# N693QS: 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: 560-5657 - Year built: 2006 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 18, 2006 - Certificate issued: June 8, 2021 - Expires: June 30, 2028 - Mode S code: A9374A - 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=693QS - Page: https://openairdocs.org/aircraft/N693QS 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 N693QS. ## FAA accident and incident reports None matched to N693QS. ## 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 DXTA2026101310103](https://openairdocs.org/sdr/DXTA2026101310103), Oct 9, 2026: LIGHT. DETACHED. EMERGENCY LIGHTING SYSTEM IN THE FLOOR NEAR THE MAIN CABIN DOOR, THE LED STRIP THAT LIGHTS THE EMERGENCY PATH TO THE MAIN CABIN DOOR HAS BECOME DETACHED FROM IT - [SDR DXTA2026030307085](https://openairdocs.org/sdr/DXTA2026030307085), Mar 1, 2026: LIGHT. INOPERATIVE. A SEGMENT OF THE FLOOR EMERGENCY LIGHTING IS INOPERATIVE BELOW SEAT THREE. DURING T/S GAINED ACCESS TO THE LT AISLE EMERGENCY LIGHT HAD FEW LED LIGHT WERE OUT. - [SDR DXTA2025080604491](https://openairdocs.org/sdr/DXTA2025080604491), Aug 5, 2025: LIGHT. DISCONNECTED. AFT EMERGENCY EXIT LIGHT OVER LAVATORY TOILET NOT ILLUMINATING DURING AIRCRAFT POWER ON CHECKLIST. (AOG) AFT EMERGENCY EXIT LIGHT OVER LAVATORY TOILET NOT ILLUM - [SDR 2025FA0000420](https://openairdocs.org/sdr/2025FA0000420), Jun 24, 2025: PANEL. CORRODED. DURING EXTERNALLY SERVICEABLE TOILET DETAILED INSPECTION FOUND THE TOILET SEAT PANEL TO BE CORRODED AND CRACKING. PERFORM REPAIR TO TOILET DECK SKIN. COMPLIED W - [SDR DXTA2025022002398](https://openairdocs.org/sdr/DXTA2025022002398), Feb 16, 2025: HANDLE. STIFF. MAIN DOOR: REPEAT WRITE UP. MAIN ENTRY DOOR HANDLE IS DIFFICULT TO LOCK AND UNLOCK AND VERY DIFFICULT TO UNLOCK OR LOCK AFTER COLD SOAK FLIGHT. VIDEO ATTACHED. - [SDR DXTA2025010601819](https://openairdocs.org/sdr/DXTA2025010601819), Jan 3, 2025: COUNTERBALANCE. OUT OF RIG. MAIN DOOR: MAIN CABIN DOOR COUNTER BALANCE OUT OF RIG,( TENSION TOO HIGH.) DOOR SLAMS SHUT. CORRECTIVE ACTION: ADJUSTED COUNTER BALANCE TENSION. OPS CHECK GOOD. - [SDR DXTA2019081302751](https://openairdocs.org/sdr/DXTA2019081302751), Aug 13, 2019: WINDSHIELD. ODOR. COCKPIT HAD A BURNING ODOR, ON SHORT FINAL CREW NOTICED A SMELL SIMILAR TO BURNING RUBBER. ODOR CONTINUED UNTIL AIRCRAFT WAS POWERED DOWN. NO SMOKE OBSERVED, AN - [SDR DXTA2019071802634](https://openairdocs.org/sdr/DXTA2019071802634), Jul 18, 2019: PCB. UNSERVICEABLE. AT FL390 APPROX 25 MINUTES INTO THE FLIGHT A FAINT ODOR WAS NOTICED IN THE COCKPIT, AFTER CHECKING THE CABIN AND LAV AREA THE ODOR WAS NARROWED DOWN TO THE COCK - [SDR DXTA2019070802593](https://openairdocs.org/sdr/DXTA2019070802593), Jul 8, 2019: COOLING FAN. DIRTY. WHILE CLIMBING THRU FL300 WE STARTED TO SMELL A STRONG ODOR. IT WAS STRONGEST NEAR THE FRONT PANEL AND MORE SPECIFICALLY THE LEVEL OF THE MFD AND PFDS. ALL INDI - [SDR DXTA201907020256](https://openairdocs.org/sdr/DXTA201907020256), Jul 2, 2019: COOLING FAN. DIRTY. CLIMBING THROUGH FLIGHT LEVEL 210 OFF OF ASE I STARTED TO SMELL AN ODOR. WE HAD ENTERED PRECIPITATION AND I HAD ALSO TURNED ON THE ANT-ICE AND RADAR. SHORTLY AF - [SDR DXTA2019070202563](https://openairdocs.org/sdr/DXTA2019070202563), Jul 2, 2019: UNKNOWN. ODOR. CORRECTION/// CLIMBING THROUGH FLIGHT LEVEL 210 OFF OF ASE I STARTED TO SMELL AN ODOR. WE HAD ENTERED PRECIPITATION AND I HAD ALSO TURNED ON THE ANT-ICE AND RAD - [SDR JGVR20190308001](https://openairdocs.org/sdr/JGVR20190308001), Mar 8, 2019: STRAKE. DELAMINATED. DURING SANDING PROCESS FOUND RH STRAKE TO HAVE MULTIPLE AREAS OF CORROSION AND TWO AREAS OF DELAMINATED COMPOSITE BEYOND LIMITS. COMPLIED WITH SERVICE BULLETIN - [SDR DXTA2019022212056](https://openairdocs.org/sdr/DXTA2019022212056), Feb 20, 2019: LIGHT. SHORTED. FLOOR EMERG EXIT LIGHT - FORWARD FLOOR LEVEL ENTRY/EXIT LIGHT WAS SHORTING OUT WITH VISIBLE SMOKE AND SPARKS. INSPECTED AND FOUND LED ASSY LIGHT STRIP SHORTED I - [SDR DXTA2018122701835](https://openairdocs.org/sdr/DXTA2018122701835), Dec 27, 2018: UNKNOWN. SMOKE. AFTER NORMAL STARTUP OF BOTH ENGINES AND AFTER AVIONICS POWER ON, AN ABNORMAL CLICKING SOUND WAS HEARD (SOUNDED LIKE AN OVERACTIVE RELAY) THE SOUND LASTED FOR A - [SDR 2019F00070](https://openairdocs.org/sdr/2019F00070), Sep 21, 2018: SKIN PANEL. DAMAGED. REPAIR TO LT AND RT WING LOWER SKIN DAMAGE. REPAIR DEFINITION DQ15836M1 DATED SEPTEMBER 20, 2018. - [SDR 2019F00069](https://openairdocs.org/sdr/2019F00069), Sep 21, 2018: SKIN. DAMAGED. REPAIR OF RIGHT WING LEADING EDGE FASTENER PULLED THROUGH SKIN. REPAIR DEFINITION DQ15823M1 DATED SEPTEMBER 19, 2018. - [SDR DXTA2018090501385](https://openairdocs.org/sdr/DXTA2018090501385), Sep 3, 2018: MANIFOLD. LEAKING. COCKPIT ODOR, JET FUEL ODOR COMING FROM OVERHEAD VENTS. NOTICEABLE WITH APU RUNNING ON THE GROUND AND ALSO DURING FLIGHT WITHOUT APU. REMOVED & REPLACED LEAKING - [SDR DXTA2018012700514](https://openairdocs.org/sdr/DXTA2018012700514), Jan 27, 2018: OIL SYSTEM. LEAKING. WHILE PERFORMING COCKPIT PREPARATION AND BEFORE ENGINE START WITH APU OPERATING, LIGHT GRAY SMOKE WITH AN ACRID ODOR THAT WAS DETECTED AND OBSERVED. CREW SHUTDO - [SDR DXTAT2PL6D005CQDY](https://openairdocs.org/sdr/DXTAT2PL6D005CQDY), Sep 7, 2017: ENGINE. FAILED. CLIMBING THROUGH 12000 FEET, NR 2 ENGINE OIL PRESSURE RED LIGHT ILLUMINATED. FOLLOWED SHORTLY BY VIBRATION AND NR 2 ENGINE ITT SPIKED FULL SCALE. DECLARED EMERG - [SDR DXTA2014072205826](https://openairdocs.org/sdr/DXTA2014072205826), Jul 21, 2014: MOTOR. FAILED. DURING FLIGHT, ANTI-SKID INOPERATIVE ANNUNCIATOR LIGHT ILLUMINATED. LANDED AFTER RUNNING ABNORMAL CHECKLIST. LOST BRAKES AFTER LANDING, LOW BRAKE ANNUNCIATOR LI - [SDR DXTA2014040805721](https://openairdocs.org/sdr/DXTA2014040805721), Apr 7, 2014: BULB. INOPERATIVE. BOTH NOSE GEAR INDICATION LIGHTS APPEAR TO BE INOPERATIVE. FLEW BY CONTROL TOWER FOR VISUAL INDICATION & BLEW THE GEAR DOWN, LANDING WAS UNEVENTFUL. PERFORMED T - [SDR DXTA2013122605607](https://openairdocs.org/sdr/DXTA2013122605607), Dec 24, 2013: RESERVOIR. FAILED. THE RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKEOFF, LEADING TO A FLASHING HYD PRESSURE & STAB MISCOMPARE ANNUNCIATOR. AFTER ABOUT 45 SECONDS, GEAR UNS - [SDR DXTA2013121605597](https://openairdocs.org/sdr/DXTA2013121605597), Dec 13, 2013: PRINTED CKT BOARD. DEFECTIVE. LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. RED LIGHT STAYED ILLUMINATED WITH NO GREEN LIGHT. THERE WAS NOTICEABLE DRAG AS IF THE AIRPLANE WAS NOT CLEAN. EXTE - [SDR DXTA2013050805383](https://openairdocs.org/sdr/DXTA2013050805383), Apr 19, 2013: RING ASSEMBLY. UNSERVICEABLE. DURING INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. FOUND TWO NUTS MISSING AT POSITION NR 15 AND NR 24. COMPLIED WITH A HOT SE - [SDR DXTA2012021704877](https://openairdocs.org/sdr/DXTA2012021704877), Feb 16, 2012: PRESSURE SWITCH. INOPERATIVE. DURING TAXI, LOW BRAKE PRESSURE AND ANTI-SKID INOPERATIVE ANNUNCIATORS ILLUMINATED AND CREW LOST BRAKE PEDAL PRESSURE. STOPPED ACFT ON TAXIWAY VIA EMERGENCY BRA - [SDR DXTA2011072204664](https://openairdocs.org/sdr/DXTA2011072204664), Jul 22, 2011: WHEEL. MALFUNCTIONED. ON DEPARTURE, AUTOPILOT DISENGAGED AND SIGNIFICANT FORWARD PRESSURE REQUIRED ON CONTROL WHEEL. AUTOPILOT WAS REENGAGED AND DISENGAGED 2 MORE TIMES UNTIL ACFT WA - [SDR DXTA2011070504641](https://openairdocs.org/sdr/DXTA2011070504641), Jul 2, 2011: FLAP SYSTEM. MALFUNCTIONED. DURING TAKEOFF, FLAP 15 IMMEDIATELY AFTER ROTATION, A GRINDING/RUBBING FELT IN THE YOKE WITH FORE AND AFT YOKE MOVEMENTS. AFTER RETACTION OF FLAPS AND LEVEL OFF - [SDR DXTA2010092004246](https://openairdocs.org/sdr/DXTA2010092004246), Sep 18, 2010: ACTUATOR. WORN. UNSAFE GEAR ANNUNCIATOR ILLUMINATED AFTER GEAR RETRACTION. TROUBLESHOT TO NOSE STRUT EXTENSION GREATER THAN 9.10 INCHES, IT IS 9.25 INCHES. WHEN RETRACTED UPLOC - [SDR DXTA2010091304234](https://openairdocs.org/sdr/DXTA2010091304234), Sep 10, 2010: ACTUATOR. FAILED. GEAR WOULD NOT RETRACT. TROUBLESHOT TO BAD NLG ACTUATOR. R & R NLG ACTUATOR AND BLED HYD SYS. OPS CHECKED GOOD IAW MM 32-30-03. - [SDR DXTA2009120403879](https://openairdocs.org/sdr/DXTA2009120403879), Nov 12, 2009: WIRE HARNESS. CHAFED. WHILE TAXIING RIGHT BRAKE FAILED AND ANTI-SKID LT ILLUM. RESET RT ADCR BIT AND APPLIED BRAKES. ANTI-SKID LT ILLUM BUT RT ADCR BIT OK. FOUND A GEAR WIRING HARNES - [SDR DXTA2009111303856](https://openairdocs.org/sdr/DXTA2009111303856), Nov 12, 2009: UPLOCK SWITCH. OUT OF ADJUST. WHILE TAXIING, RT BRAKE FAILED AND ANTI-SKID LT ILLUM, RESET RT ADCR BIT AND APPLIED BRAKES. ANTI-SKID LT ILLUM BUT RT ADCR BIT OK. FOUND NOSE LANDING GEAR UPLO - [SDR DXTA2009070703721](https://openairdocs.org/sdr/DXTA2009070703721), Jul 7, 2009: LINE. LEAKING. FUEL FUMES IN COCKPIT AND CABIN WITH APU BLEED AIR ON. SECURED APU AND FUMES STOPPED. REMOVED SECONDARY FUEL MANIFOLD P/N 38838991 DUE TO A FITTING ON LINE LEAK - [SDR CWQR200901](https://openairdocs.org/sdr/CWQR200901), Mar 10, 2009: STIFFENER. MISINSTALLED. DURING A SCHEDULED INSPECTION, FOUND THE LANDING ACTUATOR CHAFING STIFFENER P/N 6621211-26 LOCATED IN LT MAIN GEAR WELL. CONTACTED MFG FIELD ENGINEERS, DISCOVER - [SDR DXTA200802954](https://openairdocs.org/sdr/DXTA200802954), Mar 20, 2008: ENGINE. POWER LOSS. LT ENGINE WILL NOT MAKE TAKEOFF POWER IN THE TAKEOFF DETENT AND WITH EECS IN AUTO AND FAILED TO MANUAL. RAN ENGINES AT 88.4 PERCENT N1 WITH SEVERAL ACCELERATION - [SDR DXTA20082954](https://openairdocs.org/sdr/DXTA20082954), Mar 20, 2008: ENGINE. POWER LOSS. LT ENGINE WILL NOT MAKE TAKEOFF POWER IN THE TAKEOFF DETENT AND WITH EECS IN AUTO AND FAILED TO MANUAL. RAN ENGINES AT 88.4 PERCENT N1 WITH SEVERAL ACCELERATION - [SDR DXTA200702722](https://openairdocs.org/sdr/DXTA200702722), Dec 30, 2007: CONTROL WHEEL. DAMAGED. (EMERGENCY DECLARED) ON ROTATION AN UNUSUAL NOSE UP FORCE WAS NOTED REQUIRING FULL NOSE DOWN TRIM. BOTH PILOTS APPLIED NOSE DOWN PRESSURE AND CONDITION WORSENED - [SDR DXTA200702674](https://openairdocs.org/sdr/DXTA200702674), Dec 12, 2007: BLEED ACTUATOR. INOPERATIVE. DURING DESCENT FROM CRUISE ALTITUDE, CREW EXPERIENCED ENGINE VIBRATION ACCOMPANIED BY EEC MANUAL L ADVISORY WITH NO ENG VIB ANNUNCIATOR. THROTTLE AY IDLE ITT= 6 - [SDR DXTA200702126](https://openairdocs.org/sdr/DXTA200702126), Apr 21, 2007: ACCESS PANEL. MISINSTALLED. IN FLIGHT ABOVE 200 KTS THERE IS A RUMBLING VIBRATION THAT VIBRATES THE WHOLE AIRPLANE. IT CHANGES PITCH OR SEVERITY WITH INCREASE IN SPEED, 250 KTS IS THE SPEE ## 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/N693QS/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.