# N315QS: 2008 Cessna 680 - Status: Valid registration - Airframe: [Cessna 680](https://openairdocs.org/model/cessna-680) (registry code 2076811, 9 seats) - Engine: [Pratt & Whitney Canada PW306C](https://openairdocs.org/engine/pratt-whitney-canada-pw306c) (registry code 52169) - Data sheets: [TCDS T00012WI](https://openairdocs.org/tcds/T00012WI) (Textron Aviation Inc.), [TCDS E35NE](https://openairdocs.org/tcds/E35NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: 680-0220 - Year built: 2008 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 8, 2008 - Certificate issued: March 20, 2020 - Expires: March 31, 2030 - Mode S code: A35AD3 - Owner type: Corporation - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=315QS - Page: https://openairdocs.org/aircraft/N315QS 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 N315QS. ## FAA accident and incident reports None matched to N315QS. ## Service difficulty reports (38) 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 2026F00213](https://openairdocs.org/sdr/2026F00213), Sep 23, 2026: SPAR CAP. CORRODED. CORROSION, VERTICAL STABILIZER, LH AFT SPAR CAP, VFS 116 - VFS 121. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0220-54511 REV -; FIELD REPAIR - CORROSION - [SDR DXTA2026072809019](https://openairdocs.org/sdr/DXTA2026072809019), Jul 26, 2026: STRUT. DISCHARGED. WE WERE CLIMBING THROUGH APPROXIMATELY FL200 WHEN WE FELT A CLUNK IN THE NOSE AREA, & THE RED, GEAR UNLOCK LIGHT ILLUMINATED & STAYED ON FOR THE DURATION OF THE - [SDR 2026072609019](https://openairdocs.org/sdr/2026072609019), Jul 26, 2026: LANDING GEAR. FAULTED. WE WERE CLIMBING THROUGH APPROXIMATELY FL200 WHEN WE FELT A CLUNK IN THE NOSE AREA WE THINK, AND THE RED, "GEAR UNLOCK" LIGHT ILLUMINATED AND STAYED ON FOR THE - [SDR DXTA2026072709019](https://openairdocs.org/sdr/DXTA2026072709019), Jul 26, 2026: WARNING MESSAGE. ILLUMINATED. WE WERE CLIMBING THROUGH APPROXIMATELY FL200 WHEN WE FELT A CLUNK IN THE NOSE AREA WE THINK, AND THE RED, GEAR UNLOCK LIGHT ILLUMINATED AND STAYED ON FOR THE DU - [SDR JGVR20251209002](https://openairdocs.org/sdr/JGVR20251209002), Dec 9, 2025: SKIN. CORRODED. MECHANICALLY BLENDED CORRODED AREA ON LOWER AFT RT WING SKIN, INBOARD OF FLAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED AR - [SDR JGVR20251209001](https://openairdocs.org/sdr/JGVR20251209001), Dec 9, 2025: DRAG ANGLE. CORRODED. BLENDED AREAS OF CORROSION ON THE LOWER AFT DRAG ANGLE, LEFT WING INBD OF FLAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED FASTENERS WI - [SDR DXTA2025111005625](https://openairdocs.org/sdr/DXTA2025111005625), Nov 9, 2025: BATTERY. INOPERATIVE. ON PREFLIGHT INSPECTION THE ONLY EMERGENCY LIGHTS THAT ILLUMINATE ARE ADJACENT TO THE MAIN CABIN DOOR AND THE FORWARD AISLE LIGHTS. ALL OTHER INTERIOR EMERGENCY - [SDR JGVR20250710001](https://openairdocs.org/sdr/JGVR20250710001), Jul 10, 2025: SPAR. CORRODED. MECHANICALLY BLENDED 1 EA. AREA OF CORROSION ON AFT SPAR, LOWER CLIP OUTBD AREA, IN THE RH MLG WHEEL WELL, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. RE - [SDR DXTA2025053003695](https://openairdocs.org/sdr/DXTA2025053003695), May 9, 2025: ELEC CONNECTOR. OPEN. GEAR SELECTED DOWN. RIGHT MAIN GEAR DID NOT ILLUMINATE DOWN. AND THE UNLOCKED LIGHT WAS ILLUMINATED. WE RAN THE FULL GEAR DID NOT EXTEND QRH WITH NO CHANGE TO T - [SDR DXTA2025031702683](https://openairdocs.org/sdr/DXTA2025031702683), Mar 14, 2025: FLAP SYSTEM. FAULTED. FLAPS FAIL AMBER CAS: WHEN SELECTING FLAP POSITION 15 AMBER CAS FLAP FAIL MESSAGE APPEARED. FLAPS DID NOT MOVE FROM ZERO POSITION. CORRECTIVE ACTION; POWERED UP - [SDR DXTA2025010701838](https://openairdocs.org/sdr/DXTA2025010701838), Jan 4, 2025: LANDING GEAR. FAULTED. DURING DEPARTURE OUT OF TNCM RAISED THE GEAR AFTER T/O AND HEARD A NOISE THEN NOTICED THAT BOTH MAIN LANDING GEAR STILL INDICATED DOWN WITH GREEN DOWN GEAR INDI - [SDR 2024F00304](https://openairdocs.org/sdr/2024F00304), Nov 22, 2024: SKIN. CORRODED. LH AND RH HORIZONTAL STAB UPPER AND LOWER SKIN HAS AREAS OF CORROSION JUST FWD OF ACCESS PANELS 351AC AND 352AC. MECHANICALLY REMOVED CORROSION ON LH UPPER AND - [SDR 2024F00303](https://openairdocs.org/sdr/2024F00303), Nov 21, 2024: FITTING. CORRODED. RH WING SPOILER HYDRAULIC LINE CARRY THRU FITTINGS ON AFT WING SPAR JUST INBD OF WING JACKING POINT HAS 2 CARRY THRU FITTINGS WITH CORROSION AROUND THEM. MECHAN - [SDR 2024F00301](https://openairdocs.org/sdr/2024F00301), Nov 21, 2024: STRINGER. CRACKED. REPAIRED CRACKED TAILCONE/STRINGER FIREWALL WEB CRACK PER NETJETS RFTS-112267. REV.0 TITLED "N315QS (680-0220) TAILCONE FIREWALL WEB CRACK" DATED 18NOV24. - [SDR 2024F00300](https://openairdocs.org/sdr/2024F00300), Nov 21, 2024: CONTROL CABLE. CHAFED. DURING TASK 27-60-00-2200, FOUND RH WING AILERON OUTPUT CABLE CHAFFING DRAIN TUBE NEXT TO SPOILER MIXER BOX. REMOVED EXISTING DRAIN TUBE FROM AIRCRAFT. REPAIRED - [SDR 2024F00299](https://openairdocs.org/sdr/2024F00299), Nov 21, 2024: STRINGER. CORRODED. STINGER HAS 1 AREA OF CORROSION ON LOWER AFT SIDE NEAR DRAIN HOLE. MECHANICALLY BLENDED 1 AREA OF CORROSION ON STINGER LOWER AFT SIDE NEAR DRAIN HOLE. EVALUATED - [SDR 2024F00298](https://openairdocs.org/sdr/2024F00298), Nov 21, 2024: HINGE. CORRODED. FOUND AN AREA OF CORROSION ON LOWER RUDDER HINGE. MECHANICALLY REMOVED 1 AREA OF CORROSION LOCATED ON RUDDER LOWER HINGE, AFT END, LH SIDE UPPER AREA. EVALUATED - [SDR 2024F00297](https://openairdocs.org/sdr/2024F00297), Nov 21, 2024: RIB. CORRODED. LH WING INBD FLAP COVE SUPPORT RIB HAS CORROSION WHERE HYD STAND-OFF BRACKET IS ATTACHED. MECHANICALLY REMOVED CORROSION LOCATED ON LH WING INBD FLAP COVE SUPPO - [SDR 2024F00302](https://openairdocs.org/sdr/2024F00302), Nov 21, 2024: FITTING. CORRODED. LH WING SPOILER HYDRAULIC LINE CARRY THRU FITTINGS ON AFT WING SPAR JUST INBD OF WING JACKING POINT HAS 2 CARRY THRU FITTINGS WITH CORROSION AROUND THEM. MECHAN - [SDR 2024FA0000859](https://openairdocs.org/sdr/2024FA0000859), Nov 21, 2024: SPAR. CORRODED. LH MLG WHEEL WELL AFT SPAR, FWD FACE HAS 1 AREA OF CORROSION INBD OF WS 37.00. MECHANICALLY REMOVED CORROSION LOCATED IN LH MLG WHEEL WELL, AFT SPAR, FWD FACE I - [SDR DXTA2023090594410](https://openairdocs.org/sdr/DXTA2023090594410), Sep 1, 2023: UNKNOWN. UNKNOWN. AVIONICS POWER: WITH THE MAIN POWER ON DURING FINAL DESCENT MY SIC IN THE RIGHT SEAT SMELLED A FAINT ELECTRICAL SMELL RIGHT BEFORE I DID. IT SEEMED TO GO AWAY A - [SDR DXTA2022112274220](https://openairdocs.org/sdr/DXTA2022112274220), Nov 21, 2022: SPRING. BROKEN. MAIN DOOR COUNTER WEIGHT SPRING BROKE UNABLE TO CLOSE DOOR WITHOUT HELP. REMOVED AND REPLACED MED FWD COUNTERBALANCE SPRING. PERFORMED RIGGING OF MED COUNTERBAL - [SDR DXTA2021121053290](https://openairdocs.org/sdr/DXTA2021121053290), Dec 9, 2021: NONE. NONE. RIGHT MLG BRAKE: RIGHT BRAKE REQUIRED MUCH GREATER THAN NORMAL APPLICATION FORCE BEFORE IT WOULD ENGAGE DURING LANDING ROLLOUT (REPORTED FROM RIGHT SEAT PILOT) - [SDR DXTA2021090948510](https://openairdocs.org/sdr/DXTA2021090948510), Sep 8, 2021: ENGINE. LEAKING. COCKPIT ODOR: ABNORMAL ODOR IN COCKPIT AT TAKEOFF POWER. LENGTHY 10-15 MIN TAXI WITH APU OFF. APPLIED TAKEOFF POWER AND WITHIN 5 SECS NOTED UNUSUALLY STRONG ABN - [SDR DXTA2021090748310](https://openairdocs.org/sdr/DXTA2021090748310), Sep 5, 2021: UNKNOWN. ODOR. COCKPIT ODOR: REPEAT WRITE UP. WITH APU OFF UNPLEASANT STRONG ABNORMAL ODOR IN COCKPIT AND CABIN AFTER TAKEOFF. ODOR WAS ENVIONMENTAL IN NATURE AND WAS STRONGES - [SDR DXTA2021090748150](https://openairdocs.org/sdr/DXTA2021090748150), Sep 3, 2021: CONDENSER. DIRTY. COCKPIT ODOR: UNPLEASANT UNUSUALLY STRONG ABNORMAL ODOR IN COCKPIT JUST AFTER TAKEOFF. ODOR SEEMED TO BE ENVIRONMENTAL, ALMOST OILY IN NATURE BUT NOT ELECTRICAL - [SDR JGVR20200303001](https://openairdocs.org/sdr/JGVR20200303001), Mar 3, 2020: NOT REPORTED. CORRODED. REPAIRED SPOTS OF CORROSION ON LH AND RH SIDES OF FORWARD DROPPED AISLE PER AEROSPACE QRD ERO-965791, TITLED "FUSELAGE REPAIR", DATED 27 FEB 2020 AND SUPPORTED - [SDR JGVR20180110001](https://openairdocs.org/sdr/JGVR20180110001), Jan 10, 2018: DOOR. CORRODED. EMERGENCY EXIT DOOR CORRODED BEYOND ECONOMIC REPAIR, REPLACED THE DOOR. - [SDR JGVR20180109001](https://openairdocs.org/sdr/JGVR20180109001), Jan 9, 2018: RIB. CORRODED. REPAIRED AREAS OF CORROSION ON LOWER FLANGE OF WING RIB P/N 6922037-20, AT WING STATION 18.50 IN RT MLG WELL PER ENGINEERING MEMO DQ10680M1, DATED JANUARY 5, 20 - [SDR JGVR20170915001](https://openairdocs.org/sdr/JGVR20170915001), Sep 15, 2017: STRUCTURE. CORRODED. EMERGENCY EXIT HAS CORROSION AROUND MULTIPLE NUT PLATES UNDER CONTOUR RING. BLENDED AREAS. PERFORMED EDDY CURRENT INSPECTION ON BLENDED AREAS. NO CRACKS OR CORR - [SDR DXTAT2PL6D0059SG2](https://openairdocs.org/sdr/DXTAT2PL6D0059SG2), Jul 24, 2017: UPLOCK SWITCH. OUT OF ADJUST. DURING TAKEOFF, THE GEAR HANDLE WAS PLACED IN THE FULL UP POSITION. ALL GREEN GEAR INDICATIONS EXTINGUISHED BUT THE RED UNLOCK LIGHT REMAINED ILLUMINATED. CHECK - [SDR DXTA2017033106391](https://openairdocs.org/sdr/DXTA2017033106391), Mar 31, 2017: APU. COKED. WHEN HEAT CAME ON AT CRUISE ALTITUDE, A VERY STRONG BURNED OIL ODOR COMES OUT OF THE VENTS. HAD TO TURN THE HEAT DOWN TO AN UNCOMFORTABLY COOLER TEMPERATURE TO - [SDR CWQR20131002041](https://openairdocs.org/sdr/CWQR20131002041), Sep 25, 2013: TUBE. CRACKED. DURING SCHEDULED INSPECTION, WE FOUND APU BLEED AIR TUBE ASSY CRACKED AT THE APU COMPARTMENT ATTACH FLANGE. THE FLANGE WAS CRACKED 2 TO 3" WHERE THE FLANGE IS W - [SDR DXTA2012043004966](https://openairdocs.org/sdr/DXTA2012043004966), Apr 27, 2012: HOSE. DAMAGED. DEPARTED, MOVED GEAR HANDLE TO UP, NOSE GEAR FAILED TO RETRACT FOLLOWED BY BOTH A HYD PRESSURE LOW LT AND HYD VOLUMN LOW AMBER CAS MESSAGES. RETURNED TO DEPARTU - [SDR 2011FA0000341](https://openairdocs.org/sdr/2011FA0000341), May 16, 2011: TUBE. CRACKED. FOUND SERVICE AIR TUBE ASSY CRACKED IN BEND RADIUS THAT LEADS TO THE RUDDER ACTUATOR IN THE TAIL - [SDR DXTA2009090803773](https://openairdocs.org/sdr/DXTA2009090803773), Sep 7, 2009: ENGINE. VIBRATION. RED ENGINE VIBRATION R CAS MSG POSTED REPEATEDLY FOR A FEW SECONDS EACH TIME AND THEN DISAPPEARED ( N1 96.3 , N2 95.4, FL 360, SAT -52*C , RAT -25*C , ISA +3) C - [SDR DXTA2008122303425](https://openairdocs.org/sdr/DXTA2008122303425), Dec 21, 2008: TIRE. FAILED. BOTH RIGHT MAIN TIRES BLEW ON LANDING. LEFT INBOARD MAIN TIRE FLAT. LEFT OUTBOARD MAIN TIRE FLAT. RIGHT MAIN GEAR DOOR DAMAGED ON LANDING. - [SDR DXTA20082907](https://openairdocs.org/sdr/DXTA20082907), Feb 1, 2008: UNKNOWN. UNKNOWN. AFTER DEPARTING, A CONTAMINATING RUNWAY GEAR UNLOCKED LIGHT, ILLUMINATED. CLEANED GEAR AND FLAP WELLS, INSPECTED, AND OPERATED SYSTEMS NUMEROUS TIMES WITH NO DE ## Service difficulty reports on N315QS not matched to an aircraft (9) They name N315QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR DXTA200702506](https://openairdocs.org/sdr/DXTA200702506), Sep 28, 2007: SWITCH. OUT OF ADJUST. ON TAKEOFF AT ROTATION, "CABIN DOOR" LIGHT CAME ON. ONCE ON THE GROUND WITH THE DOOR OPEN, LIGHT FLICKERED ON AND OFF SEVERAL TIMES. GAINED ACCESS TO THE CABIN - [SDR DXTA200702228](https://openairdocs.org/sdr/DXTA200702228), May 31, 2007: ENGINE. FLAMED OUT. DURING TAXI WHEN THE RT THROTTLE WAS ADVANCED, THEN MOVED TO IDLE, THE RT ENGINE FLAMED OUT. ADJUSTED RT THROTTLE IAW MM 76-11-00. OPS CK NORM. - [SDR DXTA200601660](https://openairdocs.org/sdr/DXTA200601660), Oct 16, 2006: BRAKE. MALFUNCTIONED. LEFT AND RIGHT BRAKES FROM BOTH SEATS FEEL SPONGY. THE LEFT BRAKE (BOTH SEATS) FEELS TO BE WORST THAN THE RIGHT. THE BRAKE WEAR INDICATOR ON THE LEFT MAIN ARE L - [SDR DXTA200601400](https://openairdocs.org/sdr/DXTA200601400), May 21, 2006: FCU. MISRIGGED. WHEN PERFORMING THE SPEED BRAKE TEST DURING THE (AFTER START) CHECKLIST, THE RT ENGINE SHUTS DOWN WHEN THE THROTTLE IS BROUGHT TO IDLE. ATTEMPTED THE TEST AGAIN - [SDR DXTA200500733](https://openairdocs.org/sdr/DXTA200500733), May 21, 2005: WIRE. BURNED. DURING POSTFLIGHT, SMELLED ACRID ELECTRICAL SMELL INSIDE NOSE BAGGAGE COMPARTMENT. SMELL CAME FROM BEHIND PANEL ON AFT SIDE OF NOSE BAGGAGE COMPARTMENT. PERFORM - [SDR DXTA200500508](https://openairdocs.org/sdr/DXTA200500508), Jan 3, 2005: SEAL. MALFUNCTIONED. ON TAKEOFF HEARD A POPING NOISE FOLLOWED BY A DOOR SEAL LIGHT AND CABIN DOOR LIGHT. INSPECTED DOOR SEAL AS REQUIRED. PURGED SERVICE AIR SYSTEM AND DOOR SEAL WIT - [SDR DXTA200400390](https://openairdocs.org/sdr/DXTA200400390), Sep 12, 2004: B-NUT. LOOSE. DURING TAXI ON CO-PILOTS SIDE, LT BRAKE PEDAL GOES NEARLY TO THE FLOOR BEFORE BRAKING ACTION IS FELT. INSPECTED ALL BRAKE MASTER CYLINDERS, FOUND PILOT LT PEDAL - [SDR DXTA200400251](https://openairdocs.org/sdr/DXTA200400251), Feb 22, 2004: HOSE. LEAKING. ON LANDING NOTICED NO BRAKING FORCE WITH THE RIGHT BRAKE PEDAL, ON POST FLIGHT INSPECTION FOUND BRAKE FLUID VISIBLY LEAKING FROM RIGHT MAIN WHEEL ASSEMBLY. JACK - [SDR 97ZZZX2828](https://openairdocs.org/sdr/97ZZZX2828), May 14, 1997: SKIN. CRACKED. FOUND CRACK ON RIGHT SIDE LOWER RUDDER SKIN. THIS IS THE 2ND TIME A CRACK HAS BEEN FOUND IN THIS AREA ON THIS PARTICULAR RUDDER. THE FIRST WAS AT 718.2 HOURS TO ## 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.