# N683QS: 2006 Cessna 560XL - Status: Valid registration - Airframe: [Cessna 560XL](https://openairdocs.org/model/cessna-560xl) (registry code 2076702, 13 seats) - Engine: [Pratt & Whitney Canada PW545B](https://openairdocs.org/engine/pratt-whitney-canada-pw545b) (registry code 52186) - Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE) (Textron Aviation Inc.), [TCDS E00059EN](https://openairdocs.org/tcds/E00059EN) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: 560-5643 - Year built: 2006 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 27, 2006 - Certificate issued: July 13, 2022 - Expires: July 31, 2029 - Mode S code: A90FCB - Registered owners: [Netjets Sales Inc](https://openairdocs.org/faa-owner/NETJETS%20SALES%20INC), [Netjets Aviation Inc](https://openairdocs.org/faa-owner/NETJETS%20AVIATION%20INC) - Location: [Columbus, OH](https://openairdocs.org/faa-place/OH/Columbus) - Owner type: Co-owned - Owner's area on the map: 40.0074° N, 82.9207° W: Placed by OpenAirDocs at the center of ZIP code 43219, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=683QS - Page: https://openairdocs.org/aircraft/N683QS 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): 19 in force ### Matched by airframe (Cessna 560XL) - [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 2025-11-09](https://openairdocs.org/ad/2025-11-09): Fire Protection · Textron 560 and 560XL. Effective Jul 11, 2025 - [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 2020-26-05](https://openairdocs.org/ad/2020-26-05): POWER LEVER · Textron 560XL. Effective Dec 17, 2020 - [AD 2017-04-14](https://openairdocs.org/ad/2017-04-14): Electrical power · Textron 560XL. Effective Mar 9, 2017 - [AD 2012-26-15 R1](https://openairdocs.org/ad/2012-26-15-R1): Navigation · Agusta AW139, A318-111, A318-112 and 70 more. Effective Dec 3, 2014 - [AD 2014-18-01](https://openairdocs.org/ad/2014-18-01): Navigation · Bombardier ATR42-200, ATR42-300, ATR42-320 and 23 more. Effective Oct 14, 2014 - [AD 2013-09-11](https://openairdocs.org/ad/2013-09-11): Air Conditioning · Cessna 500, 501, 550 and 5 more. Effective Jul 5, 2013 - [AD 2012-09-01](https://openairdocs.org/ad/2012-09-01): Landing Gear · Cessna 560XL. Effective Jun 7, 2012 - [AD 2012-06-01](https://openairdocs.org/ad/2012-06-01): Fuselage · Cessna 560XL. Effective Apr 25, 2012 - [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010 - [AD 2007-11-17](https://openairdocs.org/ad/2007-11-17): Wires for the positive and negative terminal studs of the engine and/or auxiliary power unit (APU) fire extinguishing bottles. · Cessna 500, 501, 550 and 5 more. Effective Jul 6, 2007 - [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001 - [AD 2001-14-09](https://openairdocs.org/ad/2001-14-09): Wiring of the Landing Light Switch and theJ-Box Fairing Light Relays · Cessna 560XL. Effective Jul 26, 2001 - [AD 2000-15-51](https://openairdocs.org/ad/2000-15-51): Aileron Cable Fairlead Tube and Aileron Cable Sector · Cessna 560XL. Effective Aug 14, 2000 - [AD 2000-03-09](https://openairdocs.org/ad/2000-03-09): Residual Ice · Cessna 560 and 560XL. Effective Apr 3, 2000 - [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998 - [AD 94-01-04](https://openairdocs.org/ad/94-01-04): Traffic Alert and Collision Avoidance System · Airbus A300 B4-601, A300 B4-603, A300 B4-605R and 136 more. Effective Feb 4, 1994 ### Matched by engine (Pratt & Whitney Canada PW545B) - [AD 2010-18-09](https://openairdocs.org/ad/2010-18-09): Bleed valve/servo valve · Pratt & Whitney Canada PW545A, PW545B and PW530A. Effective Sep 10, 2010 ### Historical (superseded or no longer in force) - [AD 2012-26-15](https://openairdocs.org/ad/2012-26-15) (historical): Navigation · Agusta AW139, A318-111, A318-112 and 71 more. Effective Jan 24, 2013 - [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006 - [AD 2006-04-10](https://openairdocs.org/ad/2006-04-10) (historical): Identification sleeves · Cessna Aircraft Company, The 500, 550, 560 and 3 more. Effective Mar 24, 2006 ## Information bulletins (advisory) (4 in force) - [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021 - [SAIB CE-10-29R1](https://openairdocs.org/saib/CE-10-29R1): Lights Aft Side Ledger Divider Light. Issued May 21, 2010 - [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010 - [SAIB 2024-06](https://openairdocs.org/saib/2024-06): Oil Servicing Issues on Pratt & Whitney Canada PW545 Series Engines. Issued Nov 18, 2024 - [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021 - [SAIB CE-10-29](https://openairdocs.org/saib/CE-10-29) (historical): Lights Aft Side Ledger Divider Light. Issued Apr 28, 2010 ## NTSB investigations None matched to N683QS. ## FAA accident and incident reports None matched to N683QS. ## Service difficulty reports (34) 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 DXTA2026031607239](https://openairdocs.org/sdr/DXTA2026031607239), Mar 12, 2026: CONTROLLER. DEFECTIVE. ON TAKEOFF WE SELECTED GEAR UP AND THE LANDING GEAR WOULD NOT RETRACT . THEN THE GEAR HANDLE WOULD NOT GO BACK TO THE GEAR DOWN POSITION . WE RAN THE CHECKLIST - [SDR DXTA2025122406243](https://openairdocs.org/sdr/DXTA2025122406243), Dec 21, 2025: BULB. UNSECURE. SEAT NR 7 EMERGENCY EXIT LIGHT. READING LIGHT INOPERATIVE. TROUBLESHOT AS REQUIRED, FOUND SEAT NR 7 READING & EMER EXIT LIGHT BULB TO BE LOOSE, SECURED BULB. OP - [SDR DXTA2025120305919](https://openairdocs.org/sdr/DXTA2025120305919), Nov 30, 2025: LIGHT. INOPERATIVE. EMERGENCY LIGHTS OVER THE LAV ARE INOP. REMOVED INOP LAV EMERGENCY LIGHT AND REPLACED LAV EMERGENCY LIGHT WITH CUSTOMER SUPPLIED PART IAW CESSNA 560XL AMM CH.33 - [SDR DXTA2025102705416](https://openairdocs.org/sdr/DXTA2025102705416), Oct 23, 2025: LINKAGE. FAULTED. MAIN CABIN DOOR HANDLE WILL NOT MOVE TOWARD THE LOCK POSITION. YOU CAN NOT CLOSE AND LOCK THE DOOR. REMOVED, REPLACED, AND ADJUSTED SPADE DOOR LINKAGE IAW 560XL - [SDR DXTA2025100305178](https://openairdocs.org/sdr/DXTA2025100305178), Oct 2, 2025: DISPLAY. INOPERATIVE. AFTER TAKE OFF-APPROX. 1500 FEET AGL BOTH LT SEAT PFD & MFD DISPLAYS FAILED. WE RETURNED TO THE FIELD. PERFORMED THE OPS CHECKS FOR THE IC-615 COMPUTER WITH STA - [SDR DXTA2025032502788](https://openairdocs.org/sdr/DXTA2025032502788), Mar 22, 2025: CONTROL CABLE. OUT OF ADJUST. HIGH VIBE IN YOKE AND PEDALS STARTING AT 250KTS. INCREASED INTENSITY AS SPEED INCREASED. CHECKED ELEVATOR AFT CONTROL CABLE TENSIONS, TENSIONS WERE WITHIN LIMIT - [SDR DXTA2025022402442](https://openairdocs.org/sdr/DXTA2025022402442), Feb 20, 2025: SOLENOID. FAULTY. MAIN DOOR: MAIN CABIN DOOR WAS STUCK IN THE CLOSED POSITION. WHEN ATTEMPTING TO OPEN THE DOOR, THE LEVER WOULD MOVE TO THE OPEN POSITION, BUT THE DOOR WOULD NOT - [SDR DXTA2025022002442](https://openairdocs.org/sdr/DXTA2025022002442), Feb 20, 2025: SEAL. DETACHED. MAIN DOOR: MAIN CABIN DOOR WAS STUCK IN THE CLOSED POSITION. WHEN ATTEMPTING TO OPEN THE DOOR, THE LEVER WOULD MOVE TO THE OPEN POSITION, BUT THE DOOR WOULD NOT - [SDR DXTA2024060311958](https://openairdocs.org/sdr/DXTA2024060311958), Jun 2, 2024: HANDLE. UNKNOWN. UPON CLOSING MAIN CABIN DOOR AND ALL SEEMS NORMAL FLAGS AND LIGHTS. OUTSIDE HANDLE GOES FROM SEATED TO OUT OF POSITION. NO INDICATIONS EXCEPT OUTSIDE VIEW. REMO - [SDR DXTA2023111410048](https://openairdocs.org/sdr/DXTA2023111410048), Nov 13, 2023: LIGHT. DEFECTIVE. FLOOR EMERG EXIT LIGHT: ON PREFLIGHT, FORWARD LEFT FLOOR EMERGENCY LIGHTING HAS A STRIP APPRXIMATELY 8-9 INCHES LONG NOT WORKING. NO LIGHTS IN THAT SEGMENT WORK - [SDR DXTA2023110699810](https://openairdocs.org/sdr/DXTA2023110699810), Nov 5, 2023: BATTERY. INOPERATIVE. DURING PREFLIGHT INSPECTION FOUND AFT CABIN EMERGENCY LIGHTING IS INOPERATIVE. EXTERIOR EMERGENCY LIGHTING IS ALSO INOPERATIVE. FOUND ORIGINAL AFT BATTERY WAS D - [SDR DXTA2023072691740](https://openairdocs.org/sdr/DXTA2023072691740), Jul 25, 2023: UNKNOWN. UNKNOWN. APU (EXCEPT GENERATOR): AFTER TAKE STRONG SMELL IN AC MORE LIKE BURNING OIL OR CLEANING FLUID. SHUT DOWN APU SMELL WENT AWAY. AFTER LANDING STARTED APU SMELL RE - [SDR DXTA2023032182950](https://openairdocs.org/sdr/DXTA2023032182950), Mar 20, 2023: UNKNOWN. UNKNOWN. FLOOR EMERG EXIT LIGHT: FORWARD LEFT EMERGENCY FLOOR LIGHTING HAS A SECTION OF ABOUT 18" THAT IS NOT FUNCTIONAL. IN THAT 18" RUN, THERE ARE 3 LED'S THAT ARE WOR - [SDR DXTA2022122776920](https://openairdocs.org/sdr/DXTA2022122776920), Dec 22, 2022: LIGHT. INOPERATIVE. THE SINGLE ENGINE INSTRUMENT SPOTLIGHT IN THE ENGINE FIRE TRAY UNDER THE GLARESHIELD BETWEEN THE STANDBY INSTRUMENT AND THE ENGINE AMLCD IS INOPERATIVE. REMOVED - [SDR DXTA2022110773370](https://openairdocs.org/sdr/DXTA2022110773370), Nov 5, 2022: BATTERY PACK. NO TEST. RIGHT EXTERIOR EMERG LIGHT: AFTER SHUTDOWN, EXTERIOR LIGHTS CHECK WAA DONE. BATTERY WAS TURNED OFF BEFORE EMERGENCY LIGHTS SWITCH WAS TURNED TO OFF AND THE THRE - [SDR DXTA2021082347400](https://openairdocs.org/sdr/DXTA2021082347400), Aug 21, 2021: CONDENSER. ODOR. DURING FLT, WHEN CKPT TEMP SEL TURNED FROM FULL COLD TOWARDS HOT, A EXHAUST/FUEL ODOR DETECTED. ODOR BECOMES MORE PRONOUNCED AS AIR GETS WARM. TURNED SELECTOR B - [SDR DXTA2019121703213](https://openairdocs.org/sdr/DXTA2019121703213), Dec 17, 2019: SENSOR. DEFECTIVE. COCKPIT ODOR - VERY STRONG, ACRID ODOR COMING FROM THE AIR CONDITIONING SYSTEM. REMOVED PRECOOLER TEMP SENSOR AND INSTALLED NEW SERVICEABLE TEMP SENSOR AND PERF - [SDR DXTA2019112103110](https://openairdocs.org/sdr/DXTA2019112103110), Nov 21, 2019: LANDING GEAR. UNKNOWN. NLG INDICATOR LIGHT INTERMITTENT - ON APPROACH LANDING GEAR DOWN WAS SELECTED. THE NOSE GEAR DID NOT ILLUMINATE. THE RED UNLOCK LIGHT DID EXTINGUISH. FLAPS WERE - [SDR DXTA2019102402972](https://openairdocs.org/sdr/DXTA2019102402972), Oct 22, 2019: SENSOR. UNKNOWN. LEFT ENGINE ENGINE OIL TEMPERATURE INDICATION HIGH TEMPERATURE - #1 OIL TEMPERATURE FLUCTUATION. DURING CLIMB (PASSING 35,000?) WITH THROTTLE IN CLIMB DETENT, # - [SDR DXTA201632306208](https://openairdocs.org/sdr/DXTA201632306208), Mar 23, 2016: PRESSURE SWITCH. UNSERVICEABLE. UPON LIFT OFF THE ACFT HAD EXCESSIVE PITCH UP. IT REQUIRED EXCESSIVE FULL FWD YOLK PRESS TO MAINTAIN LEVEL FLIGHT & FULL NOSE DOWN TRIM. TROUBLE SHOT EXCESSIVE - [SDR DXTA2016032306208](https://openairdocs.org/sdr/DXTA2016032306208), Mar 23, 2016: UNKNOWN. NOT REPORTED. UPON LIFT OFF THE ACFT HAD EXCESSIVE PITCH UP. IT REQUIRED EXCESSIVE FULL FWD YOLK PRESS TO MAINTAIN LEVEL FLIGHT & FULL NOSE DOWN TRIM. - [SDR DXTA2014052005777](https://openairdocs.org/sdr/DXTA2014052005777), May 19, 2014: BRAKE SYS. UNKNOWN. AFTER LANDING AND DURING TAXING ONTO RAMP, THE RT BRAKE ON MAIN GEAR WAS HANGING UP WHEN THE BRAKE PEDAL WAS PUSHED. ACFT WOULD SHAKE & SHUTTER. HAPPENED 5 TO 6 - [SDR DXTA2014041605733](https://openairdocs.org/sdr/DXTA2014041605733), Apr 15, 2014: CONTROL UNIT. MALFUNCTIONED. ON LANDING THERE WAS A STRONG JOLT FROM THE RT BRAKE WHEN TAXIING WITH EQUAL PRESSURE, THE ACFT PULLS HARD TO THE LT, IT FEELS LIKE THERE IS NO RT BRAKING. COMP - [SDR DXTA2014032505698](https://openairdocs.org/sdr/DXTA2014032505698), Mar 24, 2014: CLEVIS. OUT OF ADJUST. DURING LANDING WITH ONLY LIGHT TO MODERATE PRESSURE APPLIED TO THE BRAKES, IT FELT AS THOUGHT THE LT BRAKE WAS GRABBING EXCESSIVELY. THIS OCCURRED INTERMITTENTL - [SDR DXTA2014031005679](https://openairdocs.org/sdr/DXTA2014031005679), Mar 8, 2014: BRAKE SYS. MALFUNCTIONED. AFTER LANDING & DURING TAXI WHEN BRAKES WERE APPLIED, THE ACFT JERKED HARD TO THE LEFT. FELT LIKE THE LEFT WHEEL LOCKED THEN A PULSE FEELING IN THE BRAKE PEDAL - [SDR DXTA2013102905550](https://openairdocs.org/sdr/DXTA2013102905550), Oct 14, 2013: ACTUATOR. FROZEN. AFTER BEING AT ALTITUDE FOR APPROXIMATELY 45 MINS THE ELECTRIC AND MANUAL PITCH TRIM FROZE UP, IT BROKE FREE WHILE DESCENDING THROUGH THE LOW 20'S. SUP: R &R LT - [SDR DXTA2013093005522](https://openairdocs.org/sdr/DXTA2013093005522), Sep 29, 2013: VALVE. MALFUNCTIONED. ON TAXI OUT, EXPERIENCED AN AGGRESSIVE GRABBING OF THE RT BRAKE. BOTH THE LT AND RT PILOT STATIONS HAD SAME RESULTS. REMOVED AND REPLACED BRAKE METERING UNIT AN - [SDR DXTA2013092405517](https://openairdocs.org/sdr/DXTA2013092405517), Sep 23, 2013: METERING VALVE. MALFUNCTIONED. BRAKES ARE GRABBING VIOLENTLY DURING TAXI, BOTH RT AND LT BRAKE, FROM EITHER PILOTS BRAKE PEDALS. R & R THE BRAKE METERING VALVE. BLED SYS. OPS AND LEAK CHECKS - [SDR DXTA2013050605377](https://openairdocs.org/sdr/DXTA2013050605377), May 7, 2013: BRAKE SYS. MALFUNCTIONED. DURING TAXI INTO RAMP BRAKES STARTED GRABBING ABRUPTLY. COULD NOT TELL WHICH MAIN BRAKE. - [SDR DXTA2012071205046](https://openairdocs.org/sdr/DXTA2012071205046), Jul 11, 2012: BRAKE ASSY. MALFUNCTIONED. DURING SLOW SPEED TAXI AFTER CLEARING RUNWAY, ACFT SHUDDERED VIOLENTLY ABOUT 4 TIMES AS IF THE BRAKES WERE GRABBING. AFTER SOME DISCUSSION ABOUT POSSIBLE FLAT T - [SDR DXTA2010072104165](https://openairdocs.org/sdr/DXTA2010072104165), Jul 20, 2010: VALVE. MALFUNCTIONED. WHILE LEVELING AT 5000 FT RT ENGINE "EEC MANUAL" LIGHT ILLUMINATED. APPROX 30 SEC LATER THE ITT REDLINED. UPON POWER REDUCTION ENGINE BEGAN TO VIBRATE. PERFORME - [SDR DXTA2009112403868](https://openairdocs.org/sdr/DXTA2009112403868), Nov 23, 2009: BRAKE ASSY. MALFUNCTIONED. AFTER LANDING DURING TAXI, AIRCRAFT'S RIGHT BRAKE LOCKED MULTIPLE TIMES; VERY HEAVY LURCHING TO THE RIGHT. LIGHT PRESSURE TO NO PRESSURE WAS APPLIED TO BRAKE PE - [SDR DXTA2009111603859](https://openairdocs.org/sdr/DXTA2009111603859), Nov 15, 2009: BRAKE. LOCKED. AFTER LANDING, DURING TAXI INTO THE RAMP, THE RT BRAKE LOCKED UP 3 SEPARATE TIME WITH LITTLE OR NO PRESSURE ON THE RT PEDAL. JERKED ACFT TO THE RT. TAXIED AIRCR - [SDR DXTA200702276](https://openairdocs.org/sdr/DXTA200702276), Jun 16, 2007: INDICATOR. INOPERATIVE. RT MLG INDICATOR LIGHT DID NOT ILLUMINATE WHEN GEAR LOWERED. PULLED T-HANDLE, BUT DID NOT BLOW GEAR DOWN. [07-11-07] REMOVED AND REPLACED RIGHT MAIN GEAR BULB I ## STCs that may be installed (OpenAirDocs) (114, first 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 560XL) - [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC ST01823WI](https://openairdocs.org/stc/ST01823WI): Installation of Garmin GTS Traffic Sensor with Garmin GTX 3000 Mode S Transponders with ADS-B Out. Blackhawk Aerospace Technologies Inc - [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc - [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 SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc - [STC ST02016WI](https://openairdocs.org/stc/ST02016WI): Installation of the Meggitt Wireless Tire Pressure Sensor. 3S Certification LLC - [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC - [STC ST00390BO](https://openairdocs.org/stc/ST00390BO): Installation of a SmartSky Networks Air to Ground Data Link System. Apcela IFC JV, LLC dba Apcela ATG - [STC ST04604CH](https://openairdocs.org/stc/ST04604CH): INSTALL SMARTSKY FLAGSHIP SYSTEM. Apcela IFC JV, LLC dba Apcela ATG - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc - [STC ST02718LA](https://openairdocs.org/stc/ST02718LA): Modification to replace the existing standby instrument. Acron Aviation Inc - [STC ST03292CH](https://openairdocs.org/stc/ST03292CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development, Inc - [STC ST12042WI](https://openairdocs.org/stc/ST12042WI): Upgrade of AirCell High Speed Internet System to Gogo Business Aviation C1 System. Duncan Aviation Inc - [STC ST09854AC](https://openairdocs.org/stc/ST09854AC): Installation of a Lumin Media Server. L2 Aviation - [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 ST04730NY](https://openairdocs.org/stc/ST04730NY): Installation of Battery Temperature Indicator. Aero-Mach Labs Inc - [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine - [STC ST02804SE](https://openairdocs.org/stc/ST02804SE): Installation of Starlink Aviation System. AeroMech Incorporated - [STC ST01979WI](https://openairdocs.org/stc/ST01979WI): Installation of Gogo Business Aviation AVANCE L5/X3 System or optional AVANCE LX5 System. Gogo Business Aviation LLC - [STC ST04742NY](https://openairdocs.org/stc/ST04742NY): Installation of SkyVue 1000 Cockpit Upgrade including dual Avidyne IFD540 FMS with LPV i. Aerospace Design & Compliance LLC - [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc - [STC ST01918WI](https://openairdocs.org/stc/ST01918WI): Installation of Garmin G5000 Integrated Flight Deck. Garmin International Inc - [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC - [STC ST01083DE](https://openairdocs.org/stc/ST01083DE): Installation of the Aviation Clean Air Airborne Air & Surface Purification System. Lee Aerospace, Inc - [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 ST02427LA](https://openairdocs.org/stc/ST02427LA): Installation of Dual Garmin GTN 6XX/7XX Series Global Navigation System with Structural Antenna and WAAS approval; Garmin GMA 35 Audio Panel; and Dual Garmin GTX 33 Mode S Transponders, Weather Radar, and ADS-B Link. JETTECH LLC - [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. 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 ST02029WI](https://openairdocs.org/stc/ST02029WI): Installation of Garmin GI 275 Standby Instrument and GSB 15 USB Port. Blackhawk Aerospace Technologies - [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited - [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine - [STC ST00011WI](https://openairdocs.org/stc/ST00011WI): Installation of Concorde RG380E/40 and 40B battery. Aero-Mach Wilco LLC - [STC ST11285DS](https://openairdocs.org/stc/ST11285DS): An update to the existing Collins Aerospace Integrated Flight Information System (IFIS) FSU-5010 and upgrade the existing XMWR-1000 to a XMWR-1000S (Sirius XM) in Part 25. BHE & Associates Ltd - [STC ST03035NY](https://openairdocs.org/stc/ST03035NY): Replacement of certain Goodrich pneumatic deicer boots. SMR Technologies Inc - [STC ST04258CH](https://openairdocs.org/stc/ST04258CH): Installation of Gogo Business Aviation Avance High Speed Data System. Ross Aviation Flight Maintenance - [STC ST00411BO](https://openairdocs.org/stc/ST00411BO): Installation of Avidyne GPS/Nav/Com. Avidyne Corporation - [STC ST01916WI](https://openairdocs.org/stc/ST01916WI): Installation of Beijing Sky Aviation Chinese Flight Inspection System. Duncan Aviation Inc - [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC - [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc - [STC ST00953DE](https://openairdocs.org/stc/ST00953DE): Installation of a cabin emergency lighting. West Star Aviation - [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 ST00158BO](https://openairdocs.org/stc/ST00158BO): Installation of Universal Avionics Systems Corporation (UASC) Flight Management System (FMS). Pro Star Aviation, LLC - [STC ST04416CH](https://openairdocs.org/stc/ST04416CH): Install Mid-Continent Instruments MD-302 Standby Instrument. Elliott Aviation Technical Products Development Inc - [STC ST00934DE](https://openairdocs.org/stc/ST00934DE): Installation of Becker Avionics BXT6553 transponder. Peregrine - [STC ST01780LA](https://openairdocs.org/stc/ST01780LA): Installation of a Patient Loading and Utility System. 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 ST01138CH](https://openairdocs.org/stc/ST01138CH): Install air ambulance conversion. Spectrum Aeromed LLC dba Spectrum Aeromed - [STC ST00883DE](https://openairdocs.org/stc/ST00883DE): Installation of Grumman LitefLCR-100 Attitude Heading and Reference System (AHRS) in place of existing LCR-93 AHRS. Peregrine All 114: https://openairdocs.org/aircraft/N683QS/stcs.md ## Related - Other Cessna 560XL aircraft: https://openairdocs.org/model/cessna-560xl/aircraft.md - The Pratt & Whitney Canada PW545B engine: https://openairdocs.org/engine/pratt-whitney-canada-pw545b.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.