# N587QS: 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: 560-5805 - Year built: 2008 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 15, 2008 - Certificate issued: September 29, 2021 - Expires: September 30, 2028 - Mode S code: A79158 - Registered owner: [Netjets Sales Inc](https://openairdocs.org/faa-owner/NETJETS%20SALES%20INC) - Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City) - Owner type: Corporation - Owner's area on the map: 35.5467° N, 97.5646° W: Placed by OpenAirDocs at the center of ZIP code 73116, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=587QS - Page: https://openairdocs.org/aircraft/N587QS 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 N587QS. ## FAA accident and incident reports (1) 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 20250223000429I](https://openairdocs.org/incident/20250223000429I), Feb 23, 2025: Cessna 560XL (N587QS), Charleston, SC, Minor damage. The aircraft struck a deer which was crossing the runway during takeoff at kjzi. The aircraft landed at kchs where the only damage maintenance found was at the… ## 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 DXTA2026051808088](https://openairdocs.org/sdr/DXTA2026051808088), May 14, 2026: BRAKE SYS. FAULTED. DURING LANDING AT APPROX 80KTS, ANTISKID INOP ANNUNCIATION ILLUMINATED. CLEARED & CAME BACK ON. BRAKES WERE INOP DURING BRIEF TAXI OFF OF RUNWAY. THE BRAKES DID - [SDR DXTA2025120105872](https://openairdocs.org/sdr/DXTA2025120105872), Nov 27, 2025: WIRE HARNESS. FAULTED. DURING FLIGHT ANTISKID LIGHT WOULD ILLUMINATE AND EXTINGUISH BEFORE COMPLETION OF AMBER C1 ANTISKID INOP CHECKLIST. DURING TAXI, ANTISKID INOP LIGHT ILLUMINATED - [SDR DXTA2025101305277](https://openairdocs.org/sdr/DXTA2025101305277), Oct 10, 2025: WIRE SPLICE. DAMAGED. THE LEFT FLOOR EMERGENCY LIGHTS ARE EXTREMELY DIM. ALL OTHER LIGHTS ARE BRIGHT. WHEN THE FLOOR LIGHTS ARE TAPPED, THEY GET BRIGHT FOR A SECOND THEN RETURNS TO B - [SDR DXTA2025072304334](https://openairdocs.org/sdr/DXTA2025072304334), Jul 22, 2025: HANDLE. BINDING. MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO OPEN OR CLOSE DOOR FROM INSIDE CABIN. INSPECTED AND NOTED TWO DOOR PINS ADJUSTED TO TIGHT AND BINDING IN THE - [SDR 2025FA0000203](https://openairdocs.org/sdr/2025FA0000203), Mar 24, 2025: STRAKE. CORRODED. LH AND RH STRAKES HAVE SEVERAL AREAS OF CORROSION ON UPPER AND LOWER SURFACES. PERFORMED 4 EACH DOUBLER REPAIRS TO LH STRAKE AND PERFORMED 6 EACH DOUBLER REPAIR - [SDR 2025FA0000201](https://openairdocs.org/sdr/2025FA0000201), Mar 22, 2025: STRAKE. CORRODED. LH STRAKE TRAILING EDGE WEDGE FITTING - [SDR DXTA2024092500648](https://openairdocs.org/sdr/DXTA2024092500648), Sep 23, 2024: DOOR. OUT OF ADJUST. MAIN CABIN DOOR NEEDS ADJUSTED. AFTER LANDING WITH COLD SOAKED AIRCRAFT, MAIN CABIN DOOR WILL NOT STAY IN DOWN LOCKED POSITION USING CABIN DOOR HANDLE. CORRECTI - [SDR DXTA2024071712372](https://openairdocs.org/sdr/DXTA2024071712372), Jul 16, 2024: LIGHT. INOPERATIVE. AISLE EMERGENCY LIGHTING ON LEFT, FRONT HALF OF THE AISLE ONLY LIGHTS FROM THE GALLEY TO JUST FORWARD OF SEAT 3 (AFT FACING SEAT ON LEFT SIDE). IT IS INOP FROM - [SDR DXTA2024040211384](https://openairdocs.org/sdr/DXTA2024040211384), Apr 2, 2024: BATTERY. INOPERATIVE. EMERGENCY LIGHTS BATTERY INOP ON PRE-FLIGHT. REMOVED FAULTY FWD BATTERY PACK & INSTALLED OVERHAULED BATTERY PACK IAW MM 33-50-01. REMOVED FAULTY AFT BATTERY PAC - [SDR DXTA2024011510611](https://openairdocs.org/sdr/DXTA2024011510611), Jan 13, 2024: UNKNOWN. UNKNOWN. MAIN DOOR WILL NOT LOCK IN DOWN PISITION FROM INSIDE CABIN. IT WILL LATCH DOWN FRIM OUTSIDE HANDLE. OP'S CHECKED DOOR COMFRIMED THAT IT WASNT LOCKING. ADJUSTED - [SDR DXTA2023110299510](https://openairdocs.org/sdr/DXTA2023110299510), Nov 1, 2023: UNKNOWN. UNKNOWN. THE MAIN DOOR IS HEAVILY WEIGHTED TOWARDS THE CLOSED POSITION. WHEN INSIDE & CLOSING THE DOOR IT SLAMS SHUT. WHEN ON THE OUTSIDE WITH A CLOSED DOOR, VERY DIFFIC - [SDR 3J7R2023061300001](https://openairdocs.org/sdr/3J7R2023061300001), Jun 13, 2023: BATTERY PACK. DISCHARGED. EXTERIOR EMERGENCY LIGHTS AND AFT LEFT BULKHEAD EXIT SIGN ARE INOP WHEN THE MAIN BATTERY IS OFF. CHARGED FOR 1.5 HOURS AND HAD THE SAME RESULT. - [SDR DXTA2023010978130](https://openairdocs.org/sdr/DXTA2023010978130), Jan 8, 2023: SWITCH. OUT OF ADJUST. ON TAKE OFF, RECEIVED A FLASHING HYD PRESS WITH A MASTER CAUTION AFTER FLAP RETRACTION. GEAR & FLAPS RETRACTED ON SCHEDULE. HYD PRESS, NLG UNLOCK LIGHT, & STAB - [SDR DXTA2022121976520](https://openairdocs.org/sdr/DXTA2022121976520), Dec 17, 2022: BATTERY. DEFECTIVE. MAIN EXIT SIGN/LIGHT: FORWARD EMERGENCY POWER BATT PACK WILL NOT TAKE CHARGE - LIGHTS ARE OUT. // SIGNOFF // REMOVED AND REPLACED THE FWD EMERGENCY BATTERY PACK - [SDR DXTA2021052442490](https://openairdocs.org/sdr/DXTA2021052442490), May 22, 2021: SEAL. DEFECTIVE. MAIN DOOR: MAIN CABIN DOOR OPEN WITH EXTREME DIFFICULTY AFTER BEING AT ALTITUDE FOR ANYTHING OVER ONE HOUR. I.E. ONCE OPEN ON THE GROUND IT OPERATES FINE. REPEA - [SDR DXTA2021033040270](https://openairdocs.org/sdr/DXTA2021033040270), Mar 30, 2021: CONTROL VALVE. DEFECTIVE. ACM OVERHEAT ON TAKEOFF. THERE WAS A HOT/BURN SMELL IN THE AIRCRAFT. COMPLETED CHECKLIST AND LANDED. DID NOT DECLARE AN EMERGENCY. DID NOT LAND OVER WEIGHT. COM - [SDR DXTA2020122404515](https://openairdocs.org/sdr/DXTA2020122404515), Dec 24, 2020: DOOR. FROZEN. MAIN CABIN DOOR FROZEN SHUT. OPENED EMERGENCY EXIT DOOR TO EGRESS AIRCRAFT. EMERGENCY EXIT DOOR REQUIRES REINSTALLATION. COMPLIED WITH TASK T2PL6D007YVC5. INSPE - [SDR DXTA2020111304353](https://openairdocs.org/sdr/DXTA2020111304353), Nov 13, 2020: RELIEF VALVE. ABNORMAL. WHILE TAXIING IN, THE "LOW BRAKE PRESSURE" AND "ANTI SKID INOP" AMBER MESSAGES ILLUMINATED. A FEW SECONDS LATER, THE BRAKE PEDALS WENT TO THE FLOOR AND WE HAD A - [SDR DXTA2020072903913](https://openairdocs.org/sdr/DXTA2020072903913), Jul 28, 2020: COUNTERBALANCE. OUT OF ADJUST. THE MAIN CABIN DOOR IS OUT OF ADJUSTMENT. IT IS HARD TO OPEN FROM THE INSIDE AND IT SLAMS SHUT WHEN CLOSING.ADJUSTED CABIN ENTRY DOOR COUNTERBALANCE ASSEMBLY IA - [SDR 2019F00003](https://openairdocs.org/sdr/2019F00003), May 1, 2018: SKIN. CRACKED. RIGHT NOSE LG DOOR SKIN CRACKED AT THE LATCH. - [SDR DXTA2017051706404](https://openairdocs.org/sdr/DXTA2017051706404), May 17, 2017: WINDSHIELD. DAMAGED. DURING CRUISE FLIGHT AT FL400 AFTER 25 MINUTES AT FL400 A STRONG SMELL OF BURNING WIRES. THAT SMELL CONTINUED ON THE FLIGHT DECK THEN AFTER 15 MINUTES OF THE BU - [SDR DXTR2016122901](https://openairdocs.org/sdr/DXTR2016122901), Dec 29, 2016: SKIN. DENTED. RIGHT LOWER WING SKIN AT RWS 143.07 DENTED, REPAIRED IAW ERO-877762. - [SDR DXTR2016122801](https://openairdocs.org/sdr/DXTR2016122801), Dec 28, 2016: STRUCTURE. CORRODED. CORROSION FOUND UNDER THE DATA PLATE ON THE TAILCONE. REPAIRED CORROSION IAW DQ6626. - [SDR DXTR2016122702](https://openairdocs.org/sdr/DXTR2016122702), Dec 27, 2016: STRUCTURE. CORRODED. CORROSION FOUND IN MULTIPLE LOCATIONS ON THE UPPER SIDE OF THE LT AND RT WINGS. REPAIRED IAW REPAIR S-560XL-5805/06RD. - [SDR DXTR2016122701](https://openairdocs.org/sdr/DXTR2016122701), Dec 27, 2016: STRUCTURE. CORRODED. CORROSION FOUND IN MULTIPLE LOCATIONS ON THE UPPER SIDE OF THE LT AND RT WINGS. REPAIRED IAW REPAIR S-560XL-5805/06RD. - [SDR DXTR2015092901](https://openairdocs.org/sdr/DXTR2015092901), Sep 26, 2015: SPAR. GOUGED. GOUGES ON LT AND RT FWD SIDE OF THE VERTICAL SPAR. GOUGE DAMAGE WAS FOUND ON THE FWD SURFACE OF THE LOWER AFT VERTICAL STABILIZER SPAR WEB. REPAIRED IAW SR 5805 - [SDR DXTR2015092301](https://openairdocs.org/sdr/DXTR2015092301), Sep 23, 2015: BULKHEAD. GOUGED. A GOUGE & A SCRATCH WERE FOUND ON THE AFT SIDE OF THE 6611371-1 AFT PRESS BULKHEAD BOND ASSEMBLY AT FS 373.75, RBL 29.63, WL 114.27, NEAR STRINGER 11R. THE GOUG - [SDR DXTA2015042706011](https://openairdocs.org/sdr/DXTA2015042706011), Apr 26, 2015: BULB. INOPERATIVE. WHEN LANDING, LEFT MAIN GEAR DIDN'T HAVE GREEN LIGHT. PERFORMED EMERGENCY GEAR EXTENSION. FOUND THE LT GEAR DOWN & LOCK LIGHT BULBS INOPERATIVE. REMOVED THE FAI - [SDR 2011FA0000397](https://openairdocs.org/sdr/2011FA0000397), Jun 14, 2011: BOLT. WORN. TWO PUSH/PULL TUBES THAT ATTACH TO THE AFT ELEVATOR BELLCRANK, WHEN TORQUING ATTACHING HARDWARE, THE NUT SHANKS OUT ON THE BOLT, ALLOWING THE BOLT TO BE ROTATED - [SDR 2011FA0000396](https://openairdocs.org/sdr/2011FA0000396), Jun 14, 2011: SHAFT. WORN. FOUND GROOVES WORN INTO SHAFT OF THE 2 SCREWS THAT ENTER INTO THE RUDDER ACTUATOR ASSEMBLY. ACFT IS SET FOR CRUISE CONFIGURATION: DURING FLIGHT, TAIL VIBRATES C - [SDR DXTA2011032104520](https://openairdocs.org/sdr/DXTA2011032104520), Mar 20, 2011: ACTUATOR. BINDING. ELEVATOR TRIM TAB JAMMED AND COULD NOT BE MOVED ELECTRICALLY OR MANUALLY. FLIGHT WAS AT 41000' AND THE PITCH TRIM ANNUNCIATOR ILLUMINATED DESCENDING THROUGH 340 - [SDR DXTA2011010304386](https://openairdocs.org/sdr/DXTA2011010304386), Jan 2, 2011: AHRS. ILLUMINATED. RED HEADING AND ATTITUDE FAIL MESSAGE ON THE NR 2 PFD. REMOVED FAULTY NR 2 AHRS & INSTALLED. OPS CHECKED REPAIRED UNIT IAW MM 34-21-01. OPS CHECKED GOOD. - [SDR DXTA2010120304345](https://openairdocs.org/sdr/DXTA2010120304345), Dec 2, 2010: TRIM SYSTEM. MALFUNCTIONED. DURING THE DESCENT FROM 39000' THE PITCH TRIM ANNUNCIATION ON THE PFDS CAME ON. WITH THE AUTOPILOT OFF THE TRIM WHEEL COULD NOT BE TRIMMED ANY FURTHER FWD. AT L - [SDR DXTA2010112904336](https://openairdocs.org/sdr/DXTA2010112904336), Nov 28, 2010: STRUT. LEAKING. ON FINAL APPROACH THE LT MLG FAILED TO FULLY EXTEND TO GIVE A GREEN DOWN AND LOCKED LIGHT INDICATION. THE LANDING GEAR WAS BLOWN DOWN IAW THE EMERGENCY CHECKLIS - [SDR 2010F00027](https://openairdocs.org/sdr/2010F00027), Mar 4, 2010: TUBE. SHORT. THE RUDDER CONTROL CABLES PASS THROUGH A PLASTIC GUIDE TUBE BETWEEN WING AND FUSELAGE. THIS GUIDE TUBE IS NOT SUPPORTED AT AFT END. IT IS TOO SHORT TO PASS THRO - [SDR DXTA20090908037](https://openairdocs.org/sdr/DXTA20090908037), Sep 6, 2009: CONTROL CABLE. OUT OF ADJUST. CHECKED ALL FLT. CONTROL CABLES (PRIMARY) IAW MM 27-10-00, 27-20-00 & 27-30-00. ADJUSTED & CHECKED AILERON WING, FUSELAGE & SERVO CABLE TENSION IAW MM 27-10-00. - [SDR DXTA2009090803775](https://openairdocs.org/sdr/DXTA2009090803775), Sep 6, 2009: CONTROL COLUMN. VIBRATION. EXCESSIVE VIBRATION IN CONTROL YOKE/COLUMN STARTING AT 230 KTS, APPROX 9-10K FT, CONTINUED AT ALL A/S AND ALTITUDES ABOVE THAT. REPEAT WRITE-UP. VIBRATES WITH A - [SDR DXTA200906043678](https://openairdocs.org/sdr/DXTA200906043678), Jun 4, 2009: ACTUATOR. BYPASSING. STAB MISCOMPARE ILLUMINATED AFTER TAKOFF, RAN CHECKLIST AND LIGHT WENT OUT AFTER THE HYD CONTROL C/B WAS CYCLED. FOUND HORIZ STAB ACTUATOR BYPASSING HYDRO FLUID ## 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/N587QS/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.