# N568QS: 2008 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: 560-5829 - Year built: 2008 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 31, 2008 - Certificate issued: July 28, 2022 - Expires: July 31, 2029 - Mode S code: A74611 - 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, fractional ownership - 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=568QS - Page: https://openairdocs.org/aircraft/N568QS 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 N568QS. ## FAA accident and incident reports None matched to N568QS. ## Service difficulty reports (31) 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 DXTA2026090209508](https://openairdocs.org/sdr/DXTA2026090209508), Aug 31, 2026: INDICATOR. MALFUNCTIONED. MAIN CABIN DOOR ANNUNCIATOR REMAINS ILLUMINATED WITH DOOR FULLY CLOSED. - [SDR DXTA2026011306521](https://openairdocs.org/sdr/DXTA2026011306521), Jan 11, 2026: HAND RAIL. OUT OF ADJUST. MAIN ENTRANCE DOOR HANDRAIL IS HITTING THE DOOR AND CAUSING DAMAGE WHEN DOOR IS CLOSED. WHEN DOOR IS OPEN, HANDRAIL IS LOWER THAN NORMAL. HANDRAIL IS ONE OR TWO - [SDR DXTA2025120105879](https://openairdocs.org/sdr/DXTA2025120105879), Nov 28, 2025: HYDRAULIC SYSTEM. FAULTED. AT GEAR DOWN SELECTION EVERYTHING APPEARED TO OPERATE NORMAL. ON SHORT FINAL WE HAD A ANTISKD INOP. LANDED AND AFTER EXITING THE RUNWAY ON THE TAXIWAY HAD A LO - [SDR DXTA2025091504937](https://openairdocs.org/sdr/DXTA2025091504937), Sep 11, 2025: FIRE LOOP. OUT OF POSITION. THE RT ENGINE FIRE DETECTION LIGHT BEGAN TO FLICKER THE LAST FIFTEEN MINUTES OF THE FLIGHT. NO SIGNS OF AN ENGINE FIRE WERE PRESENT. ARRIVED ON SITE AND NEW COW - [SDR DXTA2025051903528](https://openairdocs.org/sdr/DXTA2025051903528), May 16, 2025: PRECATCH. OUT OF ADJUST. MAIN DOOR: CREW LEFT AIRPLANE AND WENT INSIDE FBO. WHEN WE RETURNED, WE WERE UNABLE TO OPEN THE MAIN DOOR. THE HANDLE ACTUATES CORRECTLY WITH NO BINDING. CREW W - [SDR JGVR202407220003](https://openairdocs.org/sdr/JGVR202407220003), Jul 22, 2024: DOOR FRAME. CHAFED. PERFORM REPAIR TO EMERGENCY EXIT DOUBLER CHAFE LOCATIONS. PER: ERO-980291. PERFORMED REPAIRS TO 5 EACH CHAFE LOCATIONS IN CABIN SURROUNDING EMERGENCY EXIT AND L - [SDR DXTA2024031811226](https://openairdocs.org/sdr/DXTA2024031811226), Mar 16, 2024: DOOR. BINDING. MAIN DOOR: DURING CLOSURE OF CABIN DOOR FROM THE INSIDE THE HANDLE IS TOUGH TO GET TO RETURN TO CENTER, THEN BECOMES EXCESSIVILY LOOSE CAUSING AN OVERSHOOT OF T - [SDR DXTA2024031811225](https://openairdocs.org/sdr/DXTA2024031811225), Mar 16, 2024: SUPPORT. DAMAGED. MAIN DOOR TELESCOPING ROD: CREWMEMBER FELL DISEMBARKING FROM AIRCRAFT AND KINCKED AFT TELESCOPING ROD ON CABIN DOOR. SMALL DIAMETER SECTION OF ROD NOW JAMS AND - [SDR DXTA2023112010083](https://openairdocs.org/sdr/DXTA2023112010083), Nov 18, 2023: UNKNOWN. UNKNOWN. RIGHT ENGINE ENGINE SLOW ACCELERATION: ON TAKE OFF THERES A LAG OF N1 FOR A FEW SECONDS CAUSING AIRCRAFT TO DRIFT RIGHT AND MORE LEFT RUDDER IS NEEDED UNTIL SPO - [SDR DXTA2023092696430](https://openairdocs.org/sdr/DXTA2023092696430), Sep 25, 2023: MOTOR. FAILED. WHILE HOLDING SHORT OF RUNWAY, HEARD A POP COME FROM LT CIRCUIT BREAKER PANEL. WAS THE POWER BRKS CIRCUIT BREAKER. LOOKED UP AT ANNUNCIATOR PANEL & ANTI-SKID IN - [SDR DXTA2023091895550](https://openairdocs.org/sdr/DXTA2023091895550), Sep 16, 2023: BATTERY. DEFECTIVE. INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTING IS INOP. CONNECTED GPI) & ALLOW FOR BATTERIES TO CHARGE. PERFORMED EMER LIGHT APS TEST AND FAILED ALMOST IMMEDIATE - [SDR DXTA2023071791090](https://openairdocs.org/sdr/DXTA2023071791090), Jul 16, 2023: SOLENOID. DEFECTIVE. MAIN DOOR: DURING LATCHING OF MAIN CABIN DOOR THERE IS A METAL ON METAL SOUND . IT OCCURS DURING CLOSING AND OPENING. IN ADDITION THE CENTER LOWER 6 PACK LIGHT - [SDR DXTA2023070790520](https://openairdocs.org/sdr/DXTA2023070790520), Jul 7, 2023: CABLE. DAMAGED. MAIN DOOR: MAIN CABIN DOOR ON OPENING, DOOR FALLS WITH VERY LITTLE TENSION UNTIL NEARLY 3/4 WAY OPEN. VERY DIFFICULT TO CLOSE. GAINED ACCESS TO COUNTER BALANCE - [SDR DXTA2022081568060](https://openairdocs.org/sdr/DXTA2022081568060), Aug 16, 2022: BATTERY. DEFECTIVE. CABIN EMERG LIGHT: WITH THE BATTERY SWITCH OFF THE AFT EMERGENCY LIGHTS INCLUDING THE OVER WING LIGHTS ARE INOP. WITH THE BATTERY SWITCH ON ALL EMERGENCY LIGHTS - [SDR DXTA2021092349280](https://openairdocs.org/sdr/DXTA2021092349280), Sep 22, 2021: NONE. NONE. MAIN DOOR CABLE: THE MAIN CABIN DOOR IS VERY HARD TO OPEN. IT CAN NOT JUST BE OPENED BY LOWERING THE HANDLE. ADDITIONAL FORCE NEEDS TO BE USED TO OPEN THE DOOR. - [SDR DXTA2020121104454](https://openairdocs.org/sdr/DXTA2020121104454), Dec 11, 2020: CONDENSER. DIRTY. WITH APU RUNNING AND SERVICE AIR ON HOT AN ACRID BURNING PLASTIC SMELL MID CABIN WAS NOTICED. SERVICE AIR WAS THEN TURNED OFF AND CABIN DOOR OPENED TO VENT SO A - [SDR JGVR20200327001](https://openairdocs.org/sdr/JGVR20200327001), Mar 27, 2020: HINGE. CORRODED. MAIN ENTRY DOOR LH HINGE HALF COMMON TO AIRFRAME IS CORRODED ON AFT UPPER CORNER. FOUND DURING 600 HOUR CABIN DOOR INSPECTION. REMOVED MAIN ENTRY DOOR FORWARD H - [SDR 2019FA0000220](https://openairdocs.org/sdr/2019FA0000220), Jul 11, 2019: PANEL. CRACKED. LEFT WING EXHAUST VENT DOOR DAMAGE (LOUVER CRACKED). ACCOMPLISHED ENGINEERING LETTER DQ22153M1 REV A DATED JULY 10, 2019; 560-5829 (N568QS) LEFT WING EXHAUST VE - [SDR 2019F00236](https://openairdocs.org/sdr/2019F00236), Jul 10, 2019: DUCT. DAMAGED. COCKPIT FOOT WARMER DUCT (LEFT SIDE) DAMAGE. - [SDR DXTA2018052200985](https://openairdocs.org/sdr/DXTA2018052200985), May 21, 2018: UNKNOWN. ODOR. WHEN THE COCKPIT TEMP SELECTOR WAS MOVED TO WARM (10 O'CLOCK POSITION), THERE WAS AN OIL ODOR IN THE COCKPIT. REMOVED AND REPLACED CONDENSER BAG. INSPECTED BLEE - [SDR EBVR20161104001](https://openairdocs.org/sdr/EBVR20161104001), Nov 4, 2016: SKIN. CRACKED. CRACK IN LEADING EDGE RUDDER SKIN RT SIDE JUST BELOW TOP HINGE. REMOVED THE RUDDER UPPER LEADING EDGE SKIN AND INSTALLED NEW . ALL WORK WAS DONE IAW SRM 51-40-0 - [SDR DXTA2015041306004](https://openairdocs.org/sdr/DXTA2015041306004), Apr 11, 2015: ENGINE. FAILED. RIGHT ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED WITH THE MASTER WARNING LIGHT CLIMBING THROUGH ABOUT 3000 FT. THE OIL PRESSURE GAUGE INDICATED BELOW 20 PS - [SDR DXTA2015041306005](https://openairdocs.org/sdr/DXTA2015041306005), Apr 11, 2015: UNKNOWN. SMOKE. SMOKE WAS NOTICED IN THE CABIN & COCKPIT. ONCE THE POWER WAS REDUCED THE SMOKE SEEMED TO DISSIPATE. - [SDR DXTA2014041405729](https://openairdocs.org/sdr/DXTA2014041405729), Apr 13, 2014: CONTROL ROD. BINDING. AFTER TAKEOFF, GEAR SELECTED UP, THREE GREEN LIGHTS OUT & RED UNLOCK LIGHT REMAINS ON. STAB INCOMPARABLE & HYD PRESSURE LIGHT REMAINED ON. AFTER APPROXIMATELY T - [SDR DXTR2013082101](https://openairdocs.org/sdr/DXTR2013082101), Aug 21, 2013: SKIN. DAMAGED. DAMAGE TO NOSE SKIN ADJACENT TO THE RT NOSE GEAR DOOR AT CENTER HINGE POINT. (APPROX. 2.2500" IN LENGTH) PERFORMED REPAIR OF DAMAGED AREA IAW STS EA 15-2013-369 - [SDR DXTA2013020405268](https://openairdocs.org/sdr/DXTA2013020405268), Feb 1, 2013: ACTUATOR. FAILED. LANDING GEAR WOULD NOT RETRACT. UPON SELECTING THE GEAR HANDLE TO UP GEAR RETRACTION COMMENCED BUT PILOTS DID NOT HEAR THE NORMAL SOUND OF THE GEAR HITTING AND - [SDR DXTA2012080305076](https://openairdocs.org/sdr/DXTA2012080305076), Aug 2, 2012: ACTUATOR. FAILED. AFTER TAKEOFF, MLG HANDLE SELECTED UP, RED "UNLOCK" GEAR LIGHT ILLUMINATED. STAB MISCOMPAIR AND HYD PRESSURE LIGHT ALSO ILLUMINATED. MLG LOWERED NORMALLY FOR LA - [SDR DXTA2012071605052](https://openairdocs.org/sdr/DXTA2012071605052), Jul 14, 2012: SENSOR. INOPERATIVE. AFTER TAKEOFF, CLIMBING TO 3000 FT AT 160 KTS, THE GEAR RETRACTED, BUT THE RED GEAR UNSAFE LIGHT WAS ILLUMINATED. HYD PRESSURE AND STAB MISCOMPARE ILLUMINATED A - [SDR DXTA2012022304885](https://openairdocs.org/sdr/DXTA2012022304885), Feb 17, 2012: TRIM SYSTEM. CONTAMINATED. ROLL TRIM ANNUNCIATOR ILLUMINATED IN CRUISE. AUTOPILOT MANUALLY DISCONNECTED TO RETRIM AILERONS. AILERON TRIM WHEEL STUCK & WOULD NOT MOVE LT OR RT. ROLL TRIM A - [SDR DXTA2011111604793](https://openairdocs.org/sdr/DXTA2011111604793), Nov 15, 2011: ACTUATOR. CONTAMINATED. CAPTAIN`S AND F/O RUDDER PEDALS BECAME INCREASINGLY STIFF AT HIGHER ENGINE POWER SETTINGS. FOUND RUDDER BIAS ACTUATOR CORRODED AND FULL OF WATER. REPLACED ACTUA - [SDR DXTA2011010304392](https://openairdocs.org/sdr/DXTA2011010304392), Dec 31, 2010: ACTUATOR. INOPERATIVE. LT MAIN GEAR FAILED TO SHOW, DOWN AND LOCKED UPON LANDING. ROTORY TEST SHOWED BULB WORKED AND EMERGENCY CHECKLISTS WERE PREFORMED. T-HANDLE AND BLOW DOWN KNOB W ## 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/N568QS/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.