACFT ON THE RAMP BOTH MAIN GEAR BRAKES GROWL & GRAB WHEN MAKING A COMPLETE STOP. TAXIED ACFT FOUND LT & RT BRAKE GROWLING AT VERY SLOW SPEEDS. - [SDR DXTA2014021005643](https://openairdocs.org/sdr/DXTA2014021005643), Feb 8, 2014: WATER SEPARATOR. DIRTY. INFLIGHT AT FL 430 PAX COMPLAINED OF SOMETHING BURNING. WE SMELLED IT IN THE FLIGHT DECK., I WENT TO THE BACK & THE ODOR WAS STRONGEST NEAR THE LAVATORY. CREW D - [SDR DXTA2013090305491](https://openairdocs.org/sdr/DXTA2013090305491), Sep 2, 2013: CONVERTER. FAILED. WHILE RUNNING APU, NOTICED ODOR LIKE DIRTY SOCK. AFTER TAKEOFF, NOTICED ODOR LIKE BURNING OIL. NO SMOKE SEEN. REMOVED AND CLEANED OZONE CONVERTERS REMOVED AND C - [SDR DXTA2013081905478](https://openairdocs.org/sdr/DXTA2013081905478), Aug 18, 2013: COALESCER BAG. CONTAMINATED. ON GROUND, DURING APU START WITH BATTERIES, CABIN FILLED WITH WHITE SMOKE. APU BLEED AIR AND GENERATOR SWITCHES ON. ENVIROMENTAL SWITCHES AUTO AND COLD. WHITE S - [SDR DXTA2013081305474](https://openairdocs.org/sdr/DXTA2013081305474), Aug 11, 2013: PUMP. LEAKING. ENVIRONMENTAL SMOKE NOTICED FROM FRONT WEMAC VENTS. MORE PRONOUNCED IN HP MODE AND DURING POWER REDUCTION. CHECKLIST WAS USED AND IT WOULD SEEM TO BE ISOLATED T - [SDR DXTA2013020705278](https://openairdocs.org/sdr/DXTA2013020705278), Feb 7, 2013: STRUT. DAMAGED. ON DEPARTURE GEAR WOULD NOT RETRACT. 3 GREEN AND RED UNLOCK ILLUMINATED. PUT THE GEAR HANDLE BACK DOWN TO MATCH 3 GREEN CONDITION. SHORTLY AFTER, AMBER "WOW MIS - [SDR CWQR20120613040](https://openairdocs.org/sdr/CWQR20120613040), Jun 13, 2012: CABLE. FRAYED. DURING A SCHEDULED MX EVENT, FOUND THE PILOT'S RT BRAKE CONTROL CABLE FRAYED ABOUT 50 PERCENT. DID NOT SEE ANY ISSUES WITH THE CABLE RUN OR RUBBING ON STRUCTURE - [SDR DXTA2011121904826](https://openairdocs.org/sdr/DXTA2011121904826), Dec 17, 2011: FLAP SYSTEM. FAILED. WHEN SELECTING FLAPS 15, FLAPS FAILED, AMBER CAS MESSAGE DURING APPROACH AT 180KTS. OBSERVED BITE CODES 5 & 8 ON AFT BAY CONTROLLER. OPS CK OF FLAPS GOOD. MCC R - [SDR DXTA2011030704495](https://openairdocs.org/sdr/DXTA2011030704495), Mar 5, 2011: PACKING. DAMAGED. UPON GEAR RETRACTION, NOSE GEAR MADE SEVERAL LOUD "BANGS" WHILE ENTIRE AIRCRAFT SHUDDERED AND VIBRATED. AFTER APPROX 10 SECONDS, NOSE GEAR FINALLY FULLY RETRACT - [SDR DXTA2010111504306](https://openairdocs.org/sdr/DXTA2010111504306), Nov 14, 2010: ECU. INOPERATIVE. WITH APU "ON" AND APU BLEED "ON", SMOKED FILLED COCKPIT. FOUND ECU TURBINE TO BE NOT OPERATING. R & R ECU TURBINE. OPS AND LEAK CHECKED GOOD. IAW MM 21-51-00. - [SDR DXTA2010031904042](https://openairdocs.org/sdr/DXTA2010031904042), Mar 18, 2010: DOWNLOCK SWITCH. FAILED. RT GREEN GEAR INDICATOR LIGHT ILLUMINATED DURING FLIGHT. NO GEAR UNSAFE LIGHT WAS ASSOCIATED WITH IT. REMOVED RT MAIN GEAR DOWNLOCK SWITCH AND INSTALLED NEW SWI - [SDR DXTA200702562](https://openairdocs.org/sdr/DXTA200702562), Oct 23, 2007: WARNING LIGHT. FALSE INDICATION. GEAR UNLOCK LIGHT REMAINED ILLUMINATED. CYCLED GEAR ONE TIME. PERFORMED VISUAL INSPECTION OF LANDING GEAR UPLOCK SYSTEM. NO DEFECTS NOTED. VERIFIED PROPER ENGAG - [SDR DXTA200702309](https://openairdocs.org/sdr/DXTA200702309), Jun 29, 2007: LEVER. OUT OF ADJUST. SPEED BRAKE LEVER DOES NOT STAY IN THE FULLY DEPLOYED DETENT, IT TENDS TO (SPRING) BACK TO A HALF DEPLOYED POSTION. ADJUSTED SPEED BRAKE LEVER DETENT. OPERATION ## Service difficulty reports on N308QS not matched to an aircraft (4) They name N308QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA200400230](https://openairdocs.org/sdr/DXTA200400230), Jan 26, 2004: ACTUATOR. MALFUNCTIONED. AFTER TAKEOFF GEAR UNSAFE LIGHT AND HYDRAULIC PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED AIR TURNBACK AND LANDED SAFELY. REMOVED FAULTY LT MAIN GEAR ACTUATOR AND - [SDR DXTA200300120](https://openairdocs.org/sdr/DXTA200300120), Sep 19, 2003: LAMP. INOPERATIVE. DURING APPROACH, SELECTED GEAR DOWN AND THE LEFT MAIN GEAR LIGHT DID NOT SHOW DOWN AND LOCKED. MANUAL (T-HANDLE) GEAR EXTENSION PULLED TO BLOW GEARS DOWN, LANDI - [SDR DXTA200300032](https://openairdocs.org/sdr/DXTA200300032), May 16, 2003: LANDING GEAR. MALFUNCTIONED. GEAR WOULD NOT RETRACT AFTER TAKEOFF . HAD NO PROBLEM EXTENDING FOR LANDING DID NOT USE EMERGENCY BLOW DOWN . NOSE ANNUNCIATER REMAINED GREEN AND RED ANNUN REMA - [SDR CWQ2003F00008](https://openairdocs.org/sdr/CWQ2003F00008), Mar 3, 2003: DUCT. CRACKED. DURING ROUTINE INSPECTION LOOKED INTO NACA DORSAL SCOOP AND FOUND THE LOWER AIR VANE PN 651207212 CRACKED .3750 INCH WITH THE CRACK STARTING FROM THE CENTER OF ## 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 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.